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Welding - Science topic

A forum to discuss welding processes and procedures
Questions related to Welding
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I want to simulate TIG welding in ansys using 2 moving heat source to cover circumference and element birth and death method and using convection and radiation as thermal boundary conditions.  I am getting error each time  Please Help Me.
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Let's try to troubleshoot further. Can you please provide more details about your simulation setup: 1. What type of analysis are you running (e.g., steady-state, transient, thermal)? 2. What are your boundary conditions (e.g., temperature, heat flux, convection)? 3. What materials are you using, and have you checked their thermal properties? 4. Have you applied any mesh controls or refinements? 5. Are there any other warnings or errors in the ANSYS output? Additionally, you can try: 1. Checking the ANSYS documentation for specific guidance on temperature limits. 2. Searching online forums or communities for similar issues. 3. Reaching out to ANSYS support or consulting with an expert. Let's work together to resolve this issue!
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There is very tiny gap when I zoomed in
Steel Pipe - Solid Element create in Parts section - 3mm thickness
Rebar - Wire Truss element create in Parts Section - 6mm thickness
Interaction used - Tie Constraint
How connect - Welded (I hope Tie constraint is the best way of interaction for this occasion, if not please advise me best way to do this with some steps as I am kind of starter for this simulations)
Tried things
Use Tie pair with position tolerance of 1 and still did not work
Tried to cut this steel tube in to parts and then through the point I get give datum point exact location and. Use translate that rebar node to datum point, did not work - Because it is too close. Some error message 2nd point is coincidence and cannot do it.
Question - Please give me best solution to get accurate results how to use interaction between this two and avoid this error and what are the solution to avoid this space and use accurate interaction. Please help with this problem
Warning Error Messages -
For *tie pair (assembly__pickedsurf1023-assembly__pickedset1022_cns_), adjustment was specified but no node was adjusted more than the adjustment distance = 2.22000e-16.
For *tie pair (assembly__pickedsurf1034-assembly__pickedsurf1033), adjusted nodes with very small adjustments were not printed. Specify *preprint,model=yes for complete printout.
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The issue you are facing stems from the small gap between the steel pipe and the rebar and the challenges in defining the correct interaction in ABAQUS. Below is a step-by-step guide and explanation to resolve this problem:
1. Understanding the Problem
• Tiny Gap Issue: When you zoom in, the small gap (which is likely due to mesh discretization or geometry definition) prevents the tie constraint from effectively linking the steel pipe and the rebar.
• Warnings: These indicate that no nodes were adjusted to create the tie constraint, meaning ABAQUS could not establish the required interaction due to the tiny or nonexistent overlap.
2. Corrective Steps
Geometry Preparation
1. Ensure Perfect Contact:
• In the Part section, align the rebar’s position so that it touches the steel pipe precisely. Use datum points or reference geometry to ensure the rebar is positioned correctly.
• Avoid manual adjustments by ensuring the pipe and rebar geometry aligns during part creation.
2. Use Boolean Operations (Optional):
• Instead of relying on tie constraints for separate parts, you can use Boolean operations to merge the pipe and rebar into a single part (if suitable for your analysis).
Interaction - Tie Constraint
1. Modify the Tie Constraint Settings:
• Set a position tolerance in the tie constraint interaction. The default tolerance may be too small.
• Try increasing the position tolerance slightly beyond the gap size (e.g., start with 0.01 or 0.1 depending on your model units).
2. Use Adjustments:
• Enable the “Adjust Slave Surface” option to allow ABAQUS to slightly move the nodes of the rebar or pipe to bridge the gap.
3. Switch Master-Slave Roles:
• Set the steel pipe surface as the master and the rebar as the slave. This ensures that the larger element (pipe) controls the interaction.
Alternative Interaction (General Contact)
• If the tie constraint fails:
• Use “General Contact” in the Interaction module:
• Define a contact interaction with frictionless or small sliding properties.
• This can simulate a welded connection without needing precise alignment.
Mesh Refinement
• A coarse mesh might exaggerate small gaps. Refine the mesh near the pipe and rebar to improve the node alignment.
3. Simulation Workflow
1. Rebuild Geometry:
• Re-check the alignment and ensure the rebar and pipe surfaces are precisely touching.
2. Define Interaction:
• Use a Tie Constraint with a higher position tolerance or enable node adjustment.
3. Verify Connection:
• Run a preliminary simulation to confirm the interaction is working. Check the interaction outputs in the .dat file or visualization.
4. Solutions to Avoid This Issue in the Future
1. Use Reference Geometry for Alignment:
• Ensure exact positioning during the part creation phase.
2. Simplify Geometry:
• Where possible, use a single part for welded components.
3. Improve Meshing:
• Use finer meshes near interaction zones to reduce gaps.
5. Summary
The best solution for your case would be to:
1. Align the rebar and pipe accurately in the geometry setup phase.
2. Use a Tie Constraint with adjusted settings (increased position tolerance, adjust slave surface).
3. Refine the mesh near the rebar-pipe interface.
If the Tie Constraint still doesn’t work, try General Contact with appropriate settings.
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Marble’s reagent is not working well on our weld metals. Just wondering if anybody has any suggestions before we start trying all the different acids from the ASM handbook.
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Dear Dr. Alireza Nabavi ,
I suggest you to have a look at the following, interesting document:
-Metallographic Stainless Steel Etchants by PACE Technologies
Available at:
Good luck and my best regards, Pierluigi Traverso (CNR-IAS-Genoa).
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Dear Scientists,
Is it possible to fabricate/weld/have Nobelium (No) based Superalloys?
It is a radioactive material & has a half-life of 58 minutes.
Please give me the guidelines. Thank you
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I can't imagine this to be practical. We are talking about No-259 with half-life of 58 minutes, which alpha-decays to Fm-255 with half-life of 20 hours, which alpha-decays to Cf-251 with half-life of nearly 900 years, which can be considered "stable" for the intended application.
But why bother to have two alpha decays per atom (producing radiation and its associated problems), when you could start-off with Californium (Cf) in the first place? To try to answer your question: I am guessing it might be possible, but is it worth the effort?
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For two metals with large differences in corrosion resistance(for example, Al and Ti weld joint), during the corrosion process of metallographic sample preparation, one phase will be corroded completely while the other phase will be corroded excessively or not corroded, and clear metallographic photographs of the two phases cannot be obtained.
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To obtain clear metallographic photos of dissimilar metals like aluminum (Al) and titanium (Ti) with different corrosion resistances, follow these effective steps:
  1. Mechanical Polishing: Use finer abrasives to reduce surface damage.
  2. Selective Etching: Choose an etchant that selectively attacks one metal while preserving the other. Experiment to find the right balance.
  3. Protective Coatings: Apply a protective layer (like lacquer) on the more corrosion-resistant metal before etching to prevent damage.
  4. Controlled Environment: Maintain controlled conditions (pH, temperature) during etching to minimize differential corrosion.
  5. High-Resolution Imaging: Use techniques like scanning electron microscopy (SEM) for detailed images without traditional sample preparation issues.
These methods will help you achieve clear metallographic images of both phases.
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I am not getting proper steps for rotary friction welding
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May I get your case?
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I am joining two tubular shell element and forming one T Joint(Tubular).. I want to consider welding effect at the joint . How can i do it ?.. I am using Abaqus 2023 version.. I search on documents it is suggested that use Abaqus Welding Inference (AWI) . But im not able to do it in 2023 version... Please help me out.
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Hi Ram,
It might help if you could provide some background to your question. For example:
  • What materials are the tubes made of?
  • What if the welding process being used?
  • How will the tubular joint be used after it has been made?
  • What aspect of the weld do you think you should model and why?
Regards,
Simon
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What is the difference between 6010 and 7018 welding rods
What is the difference between 6010 and 7018 welding rods:6010 and 7018 are both types of welding electrodes used in shielded metal arc welding (SMAW), also known as stick welding.
Differences between 6010 and 7018 welding rods
Electrode E6010 and E7018:
  • 6010: It is classified as a fast-freeze or fast-fill electrode. It has a cellulose-based coating that provides deep penetration and is designed for welding in the flat, horizontal, vertical, and overhead positions. 7018: It is classified as a low-hydrogen or iron powder electrode. It has a basic or low-hydrogen coating that produces strong and ductile welds. It is typically used for welding in the flat and horizontal positions. more info : https://weldmetals.blogspot.com/
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The main difference between 6010 and 7018 welding rods lies in their tensile strength, coating, and applications. 6010 rods have a tensile strength of 60,000 psi, a cellulose-based coating, and are known for their deep penetration, making them ideal for welding through dirty or less-prepared surfaces like pipes and structural joints. They are used primarily with DC. In contrast, 7018 rods have a higher tensile strength of 70,000 psi, a low-hydrogen coating, and produce smoother, cleaner welds, making them suited for heavy structural applications like construction and bridge work. They can run on both AC and DC and require cleaner surfaces to avoid defects.
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for example, calculate the percentage of welding nugget elements AISI 304 to carbon Steel
thanks for your attention.
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You can simulate in SYSWELD followed by validation with the nugget size and shape. In this software, there's a feature that can indicate the percentage of phases such as Austenite, Ferrite, etc.
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What is the difference between 6010 and 7018 welding rods:6010 and 7018 are both types of welding electrodes used in shielded metal arc welding (SMAW), also known as stick welding.
6010 welding rods are known for their deep penetration and fast freezing slag, making them suitable for welding in all positions, including overhead. They are commonly used for welding thick metals, such as steel and iron, and are often employed in construction, shipbuilding, and heavy fabrication industries. However, 6010 rods produce a rougher weld bead and require more skill to use effectively.
7018 welding rods, on the other hand, are known for their smooth weld bead and low spatter, making them ideal for welding thin metals and producing high-quality welds. They are often used in applications where precision and a clean finish are required, such as in automotive, aerospace, and pipe welding. However, 7018 rods require a higher level of skill and experience to use properly, as they are more sensitive to welding conditions and can be more challenging to control.
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we need surface area, corrosion current, equivalent weight and density of the metal involved for corrosion rate calculation in mm/year (lets say). For dissimilar metal welds, how can we measure equivalent weight and density? Is there other way to measure and compare corrosion rate?
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Dear Professors and Researchers,
We have been privileged to edit a book on "Advances in Solid-State Welding and Processing of Metallic Materials" that would be published by CRC Press, Taylor and Francis Group, USA.
We invite you to contribute a book chapter to the edited book in the above-mentioned areas of research. We request your contribution to this noble academic knowledge-sharing process.
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Is the proposal still on ?
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I want to realize a auto-analyze process for weld fatigue by fe-safe software. However, I found that the current.macro in Tools can not record the commands of the GUI operation about defining the welds and assigining the element groups for them. For each project, I can only manually define the weld and assign the element groups for them, and cannot achieve this trivial process by way of instructions or scripts, which hinders the realization of batch processing
Can anyone help solve this problem?
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Follow this approach:
1. **Use the fe-safe script interface**: Instead of relying on the GUI operations, you can use the script interface provided by fe-safe to programmatically define the welds and assign the element groups. This will allow you to create a reusable script that can be executed for batch processing.
The fe-safe script interface is typically accessible through a scripting language, such as Python or MATLAB. You can find the documentation and examples for the script interface in the fe-safe user manual or by contacting the fe-safe support team.
Here's a general outline of the steps you can follow:
a. **Initialize the fe-safe environment**: Connect to the fe-safe application and create a new analysis or open an existing one.
b. **Define the welds**: Use the script interface to define the weld locations and their properties, such as the start and end points, weld type, and associated element groups.
c. **Assign element groups to the welds**: Use the script interface to select the relevant element groups and associate them with the defined welds.
d. **Save the analysis**: After defining the welds and assigning the element groups, save the analysis to be used for the fatigue evaluation.
2. **Investigate alternative approaches**: If the script interface does not provide the necessary functionality, you could explore other options, such as:
a. **Modify the current.macro file**: Investigate if you can directly edit the current.macro file to include the necessary commands for defining the welds and assigning the element groups. This may require a deeper understanding of the file format and the available commands.
b. **Develop a custom automation tool**: Create a separate application or script that can interface with the fe-safe software and automate the weld definition and element group assignment process. This could involve using the fe-safe API or developing a standalone tool that interacts with the fe-safe GUI.
c. **Collaborate with fe-safe developers**: Reach out to the fe-safe support team or developers to understand if there are any planned or potential improvements to the automation capabilities in the software. They may have suggestions or be able to provide guidance on the best approach to achieve your desired level of automation.
Hope it helps. partial credit AI
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I am using apparent heat method for simulation
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this is my simulation
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I conducted a tensile test to analyze the strength of a welded joint and to implement an FEM model. Due to the high hardness of the base material, slippage between the grip and the base material was anticipated, so an additional jig was fabricated for the test. The specimen consisted of two base materials, each 50 mm wide and 120 mm long, connected by welding, with a total length of 240 mm. Since the strength of the welded joint was expected to be weaker and its area smaller compared to the base material, the deformation was anticipated to be localized to the welded joint.
In the test results, the specimen reached the fracture point after a total deformation of approximately 6 mm. However, as expected, the actual specimen exhibited deformation localized to the welded joint, with less than 1 mm of deformation (a difference of about 5 mm). Initially, I thought this error was caused by slippage between the grip and the jig, but after reading Han Lu's question, I reconsidered.
Han Lu's Question
1) If there was no slippage between the grip and the jig, is it reasonable to think that the difference in deformation between the specimen and the test data(almost 5 mm) is due to the deformation of the machine?
2) If the deformation in the test data includes the machine deformation and thus cannot be trusted, can the maximum load be considered a reliable result?
3) Given that the length of the welded joint is quite short, should I consider using DIC or an extensometer to obtain accurate data?
In conclusion, the test was conducted to implement a model for FEM analysis, but I would like to know if such data can be used to create the model.
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Hi Minseong,
Thank you for your reply with the explanation of the need for the strength of a tack weld.
I have worked on the structural analysis of welded joints for many years, including the use of FEA.
Will your final CAE model be made from brick elements? If yes, will you have a fine mesh that is able to predict the stress distribution in the fillet weld? And, if so, will you predict the tack failure when the peak stress (or strain) is equal to a critical value. Or, will you determine the average stress in the tack weld and compare it to the measured strength in the tests?
Also, I assume that some tack welds will experience both direct and shear loads. It seems that your testing only applies a direct load.
You might find that previous work on fillet welds would be useful, for example:
Effect of loading angle on the behaviour of fillet welds
And
Fillet and PJP welds
Regards,
Simon
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Hello,
I have modeled a steel conical roof in Abaqus. Now I want to model the location of a groove weld in Abaqus in a spiral pattern from the bottom to the top of the roof. How should I model this groove?
It is very important that I only want to model the weld location, not the welding process itself (the blue area in the image).
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Hi
You can accurately draw it in CATIA V5R21 and insert it to ABAQUS.
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I am trying to simulate the above truss in Abaqus to get its natural frequencies through Modal Analysis. The joints are connected through welding. However, I am unsure how to define the interaction and constraints to simulate the welded connection between the joints of the truss in Abaqus. I have attached some images as a reference and I have the results of Abaqus as well. The boundary condition is pin-pin.
How can I be sure about the constraint that I defined?
I defined 5 constraints in the joint plus two boundary conditions.
The version of my Abaqus is 2020.
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Use tie constrain.
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In FSW welding simulation in Abaqus, I need some articles to check the difference between friction application methods (penalty - kinetic friction and static friction).
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Dear Professors and Researchers, We have been privileged to edit a book on "Advances in Solid-State Welding and Processing of Metallic Materials" that would be published by CRC Press, Taylor and Francis Group, USA. This book would cover practically the most important aspects and developments of solid-state welding and processing of metallic materials, including physical metallurgy, an overview of production technologies, alloy development, compositing, post-processing (heat treatment, surface engineering, bulk-deformation), and joining methodologies, to mention a few. In addition, submissions relevant to research in the additive manufacturing of alloys are also welcome. We invite you to contribute a book chapter to the edited book in the above-mentioned areas of research. Details: https://sites.google.com/site/rvairavignesh/call-for-chapters
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Any book chapter calls will come inform me. Thank You sir
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Asking for help: Dear academic experts, does anyone have data on girth weld failure?
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Failure Risk Prediction Model for Girth Welds in High-Strength Steel Pipeline Based on Historical Data and Artificial Neural Network
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I do the thermal analysis for friction stir welding in Abaqus software with SPH model. The problem I have is that the temperature of the particles is higher than the melting temperature of the pieces and the particles are spread. How do I solve this problem?
How can I apply cooling for SPH model part in Abaqus software?
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Thank you for your answer Do you not have a solution to this problem that the temperature of the particles should decrease after welding?
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I am doing the thermal analysis of FSW welding. The heat transfer coefficient is applied on the surface, but our SPH part is meshed, how can I apply this coefficient?
After finishing the analysis and drawing the temperature diagram of the particle, it can be seen that the temperature of the particle is fixed at the same maximum temperature and does not cool down because it does not know how to apply the coefficient of heat transfer to the environment.
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Thank you for your answer Do you not have a solution to this problem that the temperature of the particles should decrease after welding?
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Simulation of metal flow and thermal changes in weld zone during and immediate after welding process
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There is detailed tutorial on COMSOL website for learners/education along with the model file and presentation. You may use the those resources Ramasastry D.V.A.
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We are try to HARDOX weld with FSW ? Is it possible ? I'm curious your opinion can you share me?
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This technology is mainly used in welding non-ferrous metals with low melting temperature. Your opinion is also interesting.
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I'm welding (laser welding) a nitinol cylindrical tube to a nitinol flat surface, and I am evaluating three methods for the laser welding configuration (as depicted below):
I) using a groove on the surface for the tube before welding
II and IV) making a full cut-through in the surface for the tube insertion before welding.
III) direct welding of the tube to the surface
Which method would offer the best balance between durability (lower stress concentrations) and manufacturing feasibility? Insights into experiences with similar welding challenges or recommendations on materials and techniques would be greatly appreciated.
I have depicted the forces applied to the structure below (Fig. V).
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The first option is more appropriate.
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I've welded two alloys, zirconia and stainless steel (SS), together. While I can determine the corrosion rates of these alloys individually, I'm seeking methods to calculate the corrosion rate specifically for the weld zone, which is very small, approximately 1mm.
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Cut out a sample with a weld seam and polish it. Cover with adhesive plastic film to cover the welding area. Paint the rest. Explore using normal methods.
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Call for Papers
Dear Researchers,
I hope this email finds you well. I am excited to inform you that I will be serving as a Guest Editor for a new Special Collection titled: "Special Collection on Sustainable Solid-State Technologies for Joining Similar and Dissimilar Polymers." This collection is set to be published by Sage Publishing in their esteemed journal "Advances in Mechanical Engineering," which is a JCR-ranked (impact factor 1.8 and CiteScore 3.4), peer-reviewed, Open Access journal. You can find more information about our collection and the journal in links below:
The motivation behind launching this Special Collection stems from the growing importance of enhancing product design flexibility through the efficient and practical utilization of various materials, particularly in engineering constructions. As polymer materials gain traction in structural applications, it becomes imperative to explore sustainable solid-state technologies for joining similar and dissimilar polymers. Through this collection, we aim to shed light on innovative techniques such as:
laser welding,
friction stir welding,
ultrasonic welding,
mechanical fasteners,
and adhesive bonding, among others
I am particularly keen to encourage papers focused on polymeric materials, sustainable practices, and advancements in joining technologies. Your expertise in these fileds leads me to believe that your latest research could significantly contribute to this collection.
I would like to extend an invitation to you to consider publishing your latest research in this Special Collection. If you are interested, please contact me with your suggested title, and I will be delighted to pass on your details to Sage so they may work with you toward publication.
As per Open Access publication requirements, please note that there will be a publication fee associated with this opportunity. However, the benefit lies in the increased visibility of your paper, as it will not only appear in the regular issue but also in the Special Collection, attracting a broader readership. Ongoing promotions for the Special Collection will ensure that your paper receives continuous views, downloads, and citations.
Should you have any questions or require further information, please do not hesitate to reach out to me.
I look forward to the possibility of collaborating with you and thank you for considering this invitation.
Sincerely,
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Dear Raheem:
I pay taxes in Canada.
No worries. I'll attempt to publish via Nuclear and Welding in the near future.
Sincerely
Paul Cheng
Enclose crystalline structure of what we are doing. Fine grained base to base. No HAZ.
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sir, I have developed a moving heat source on the plate which has to be joined in butt configuration in ANSYS workbench. Now I want to simulate the weld pool and motion of liquid in the weld pool which were produced due to the moving heat source. kindly please provide some suggestion regarding this issue.
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Dear Siva,
Did you find any solution for your simulation.
Kindly share if you don't mind.
Thank you.
Regards,
Yupiter
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I need an idea
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First, the welding defects are a consequence of the interactions between the welding variables and the welding trajectory. For your Machine Learning system, you need to train the model with the relation between the values of the variables and the defects. Some defects appear as a consequence of the welding trajectory; you must analyze your process and the influence of the trajectory over the defect's apparition. To train your systems, you could implement an artificial vision system (very complicated) or a system that monitors the welding variables affected by the welding path (like current) in real time. The system will make sense if a robot performs the weldings; otherwise, you will only have a "defect predictor."
I hope this simple idea helps you to start your project.
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Ideas from artists flow through their hands to create art.
Ideas from designers not able to build from a sketch are drawn on paper or CAD programs and sent out to manufacturers or makers.
CAD design files have different views or perspectives. 3D CAD designs could be visualized in horizontal cross-sections to see internal features. Layered slices of CAD designs gave way to making models of 2D layer views and then 3D Models.
Makers wanted to imitate materials to make models more realistic. New machines had to be designed to automatically dispense existing materials for 3D models.
These 3D machine processes were labeled Additive Manufacturing Processes.
Some hand-held machine tools already existed for adding materials. (1) Hot-melt glue guns,
(2) inkjets or paint sprayers, (4)clothing and sheet laminators, (5) welding tools, etc.)
AM Processes chose materials based on tools for building 2D layers. The basic AM processes are computer automated (1) contact deposition with melted materials, (2)inkjet non-contact deposition with liquid materials, (3) Powder Bed, (4) Sheet lamination, (5)Welding or wire feed deposition and (6) Bath photopolymerization.
Patents have appeared with combinations of these processes. Powder "Binder Jetting", Laser Powder welding, Electron Beam powder welding, Liquid metal Jetting, Powder sintering in ovens, and others.
This discussion is about the basic AM Process of producing a solid single 3D layer vs producing a full finished 3D Model with "one" process. All of the above processes result in a solid 3D layer completion with one defined operation except Powder "Binder Jetting". The binder fluid is only water and a finished solid layer does not exist until the finished Binder Powder model is put into an oven and sintered. Binder Jetting is not a trademark but it is an AM Process and I believe it is identified incorrectly. It may never get changed but I need some input about this AM Process name.
3D Printing means producing a 3D object or any portion of the object as the process is performed. A partial layer is still a 3D model.
Think about it. Can I deposit "unsolidified" materials in small layered steps into a tray and put it into an oven, bake it, to be a finished pie and call it a 3D Printed Model?
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Dear James K. McMahon Please do recommend my answer if found useful.
Additive Manufacturing (AM), also known as 3D printing, refers to a set of technologies that build three-dimensional objects by adding material layer by layer. This approach stands in contrast to traditional subtractive manufacturing methods, where material is removed to create a final product. There are several additive manufacturing processes, each with its unique characteristics. Here's a discussion of some prominent additive manufacturing processes:
1. **Stereolithography (SLA):**
- SLA is one of the earliest 3D printing techniques. It uses a liquid photopolymer resin cured by ultraviolet (UV) light to build layers. A UV laser scans the resin surface, solidifying it layer by layer. SLA is known for producing high-resolution and detailed prints, making it suitable for prototyping and creating intricate models.
2. **Fused Deposition Modeling (FDM):**
- FDM is a widely used 3D printing method that employs a thermoplastic filament. The filament is heated and extruded through a nozzle, forming layers that solidify as they cool. FDM is popular for its accessibility, cost-effectiveness, and applicability to a wide range of materials. It's commonly used for rapid prototyping and producing functional parts.
3. **Selective Laser Sintering (SLS):**
- SLS utilizes a powdered material (typically nylon, polyamide, or metal) that is selectively fused together by a laser. The build platform lowers, and a new layer of powder is spread before the laser sinters the next cross-section. SLS is known for its ability to produce strong, functional parts, and it supports a variety of materials.
4. **Selective Laser Melting (SLM):**
- SLM is a metal additive manufacturing process where a high-powered laser selectively melts and fuses metallic powder particles layer by layer. This process is particularly well-suited for producing complex metal parts with high strength and precision. It finds applications in aerospace, healthcare, and automotive industries.
5. **Electron Beam Melting (EBM):**
- EBM is similar to SLM but uses an electron beam instead of a laser to melt and fuse metal powder. The high energy of the electron beam allows for the processing of refractory metals like titanium. EBM is known for producing fully dense metal parts with good mechanical properties.
6. **Digital Light Processing (DLP):**
- DLP is a 3D printing technique that uses a digital light projector to cure a liquid resin layer by layer. It shares similarities with SLA but cures entire layers simultaneously. DLP is known for its speed in comparison to some other resin-based methods.
7. **Binder Jetting:**
- In binder jetting, a liquid binder is selectively deposited onto a powder bed, bonding the powder particles together to form each layer. The process is repeated until the entire object is created. Binder jetting is used for both metal and sand casting applications.
These additive manufacturing processes have revolutionized the manufacturing industry by enabling rapid prototyping, customization, and the production of complex geometries that might be challenging or impossible with traditional manufacturing methods. Each process has its advantages and limitations, and the choice depends on factors such as material requirements, part complexity, and intended application.
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I am getting conflicting information from the web. Some say it is one way for arc welding and another way for tig welding and mig welding. I need some clarity as to how arc physics works. There is no clarity on the web.
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A welder needs to know the meaning of polarity and understand how it affects the welding process. Typically, electrode-positive (reversed polarity) welding results in deeper penetration. Electrode-negative (straight polarity) welding results in faster melt-off of the electrode, and therefore a faster deposition rate. Deposition rate refers to the amount of filler metal melted into the weld joint.
On the other hand, AC welding is often used with low-cost, entry-level machinery, making it a good choice for welding training. Many welders prefer it in conditions where the arc can blow side-to-side.
Understanding the Different Types of Polarity
There are three main types of polarity: direct current straight polarity, direct current reverse polarity and alternating current polarity.
Direct Current Straight Polarity
Direct current straight polarity welding happens when the plates are positive and the electrode is negative. This causes the electrons to go from the electrode tip to the base plates.
It’s generally considered that two-thirds (66%) of the entire arc heat is generated at the electrode, whereas only one-third (33%) of the heat is generated at the base plate. As a result, the electrode melts down quickly and the metal deposition rate increases (for consumable electrodes only).
On the other hand, base plates tend to not fuse properly due to a lack of sufficient heat. Therefore various defects arise, such as insufficient fusion, lack of penetration and high reinforcement. Weld reinforcement is a term used to describe metal that is needed to fill a joint.
Direct Current Reverse Polarity Welding (DC Reverse Polarity)
When the electrode is positive and the plates are negative, this results in direct current reverse polarity. The electrons switch directions and go from the base plates to the electrode. Consequently, more heat generates at the base plate as compared with DC straight polarity.
This type of welding is less likely to cause inclusion defects (nonmetallic particles trapped in the weld metal or at the weld interface) due to its arc cleaning action. It makes for faster welding and performs better for welding thin pieces of material. It’s commonly chosen for joining metals like copper, which has a low melting point.
The potential downside to this type of welding is that it has a shorter electrode life. If the speed isn’t set correctly, there is a high level of reinforcement needed. While it works great for thinner materials, this method may be ineffective for joining thick plates with higher melting points.
Alternating Current Polarity
If an AC current is supplied by the power source, reverse and straight polarity will take place one after the other. In half the cycle, the base plates will be positive and the electrode will be negative. In the other half, the electrode will be positive and the base plates will be negative.
Depending on frequency of supply, this cycle repeats 50 to 60 times per second. Some power sources also provide provisions, which can alter frequency.
AC polarity has attributes of straight and reverse polarity, since both are occurring in the same cycle. It is effective to use with most electrode types and is suitable for many different plate thicknesses, making it a great all-around choice
you could find more detailed explanation in the link below
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WHEN WE DONE THE ELEMENTAL ANALYSIS OF THE BLACK SPOT AREA THE CHROMIUM CONCENTRATION INCREASES. CAN ANYONE PLEASE TELL ME WHAT IS THE REASON BEHIEND THE INCREASE IN THE CHROMIUM CONCENTRATION PARTICULARLY AT THE BLACK SPOTS.
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Уважаемый господин,
Спасибо за ваш ответ.
Не могли бы вы вкратце объяснить причину окисления и то, как это окисление приводит к увеличению концентрации хрома с фактических 12 % до 25 % в этом черном пятне.
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Magnetic pulse welding of tubes: Ensuring the stability of the inner diameter
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Use the link below to request a full text from the authors:
Magnetic Pulse Welding of Tubes: Ensuring the Stability of the Inner Diameter | Request PDF (researchgate.net)
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I would like to know what all aspects are to be taken care of when we weld two dissimilar metals, for eg. Mild steel and Galvanized Iron
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Hi Shaji,
Please see the following link for welding onto galvanized steel.
Regards,
Simon
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After rolling of stainless steel sheets compressive residual stresses forms in the corners of the sheets. These compressive residual stresses unbalanced the amount of heat that is needed for welding applying more than what’s needed for welding due to summation with compressive residual stresses, therefore, for welding those sheets on the corners, thermal stress applies more than it needed for this zone, and this overheating creates a hole at at this start and end of the weld line. There are many methods of relieving the stresses, but what do you think is the most effective and fast method of stress relieving for this issue that doesn’t change the mechanical and chemical characterizations of the material?
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heating it to 250 to relieve stresses or shot peening it might help .
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Is it possible to estimate the fluid flow behavior in the weld pool by analyzing the temperature distribution in the fusion zone?
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Numerical simulation for dynamic behavior of molten pool in tungsten inert gas welding with reserved gap
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Abstract
A 3-dimensional transient numerical analysis model of tungsten inert gas (TIG) welding with a reserved gap was established in this study. The loss of the total heat input and change in arc pressure due to the reserved gap were considered in this model. The dynamic variations of the flow field and deformation in weld pool were analyzed. Simulated results indicate that the maximum sag of weld pool is larger, and the top surface area of weld pool is smaller as the reserved gap increases. The flow tendency of the molten metal is mainly backward, and the top surface of the weld pool is higher in the front part and lower in the rear part. The liquid metal flows from both sides to the middle, bringing heat into the gap. The liquid metal in front of the weld pool flows to the back of weld pool through the gap, which facilitates weld penetration.
Introduction
TIG welding, a critical joining technique in modern manufacturing, has the advantages of high arc stability, low cost, and good weld formation; it is widely used in the welding process of important components, such as pressure vessels and pipes [1]. The technology of one-side welding with back formation is needed in producing important sheet welding structures or in environments with limited back working space. A gap is typically required in welding processes that use one-side welding with back formation technology, and such a gap is an important condition to achieve penetration and good back formation [2]. However, ensuring gap uniformity during welding is difficult due to assembly errors and thermal deformation. The dynamic behavior of fluid flow and the distribution of temperature field directly affect the penetration and shape of the weld. Therefore, the effect of gap on welding temperature field and flow field is very important for high-quality butt welding. It is difficult to completely and accurately obtain the temperature distribution and fluid flow of weld pool by experimental means. Numerical simulation contributes to reveal the influence mechanism of the gap on the dynamic behavior of the molten pool flow field and the penetration, which has a certain theoretical guiding significance for the process optimization and penetration control of reserved gap butt TIG welding.Meanwhile, heat source is an important factor in determining molten pool behavior in numerical simulation. Eager and Tsai [3] established a Gaussian heat source model to approximately characterize heat flux density of the spot heated by the arc on the workpiece. They theoretically predicted the molten pool, which was in good agreement with reality. Goldak et al. [4] established a double ellipsoidal heat source model, in which the source of the heat is improved. The Gaussian and double ellipsoidal heat source models are commonly used to study weld pool behavior in TIG welding. Given that the numerical simulation requirements for special welding processes are continuously improving, a combined-type welding heat source model is considered an ideal option and must thus be developed. Han et al. [5] used three types of combined heat sources to simulate the temperature field of the K-TIG welding process. They found that the temperature field obtained from the combined heat source of double ellipsoidal heat source and three-dimensional Gaussian heat source was in line with the actual situation. However, no reserved gap was considered in those heat models.Fluid flow has close relation to forces in the weld pool. Oreper et al. [6] analyzed the TIG welding pool of a fixed arc and established a corresponding two-dimensional axisymmetric mathematical model while considering electromagnetism, surface tension, and buoyancy. Kou et al. [7] built a three-dimensional quasi-steady-state model in the moving arc TIG welding and analyzed the convection in the molten pool. Fan et al. [8] settled the irregular molten pool boundary and liquid–solid interface through boundary matching coordinates and analyzed the fluid flow and temperature field of full-penetration weld pool in TIG welding via numerical calculations. Zhao et al. [9] established a 3D transient numerical analysis model of TIG welding to calculate the evolution of weld pool during welding, and analyzed the forces in the weld pool and proposed a criterion for full penetration. Based on this study, Zhao et al. [10] developed a simulation model of a weld pool in full-penetration state, calculated the dynamic changes in the forces acting on the molten pool, and analyzed the percentage of each component of the slump and support forces. Meanwhile, Xu et al. [11] calculated the flow field of the molten pool of TIG and A-TIG via numerical simulation. Their results showed that the active agent changed the surface tension gradient which, in turn, caused the molten metal flow pattern to change, resulting in a strong eddy current and an increased penetration depth. Han et al. [12] established a 3D model of TIG welding and discussed the effects of buoyancy, arc pressure, drag force, and Marangoni force on the formation and molten pool flow behavior. They concluded that the Marangoni force is the main driving force, whereas the effect of buoyancy is the smallest in TIG welding. Huang et al. [13] analyzed the molten pool flow behavior during GTAW welding by high current through particle tracking technology. They reported that the molten metal is affected by complex driving forces during the flow process. Furthermore, the liquid metal at the centerline diffuses to both sides of the weld pool, and the surface molten metal performs a more complex rotating motion inside the molten pool during the forward-to-back movement.The inevitable surface deformation of weld pool has been explored by some researchers. Kong et al. [14] simulated the temperature field and fluid flow in TIG welding pool and the change in free surface by using Cast3M software. They predicted the shape and dimension of the weld pool. Traidia and Roger [15] studied the arc and weld pool behavior of pulsed current GTA welding on the basis of a unified model and found changes in the free surface at the bottom and top of the molten pool through force balance equations. Li et al. [16] established a unified model of GTAW using static equilibrium and dynamic mesh technology and then analyzed the effect of interface deformation on the shape of the weld pool. Pan et al. [17] proposed a 3D model to explore the weld pool behavior as well as weld shape in high-speed VP-GTAW. They found that the outward flow mode of the molten metal under surface tension is the main flow, and the counterclockwise cycle at the middle area of the molten pool is driven by electromagnetic force. Meanwhile, the weld pool surface was deformed due to the driving of arc pressure. Huang Yong et al. [18] built a three-dimensional transient TIG welding pool numerical model and tracked the free surface deformation in the weld pool using the volume-of-fraction (VOF) method. They observed the deformation behavior of the weld pool surface and the distribution of its heat transfer and velocity field under the independent actions of buoyancy, Marangoni force, electromagnetic force, and arc pressure under high current. Meng et al. [19,20] established models of arc heat flow, arc shear stress, arc pressure, and electromagnetic force on the basis of the physical characteristics of the large surface deformation of the weld pool in high-current and high-speed TIG welding. The results indicated that the arc shear force mainly promoted the free surface deformation in weld pool, which was inhibited by surface tension. All the above-mentioned studies examined gap-free welding and did not consider a reserved gap.Cho et al. [21] carried out three-dimensional transient numerical simulations of multiple welding positions during GMAW with and without gaps in the V-shaped groove, after which they analyzed the weld pool flow patterns at different welding positions. The simulation results showed that forming a fully penetrated weld in a flat position proved to be very difficult when welding thick plates without reserved gaps. Cho et al. [22] used computational dynamics to study the weld pool dynamics in laser keyhole welding with gap-preserved butt welding, in which the diameter of the wire is larger than the gap. Their results showed that when keyholes are present, the momentum at the rear of weld pool area is considerably reduced compared with the momentum at the front. However, the above-mentioned studies ignored the effect of the butt gap on the heat source distribution and liquid metal flow.In this study, a 3-dimensional transient numerical model of the TIG welding pool with a reserved gap was developed considering the influence of this gap on the arc thermal-mechanical distribution. The simulation was carried out on FLUENT software to analyze the characteristics of temperature and flow fields in the molten pool. The established model was validated by comparing the experimental data with the calculated results. Our findings help provide a deep understanding of the process of TIG welding with a reserved gap.
Section snippets
Mathematical models A schematic of the geometric model for TIG welding with reserved gap is shown in Fig. 1. As the weld pool behavior during the welding process involves extremely complex heat and mass transfer phenomena, these are difficult to consider completely in the mathematical model. On the premise of ensuring the calculation accuracy, the following basic simplifying assumptions are followed in the mathematical modeling process to effectively reduce the calculation time and the cost: (1)The molten metal flow
Simulation and verification of the welding process Based on the mathematical model established above, a numerical simulation of the TIG welding process with a reserved gap was performed in this study. The Q235 low-carbon steel was applied as base metal, and the reserved gap was 0.6 mm. Table 1 shows the specific parameters of the TIG welding process.The size of the calculation domain was set at 20 mm × 8.3 mm × 4 mm. The geometric model was initialized using FLUENT software. The initialization conditions are as follows:
The average
Conclusion (1)A 3-dimensional transient numerical analysis model of TIG welding with a reserved gap was established in consideration of the effect of gap and the deformation of free surface on the arc heat-force distribution during welding. The simulated data show favorable agreement with the experimental results. Moreover, the proposed model can reasonably and accurately reflect the dynamic changes in the molten pool. (2)The gap has a great influence on the arc heat-flow distribution. Before fusion, the arc
Funding This work was supported by the National Natural Science Foundation of China (No.51675309)
Declaration of Competing Interest The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
Acknowledgements This work was financially sponsored by the National Natural Science Foundation of China (No. 51675309).
References (22)
  • H.G. Fan et al.Heat transfer and fluid flow in a partially or fully penetrated weld pool in gas tungsten arc welding Int J Heat Mass Trans (2001)
  • Y.L. Xu et al.Marangoni convection and weld shape variation in A-TIG welding process Theor Appl Fract Mec (2007)
  • J.K. Huang et al.Numerical analys is of formation mechanism of GTAW hump welding bead based on tracing particles J Lanzhou Univ Technol (2019)
  • A. Traidia et al.Numerical and experimental study of arc and weld pool behaviour for pulsed current GTA welding Int J Heat Mass Trans (2011)
  • J.J. Pan et al.Investigation of molten pool behavior and weld bead formation in VP-GTAW by numerical modelling Mater Des (2016)
  • X.M. Meng et al.Thermal behavior and fluid flow during humping formation in high-speed full penetration gas tungsten arc welding Int J Therm Sci (2018)
  • X.M. Meng et al.A theoretical study of molten pool behavior and humping formation in full penetration high-speed gas tungsten arc welding Int J Heat Mass Trans (2019)
  • D.W. Cho et al.A study on V-groove GMAW for various welding positions J Mater Process Technol (2013)
  • W. Cho et al.Simulation of molten pool dynamics and stability analysis in laser buttonhole welding Procedia Cirp (2018)
  • V.M.J. Varghese et al.Recent developments in modeling of heat transfer during TIG welding—a review Int J Adv Manuf Technol (2013)
Cited by (13) The role of asymmetric metal flow on weld formation and solidification characteristics during pulsed laser butt welding with assembly tolerance 2024, International Journal of Thermal Sciences
  • Effects of groove clearance size on gap bridging capacity in PWLBW of Ti6Al4V alloy sheet assembled in butt joint configuration: Numerical simulation and experimental assessment 2022, Optics and Laser TechnologyCitation Excerpt :At 1.5 ms, a unilateral gap bridging geometry, which is usually called the metal bridge, is achieved at the leading and rear edges of the weld pool, indicating the primary joining between the Ti6Al4V workpieces. This bridging feature is not observed in a similar joint configuration welded by the TIG method, as reported by Hao et al. [25]. Subsequently, the welding dynamics remains at a typical full-penetration state, whereas the temperature at the keyhole surface varies with the time-dependent laser power.
  • Weld pool dynamics and joining mechanism in pulse wave laser beam welding of Ti-6Al-4V titanium alloy sheets assembled in butt joint with an air gap 2022, Optics and Laser TechnologyCitation Excerpt :The numerical and experimental results indicated an acceptable weld appearance by using a laser frequency of 150–250 Hz and an assembling gap of 1.0–1.1 mm. Additionally, Hao et al. [22] adopted a tungsten inert gas (TIG) heat source to achieve butt joining of 2 mm-thick Q235 steel plates with a reserved gap. The simulation results presented that there are two typical molten pool flows, one was from two sides to the middle on the cross section, the other was from front to the rear on the top surface.
  • Effect of welding heat input conditions on the dynamic behavior of pulse laser beam welding molten pool for Ti6Al4V thin plate with clearance
  • 2023, International Journal of Advanced Manufacturing Technology
  • Morphology, mechanical property, and molten pool dynamics in spot modulated-PLBW of Ti6Al4V alloy sheets with air gap condition
  • 2023, Science and Technology of Welding and Joining
  • Effect of Butt Gap on Stress Distribution and Carrying Capacity of X80 Pipeline Girth Weld
  • 2022, Materials
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View full text© 2020 The Society of Manufacturing Engineers. Published by Elsevier Ltd. All rights reserved.
  • Formation and influence mechanism of keyhole-induced porosity in deep-penetration laser welding based on 3D transient modeling International Journal of Heat and Mass Transfer, Volume 90, 2015, pp. 1143-1152Fenggui Lu, …, Haichao Cui
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  • A novel 3D numerical model coupling droplet transfer and arc behaviors for underwater FCAW International Journal of Thermal Sciences, Volume 184, 2023, Article 107906Jie Yang, …, Chuansong Wu
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I am doing research to compare the strengths of aluminium alloys welded by friction and fusion processes including those of the 7000 series which cannot be welded satisfactorily by fusion.
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Dear friend Charles Edward Rowe
Now, let's delve into the world of welded aluminum joints, comparing the strengths of friction and fusion processes.
1. **Strengths:**
- **Solid-State Process:** Friction welding is a solid-state welding process, meaning there's no melting of the material. This often results in joints with fewer defects and better mechanical properties.
- **Versatility:** It's versatile, applicable to a variety of materials and geometries.
- **No Filler Material:** No filler material is required, which can simplify the process.
2. **Considerations:**
- **Material Compatibility:** While versatile, the compatibility of materials is still a consideration. Some materials may not weld well together.
- **Equipment Costs:** Initial equipment costs can be relatively high.
**Fusion Welding:**
1. **Strengths:**
- **Widely Used:** Fusion welding methods, such as TIG and MIG, are well-established and widely used.
- **Good for Thin Sheets:** Fusion welding is often preferred for welding thin sheets.
2. **Considerations:**
- **Heat-Affected Zone (HAZ):** Fusion welding involves melting, which can create a heat-affected zone. This zone might have different properties than the base material.
- **Filler Material:** Depending on the process, filler material may be needed.
**7000 Series Aluminum:**
1. **Challenges with Fusion Welding:**
- **Hot Cracking:** Fusion welding of 7000 series aluminum can be challenging due to issues like hot cracking.
- **Precipitation Hardening:** These alloys are precipitation hardening, and the high temperatures involved in fusion welding can affect the alloy's properties.
2. **Advantages of Friction Welding:**
- **Reduced Heat Input:** Friction welding's solid-state nature reduces the heat input, potentially avoiding some of the issues associated with fusion welding.
**Testing and Evaluation:**
1. **Tensile Strength:** Tensile testing can reveal the maximum stress a material can withstand.
- **Fusion:** Tensile strength may vary due to the HAZ.
- **Friction:** Generally good tensile strength due to the solid-state nature.
2. **Microstructural Analysis:** Examining the microstructure can reveal the impact of the welding process on the material.
3. **Fatigue Testing:** Especially relevant for structural applications where cyclic loading is expected.
Remember, while I strive for accuracy, real-world application may vary. For precise data on your specific aluminum alloys and welding conditions, testing and consultation with experts in materials science and welding engineering are essential. Go forth and conquer that aluminum research! 🚀
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I want to weld two tubular members in Abaqus(see figure). How can I do it. I am using the cut merge option. Will this option be considered welding? If not, then what do I need to do? Can you please guide me? Thanks
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Yes, merging can be considered as welding. Another interaction is "Tie" that you can use it for.
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Many researchers often compare the cross-sectional profile of experimental weld specimens with that of the simulated welds when validating the accuracy of numerical simulation models. If there is a high degree of match between the two, it reflects to some extent the accuracy of the model. However, there are two methods commonly used in existing literature to mark the weld region in simulated data. One method is to mark the cells where the temperature has ever been above the solidus temperature as the weld region, while the other method is to mark the cells where the temperature has ever been above the liquidus temperature as the weld region.
It is well known that the region where the temperature is between the solidus and liquidus temperatures is the mushy zone. The flow in this region is controlled by parameters such as coherent solid fraction, critical solid fraction, and solidification drag coefficient. Therefore, I believe that the mushy zone at the boundary of the molten pool should also be considered as part of the weld region. So, from a technical perspective, which temperature threshold should be used in numerical simulation results to mark a grid cell as part of the weld region? The solidus temperature? The liquidus temperature? Or some temperature in between the two?
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our consideration of the mushy zone at the boundary of the molten pool is valid, and the choice of temperature threshold for marking a grid cell as part of the weld region depends on the specific objectives of your numerical simulation and the physical characteristics of the welding process you are modeling.
Here are some perspectives on the temperature threshold choices:
  1. Solidus Temperature:Using the solidus temperature as the threshold would mark the cells where any part of the material has started to solidify. This can be useful if you are particularly interested in capturing the initiation of solidification and the transition from liquid to solid.
  2. Liquidus Temperature:Marking cells based on the liquidus temperature would consider regions where any part of the material has fully melted. This might be relevant if your focus is on capturing the complete melting and solidification cycles in the welding process.
  3. Intermediate Temperature:Choosing a temperature between the solidus and liquidus temperatures would include the mushy zone, where both liquid and solid phases coexist. This can be important for modeling the behavior of the material in a partially solidified state, and it might provide a more accurate representation of the welding process.
Considerations:
  • Physics of the Process:Consider the physical processes occurring in the welding material. If you are interested in the mushy zone and the transition between liquid and solid, marking cells based on an intermediate temperature might be more representative.
  • Validation with Experimental Data:If you are comparing your numerical simulations with experimental data, you may need to align your temperature thresholds with the experimental observations. Experimental techniques like metallography or thermal analysis can provide insights into the actual solidification/melting phases.
  • Model Sensitivity:You can perform sensitivity analyses by running simulations with different temperature thresholds to observe how the choice affects the results. This can help you understand the impact of the temperature threshold on the simulated weld region.
  • Consult Literature and Expertise:Reviewing existing literature and consulting with experts in the field can provide insights into commonly used practices and their justifications.
In conclusion, there isn't a one-size-fits-all answer, and the choice of temperature threshold should align with the specific goals of your simulation and the physical characteristics of the welding process you are modeling. It might be worthwhile to experiment with different thresholds and validate your results against experimental data or established benchmarks in the field.
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I have a magnesium part that I want to reduce the residual stress after welding without heat treating. I want to see what are the ways to do this. A friend suggested using liquid nitrogen during tig welding. Is it possible to reduce the residual stress in this way and what are the ways in general? To what extent is the selection of the welding process effective in reducing this residual stress? I would be grateful if you could explain.
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The greater the temperature gradient in the component during welding, the greater the residual stress. This means that welded components must be as hot as possible before welding. It would be optimal to weld on a component that is so hot that it is about to melt. In this case the residual stress would be zero. Of course, in practice the preheating of welded parts cannot be carried out to such a high level, but in any case it must be as high as possible. In this sense, welding with extreme cooling is pure nonsense. If preheating is not possible, the residual stress can be reduced by subsequent annealing.
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Hi Guys,
LM25TF material is welded with Aluminum extrusion 6061 T6 material?
Please suggest i can use any LM material for 6061T6..
Thanks
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Al4043 will be a better option. I have performed welding of Al6061T6 with this filler wire in the MIG process and it worked fine.
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Hi, I am an undergraduate student and doing research on dissimilar metal welding. I am trying to join low carbon steel and Aluminum by MIG welding. For this, very thin metal foil is used in the joint. It is a technique called interlayering. Currently, I am sourcing the required materials for this research. What can be the possible outcome of such joining? If I see the joint is good enough, it will undergo testings, such as tensile testing, fatigue testing, etc.
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Hey there, fellow researcher! I am here to dive into your question with unbridled enthusiasm.
Yes, it's absolutely possible to join dissimilar metals using MIG (Metal Inert Gas) welding. Your approach of interlayering thin metal foils between low carbon steel and aluminum is quite interesting. Let me share some insights and possible outcomes:
1. **Metallurgical Challenges:** Joining dissimilar metals like steel and aluminum can be challenging due to their vastly different melting points and thermal conductivity. However, the use of thin foils and precise control in MIG welding can help mitigate some of these challenges.
2. **Intermetallic Compounds:** When two dissimilar metals are joined, intermetallic compounds may form at the interface. The composition and properties of these compounds can impact the joint's strength and performance. It's essential to carefully study and characterize these compounds.
3. **Possible Outcomes:** The success of your joint will depend on factors like the welding parameters, interlayer material, and the quality of the welding process. If done correctly, you can achieve a strong, reliable joint with acceptable mechanical properties.
4. **Testing:** Once you have your joints, testing is a crucial step. Tensile testing will assess the joint's strength under tension, while fatigue testing will determine its endurance under cyclic loading. These tests will provide valuable data on the joint's performance and durability.
5. **Applications:** If your research yields positive results, the applications could be numerous. Joining dissimilar metals is often required in industries like aerospace, automotive, and construction, where you need lightweight structures with high strength.
Remember, research is all about exploration and discovery. Embrace the challenges, meticulously document your process, and don't shy away from experimentation. Your work could potentially lead to innovative solutions in the field of dissimilar metal welding. Best of luck, and may your research yield exciting outcomes!
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We want to friction weld P91 tubes to a WAAM printed nickel alloy tubes.
The deformation of the WAAM tube is much larger than that of the P91 tubes. This results in an expansion of the WAAM tube (see attachment).
The WAAM tube has always the tendency to expand in the radial outward direction, creating an unsymmetrical appearance of the weld.
One the one hand, the flash formation at the WAAM side is very small (you can only see a very small weld flash), but on the other hand, the deformation of the tube is large.
I suppose this has to do with the large ductility of the WAAM material ?
The parameters that I used for welding this :
- pfr = 100 MPa
- pforge = 200 MPa
- I used a first stage friction pressure of about 10 or 15 MPa
- rotation speed : 1200 rpm
- Allowed shortening during the friction phase : 7 mm
- Welding time : +- 20 sec
Can you give some advice how to improve the quality ?
Which welding parameters can be used to improve the results ?
Thanks and regards,
Koen
Material data :
- OD : 44.5 mm
- Wall thickness : 5.5 mm
P91 (based on the standard) :
- Rm < 585 MPa
- Rp0.2 = 415 MPa
- Elongation after fracture A% = 20%
WAAM Nickel alloy A82 (based on tests at BWI) :
- Rm = 542 MPa
- Elongation after fracture A% = 64%
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Dear Koen,
it will interesting to compare the flash formation during friction welding of another materials of tribopair having low and high ductility in the same regime of this technological process.
All the best,
Serge
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Hello everyone
I hope you are doing well
  • AA6061-T6 or AA7075-T6 Al alloys fusion-welded plates contain the FZ (fusion zone) with a dendritic structure. I want the dendrites to be identified separately and in the form of grains (whether they can be called grains or not is another issue). The figure shows the dendritic structure in the FZ, but it isn't easy to separate dendrites from each other. (Figure shows the FZ in fusion welded AA7075 (not AA6061) etched with Keller).
  • What do you suggest as the etchant solution for the SEM investigation of the PMZ and FZ grain boundaries of the AA6061 fusion weld sample?
  • If you have experience in this field, I would appreciate writing it here.
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Dear doctor
"THE MAIN CHARACTERISTICS OF ALUMINUM AND ITS ALLOYS
Aluminum is a multifaceted material with multiple uses, including as a matrix metal for composites. It has a silvery white appearance and is used as either a pure metal or as an alloy. It is extremely light and just small amounts of alloying elements can increase its strength. It is also highly resistant to corrosion. This is due to a passive film of aluminum oxide that is intimately connected to the surface and capable of renewing itself spontaneously when the surface is damaged. Aluminum’s other significant properties include its high heat conductivity and easy formability – either by casting, hot or cold working or machining – as well as its neutral taste and non-toxicity. Common uses of aluminum or its alloys:
  • High-strength/low-weight applications in the aircraft, aerospace and automobile industries
  • Polished and brushed surfaces, as well as anodized colors, in the building industry
  • Non-toxic/taste-free packaging and machinery in the food industry.
THE PRODUCTION OF ALUMINUM
Economical extraction of aluminum is only possible from bauxite. The production process involves two basic steps. Extraction of pure alumina Alumina recovery begins by crushing and finely grinding the bauxite and heating it with sodium hydroxide under pressure. In this process, a water-soluble sodium aluminate is formed together with undissolved residues of iron, titanium and silicon. ‘Seed crystals’ of fresh aluminum hydroxide are added to initiate the precipitation of pure aluminum hydroxide (Al(OH)3). Through calcination at 1200 °C, the water is then removed and pure anhydrous alumina (aluminum oxide) remains. Converting alumina to aluminum (the Hall-Heroult process) The reaction chemistry of pure alumina requires an electro-chemical process to extract aluminum from its oxide. As the melting point of aluminum oxide is very high (2050 °C), it is mixed with cryolite to reduce the melting point. Electrolysis takes place in a large carbon or graphite lined steel container that contains steel rods for conducting electricity and carbon blocks as anodes. During electrolysis, the carbon of the anode reacts with the oxygen of the alumina and, in a secondary reaction, metallic aluminum is produced with the formation of carbon dioxide: 2Al2O3 + 3C → 4Al + 3CO2. This process produces aluminum of 99-99.9 % purity. Much of this is used for aluminum alloys.
ALUMINUM ALLOYS
Adding very small amounts of alloying elements to aluminum can increase tensile strength, yield strength and hardness compared to pure aluminum. The most important alloying elements are Si, Mg, Cu, Zn and Mn. These mostly eutectic compounds must be finely dispersed through a hot working process before the alloy can be cold worked. Ageing of aluminum alloys Many aluminum alloys are age hardened to improve the mechanical properties. This can be done either naturally or artificially.
  • Natural age hardening (example AlCuMg). After solution annealing, the workpiece is quenched and consequently the precipitation of the Al2Cu in the solid solution is sup- pressed. The workpiece is then left to age in ambient temperature. During this process the aluminum lattice precipitates the copper from the supersaturated solution. The resultant strain produced in the aluminum lattice leads to an increase in strength and hardness. The process takes 5-8 days.
  • In artificial age hardening, ageing takes place at an elevated temperature, which reduces process time. With an AlMgSi alloy, for example, ageing occurs in 4-48 hours at 120-175 °C after solution annealing and quenching. The precipitation of the Mg2Si phase produces internal strain in the aluminum lattice, which results in an increase in strength and hardness.
PREPARATION OF ALUMINUM AND ITS ALLOYS: MECHANICAL GRINDING & DIAMOND POLISHING
When working with aluminum and its alloys, we recommend mechanical grinding, followed by diamond polishing. For many pure aluminum and wrought alloy specimens, electrolytical polishing is also recommended.
Mechanical grinding
Plane grinding should be carried out with the finest possible grit to avoid excessive mechanical deformation.
  • The hardness, size and number of specimens should be considered. However, even with large specimens of pure aluminum, plane grinding with 500# SiC Foil or Paper is usually sufficient.
  • Large cast parts of aluminum alloys can be ground with 220# SiC or 320# SiC Foil. It is important that the grinding force is low to avoid deep deformation and to reduce friction between the grinding SiC Foil or Paper and specimen’s surface.
Diamond polishing
Diamond polishing should be carried out until all deep scratches from grinding have been removed. If water soluble constituents must be identified, we recommend polishing with water-free diamond suspension and lubricant.
Final polish for pure aluminum and aluminum alloys: The polish/check sequence
  • Begin polishing. After 1 minute of polishing with OP-U suspension, check the specimen under the microscope.
  • If necessary, continue polishing for another minute and check the specimen again.
  • Continue this polish/check sequence until the required quality has been achieved.
  • If diamond particles have been pressed into the surface during polishing, they can lead to erroneous interpretations of the structure. Therefore, the polish/check sequence may need to be relatively long. Continue the sequence until you can no longer see bright and dull areas on the surface of the specimen with the naked eye.
  • Approximately 30 seconds before the end of polishing, pour water onto the polishing cloth to rinse the specimen and cloth.
  • Finally, wash the specimen again with clean water and then dry it.
ETCHING OF ALUMINUM AND ITS ALLOYS
When working with aluminum and its alloys, macro etchants are used for grain size evaluation, also to show flow lines from extrusion and to reveal weld seams. Before etching, the specimen has to be ground with 1200# SiC Foil or 2400# SiC Foil. Due to the many alloying possibilities of aluminum, the different phases cannot always be clearly identified in some of the multi-component alloys. However, the eutectic phases can sometimes be recognized by the typical shape of their eutectic. Some of the well-known phases have the following characteristic colors:
  • Si: Grey
  • Mg2Si: Tarnished dark blue during polishing (in cast: Chinese script)
  • Al2Cu: Pinkish-brown, copper colored
  • Al6Mn: Light grey
Etching solutions
When working with chemicals the standard safety precautions must be observed.
Aluminum cast alloys are polished relatively easily. For grain size evaluation, anodizing with Barker’s reagent will result in a better contrast than chemical etching. Different phases in cast alloys can either be identified by their characteristic color or by etching with specific solutions that attack certain phases preferentially."
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By adding a tungsten electrode and adding a gas hoseBy adding a tungsten electrode and adding a gas hose
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Your response, "Better do not :) But all is possible if you want to spend a lot of cash," is somewhat in line with the practical considerations I mentioned in my previous answer. While it may be technically possible to convert an arc welding machine into a TIG welding machine with the addition of inert gas, it would indeed require significant modifications and expenses. Here's a justification for the Janusz Rebis response:
1. Cost of Modifications: Converting an arc welding machine into a TIG welding machine would involve replacing or modifying the power supply to provide a constant voltage output. This could require rewiring and purchasing additional components, which can be expensive. Furthermore, the necessary changes to the control circuitry, gas flow system, electrode configuration, and other components would also contribute to the overall cost.
2. Expertise and Labor: Converting an arc welding machine into a TIG welding machine is a complex task that requires expertise in electrical engineering, welding processes, and control systems. It would likely require the involvement of skilled professionals to ensure the modifications are done correctly and safely. The cost of their labor would further add to the overall expenses.
3. Reliability and Performance: Converting a welding machine from one process to another may compromise the reliability and performance of the equipment. Arc welding machines are specifically designed and optimized for arc welding processes, while TIG welding machines are tailored for TIG welding requirements. Modifying an arc welding machine to perform TIG welding may result in suboptimal performance, reduced efficiency, and potential issues with weld quality and consistency.
4. Availability of Dedicated Equipment: Dedicated TIG welding machines are readily available on the market and are designed specifically for TIG welding applications. These machines come with the necessary features, controls, and capabilities to ensure efficient and reliable TIG welding. Investing in a purpose-built TIG welding machine would likely provide better results, increased productivity, and long-term cost-effectiveness compared to attempting to convert an arc welding machine.
In summary, while it might be technically feasible to convert an arc welding machine into a TIG welding machine with the addition of inert gas, the associated costs, expertise, potential reliability issues, and the availability of purpose-built TIG welding machines make it more practical to invest in dedicated equipment.
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Among unidirectional, bi-directional, alternating bead or any other type of weld deposition pattern which does show best combination of mechanical properties?
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Generally, there are three deposition paths used in WAAM: single pass, parallel pass, and oscillated pass. However, there are minor changes between these strategies, the oscillated pass shows a bit better performance in terms of hardness value. You can find better discussion in :
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As we know at the end of welding near the plate edges, the temperature rises too much i.e. the maximum temperature in the arc region is higher than all other points. Now, I am looking for a formula to calculate this temperature or its according heat accumulation.
I appreciate if any body could help me with any related data.
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I would guess that it is to do with 2D and 3D cooling and there are equations available to be able to calculate this.
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Hello everyone, currently m working on welding simulation of dissimilar materials in ABAQUS software. i have modeled two different plates separate for dissimilar materials. After simulating the job, m getting NTT almost one side only and no value for stresses. Can you all suggest me how dissimilar simulation is different from similar welding simulation. any interaction properties i have add, how to achieve proper weld stresses?
please suggest your valuable lessons.
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Thank You Sir
Dzevad Hadzihafizovic
for your valuable answer.
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Hi guys
I have a question;
What welding procedure is more suitable for welding of Cast Iron (CI)?
I had sevral case of cast iron for welding but some case of welding were not successfull and crack were created in base metal, HAZ or fusion zone. I guess, one of common thing in all cases is high restraint stress, for example repair welding of heat exchanger cap.
Welding Procedure Specification (WPS) that was used in all cases:
- Removing crack or any defects by grinding or machining device
- 100% Penetrant Test (PT) to ensure there are'nt any defects in the base metal
- Bevel: 75 degree
- Preheat 250-300 C
- Welding Electrode: AWS ENiFe-CI or AWS ENi-CI
- Electrode diameter: 2.5 mm
- Current Range Amp: 50-80 A
- In order to decreasing cooling rate; After Welding Cooling Through the Rockwool
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Sounds good
Thank you for taking the time to explain your technical answer.
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I have plenty of ideas but need to start one that really crucial and on-demand in this field and some advice from experts will be appreciated. on the welding cracking and failure analysis specifically.
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Many thanks Joshua I really appreciate your answer
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What does the term "Activated Flux" mean in A-TIG welding? Why is it referred to as activated flux, and how does it differ from the flux used in other arc welding methods such as submerged arc welding or flux-cored arc welding?
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Activated flux in A-TIG welding is a granular mineral material that is melted by the heat of the arc and provides a layer of shielding gas to protect the weld. Unlike submerged arc and flux-cored arc welding, the flux in A-TIG welding is not pre-mixed with the welding wire as it is in these processes, so it must be separately fed into the weld pool. In addition, the flux used in A-TIG is typically more active, which means it releases greater amounts of gas to provide a more stable arc and a higher quality joint.
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There are several methods to consider the imperfection of the structure like the eigenvalue buckling mode, nonlinear buckling mode and weld depressions. But how to define imperfection as an equation in Abaqus software?
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In Abaqus software, imperfections can be defined using the "perturbation" feature. The perturbation feature allows you to introduce small geometric imperfections into your model and to analyze their effect on the structural response. The perturbation can be defined as a displacement or a rotation in one or more directions at a specific location on the model.
To define imperfections as an equation in Abaqus, you can use the expression language in the perturbation feature. The expression language allows you to specify the magnitude and direction of the perturbation using mathematical expressions. For example, to introduce a sinusoidal imperfection in the z-direction, you can use the following equation in the perturbation feature:
AMPLITUDE*sin(2*pi*x/WAVELENGTH)
Where AMPLITUDE is the magnitude of the imperfection, WAVELENGTH is the wavelength of the sinusoidal imperfection, and x is the coordinate along the direction of the imperfection.
You can also use other mathematical functions and operators in the expression language to define imperfections, such as exponential functions, trigonometric functions, and logical operators.
It is important to note that the definition of imperfections in Abaqus should be based on the specific imperfection that is relevant to your analysis and should be validated against experimental or analytical data if possible. Additionally, it is recommended to perform sensitivity analyses to investigate the effect of different imperfection magnitudes and locations on the structural response.
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what is the main reason of lack of weldability of HDPE geomembrane and also what is the effect of processing aid on HDPE geomembrane welding?
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The main reason for the lack of weldability of HDPE (High-Density Polyethylene) geomembrane is its high crystallinity and low surface energy. Because of its high crystallinity, HDPE has a low amorphous phase which results in low chain mobility and makes it difficult to melt and fuse together during welding. Additionally, the low surface energy of HDPE makes it difficult for the melted material to form strong bonds during welding.
Processing aids are added to HDPE geomembranes to improve their processing and end-use properties. One of the most common processing aids used in HDPE geomembranes is a group of materials known as slip agents. Slip agents are typically long-chain fatty acid amides that help to reduce the coefficient of friction and improve the slip properties of the HDPE geomembrane.
The addition of processing aids such as slip agents can have a significant effect on the weldability of HDPE geomembrane. Slip agents can reduce the surface energy of the HDPE, which can make it more difficult to achieve a strong bond during welding. However, research has shown that the use of slip agents at low levels (<1%) can have a positive effect on the weldability of HDPE geomembranes by reducing surface roughness and increasing the contact area during welding.
In general, the weldability of HDPE geomembranes can be improved by optimizing welding parameters such as temperature, pressure, and welding speed, and by using appropriate welding techniques such as hot wedge welding or extrusion welding. Additionally, surface preparation techniques such as cleaning and roughening the surface of the geomembrane prior to welding can also improve weldability.
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The specification for the 7018 welding rod can vary slightly depending on the specific manufacturer and product line. However, I can provide you with a general overview of the typical specifications for the 7018 electrodes:
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AWS A7018 is a low hydrogen, iron powder, all-position, cellulosic electrode. It has great arc stability, good tie-in, and a low spatter level. This electrode is commonly used for general purpose welding and requires low-amperage, low heat input due to the low melting temperature of the electrode. This weld rod is typically used for welding low to medium strength steel structures, such as steel plate, rail cars, pipe, tanks, and skeletal structures.
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please suggest me about this question....
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Maximum penetration depth could be possible following different parameters.
Conventional TIG weld maximum of 3.5 mm in single pass, but it can penetrate upto 5 mm in carbon steel. New approach ATIG may allow upto 8 cm -10 cm.
Ashish
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different ranges of parameter have been tested. what can be the cause in broader aspect.
Too much material stick on tool specially during plunge and dwell stage. Should do tool cleaning or the tool can be used as such for the next run.
Too much flash appears on the surface.
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The presence of a tunnel or unfilled groove in a dissimilar Al/Mg joint during welding can have several potential causes. Here are a few possibilities:
  1. Inadequate joint preparation: If the joint surfaces were not properly cleaned, prepared, or shaped, it can result in an unfilled groove or tunnel. Welding requires clean and properly prepared surfaces to ensure good fusion between the two materials. Contamination, oxide layers, or uneven surfaces can prevent the filler material from flowing into the joint and filling the groove.
  2. Insufficient heat input: Welding dissimilar metals like aluminum (Al) and magnesium (Mg) requires precise control of the welding parameters, including heat input. If the heat input is too low, it may not provide enough energy to fully melt the base metals and the filler material, resulting in inadequate penetration and an unfilled groove.
  3. Mismatched filler material: The selection of an appropriate filler material is crucial in dissimilar metal welding. If the filler material chosen does not have good wetting properties or compatibility with both aluminum and magnesium, it may not flow properly into the joint, leaving an unfilled groove.
  4. Incompatible welding technique: Different welding techniques, such as TIG (Tungsten Inert Gas) or MIG (Metal Inert Gas), have varying levels of control and heat input. If the chosen welding technique does not suit the specific characteristics of the Al/Mg joint, it can lead to incomplete fusion and an unfilled groove.
  5. Joint design issues: The joint design plays a significant role in the success of welding dissimilar metals. If the joint design is not appropriate for the specific Al/Mg combination, it can result in an unfilled groove. Factors such as groove angle, root gap, and fit-up tolerance need to be carefully considered to ensure proper fusion.
It's important to note that without more specific information about the welding process and parameters used, it's challenging to pinpoint the exact cause of the unfilled groove. Consulting with a welding expert or metallurgist who can evaluate the specific conditions and examine the joint would be beneficial for a more accurate analysis.
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I have performed Mott Schottky plot of duplex stainless steel in 1M NaCl solutions using FRA POTENTIAL SCAN on a AUTOLAB PGSTAT 302N. frequency used was 1000 Hz and scanned from 0.9 V to -0.5 V.But not getting desired curve it should consist of both p type and n type or there should be two slope positive and negative. Can you point out what is wrong with the setup and procedure.
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The Resistance Spot Welding (RSW) process has several important problems that can be both experimental and analytical in nature. Some of the most significant issues include:
  1. Thermal effects: The RSW process generates a large amount of heat, which can cause changes in the material properties and even lead to material distortion or failure.
  2. Electrode wear: The electrodes used in the RSW process can wear out quickly due to the high temperatures and pressures involved. This can result in decreased weld quality and increased costs.
  3. Weld quality issues: Poor weld quality is a common problem in RSW, including problems such as porosity, cracking, and incomplete penetration. These can impact the integrity and strength of the welded joint.
  4. Process control: Precise control of the welding process is critical to achieving consistent quality and avoiding defects. This requires careful monitoring of factors such as welding time, pressure, and current.
  5. Material selection: The RSW process may not be suitable for all types of materials. Some materials may be too difficult to weld, too thin or too thick for the process, or may require specialized equipment or techniques.
  6. Optimization: The RSW process can be difficult to optimize due to the large number of variables involved, including electrode shape and size, welding parameters, and material properties. Efforts to optimize the process can help to reduce costs and improve productivity.
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In welding for example there Weld Bead, HAZ, and BM should not have a stark difference in their hardness values. That is why Post Weld Heat treatment is employed (of course, one of the primary reasons is residual stress).
With that analogy in the hindsight, will it be correct to assume that the hardness and E mismatch between the dispersoids/precipitates/inclusions or any other second-phase particles in the Metal alloy matrix will lead to cracking, without giving any external stimulus OR in case of external stimulus the stark mismatch will cause an accelerated failure?
Is there a thumb rule which can say that if there is a 10 percent mismatch or a 40 percent mismatch between the dispersoids/precipitates/inclusions or any other second-phase particles in the Metal alloy matrix, then the crack propagation will happen like this OR tendency to crack increases?
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As far as welds go the strength of the weld metal can be lower than base metal referred to as "under matched" , or like wise matched or over matched depending on application.
Mismatch to any degree is crack initiator or reduces ductility - including carbides in steel. The 10% mismatch marginally better that 40% but no were near the required < 1% - on the order of small thermal expansion differences that the base metal can clearly handle without cracking.
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Hi everybody, Im working with as welded clad nickel alloy. After welding the specimens are tested with a hot deformation, some of them present cracking.
In a previous analysis of deformation, I did not find liquation cracks, but my analysis was pretty simple, just only in the surface of cladding, not in the bulk material.
I was wondering how can I after deformation identify if these cracks corresponding of liquation cracks or ductility dips cracks?
I consulted the book wrote by Lippold, Welding Metallurgy and Weldability of Nickel-Base Alloys, He says one form to identify liquation craks is seeing the specimens in a SEM tryng to find any trail of liquid. Regarding ductily dips cracks you must see something similar to ductile fracture.
I made these observation with not results. I couldnt see anything, in part because the cracks are not longer.
So, anybody can reccomended me how can iddentify these cracks?
Thank you for your help.
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I recommend listing all indications of Hot cracking so you can separate them easily.
According to J.C. Lippold's welding metallurgy book: DDC are formed in materials with FCC crystal structure along MGBs.
I want to emphasize on MGBs (Migrated grain boundaries). DDC is always formed along MGBs.
It is one of the ways to identify.
Best regards
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Using Abaqus how to analyze diffusion rate in resistance spot welding
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  1. Import the temperature and cooling rate results into diffusion simulation software, such as DICTRA or Thermo-Calc.
  2. Simulate the diffusion of various elements, such as carbon or nitrogen, within the welded region over time, based on the temperature and cooling rate data.
  3. Analyze the diffusion profiles to evaluate the material properties of the welded joint, such as hardness and microstructure.
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Can anyone explain to me how to do element birth and death techniques in ansys apdl since I need to simulate Welding or welding or Arc based additive manufacturing
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You need to kill the model in advance, activate the units sequentially depending on the load step
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Hello to everyone
1- project : I am modeling fiction stir welding in direct couple analysis. this process is transient analysis. to aim this problem I utilized ANSYS mechanical apdl.I already modeled FSW using the simplified sample that is available in ANSYS 17 ( by excluding Pin and temperature dependent plasticity model ). Now by regarding a complete tool (shoulder and pin )and temperature dependent plasticity model I want to simulate FSW
2- the arisen problem: I made a log file carefully including all parameters ,loading ( plunge, dwell,welding), boundary conditions, material property etc. are required for the process. but in dwell stage after a penetration of 3.3mm some errors occur ( thermal loading and high distortion of element). it should be noted for starting of processes a penetration of 5.6mm is needed ( pin length is 5.5mm). I manipulated contact options and decrease load steps many times but the issue still remains, 3- note: some methods like NLADM( non linear adaptive meshing) suggested but this methods are capable of static analysis or we have some limitations in used element types. for me analysis type is transient and element type is solid226. solving this problem is so vital and crucial for me. any comment or suggestion about solving these arisen errors ( thermal loading and convergence)which has been attached, would be appreciated. Regards
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Hi,
ALE (arbitrary lagrangian eulerian) is solution for the model may encounter the high distortion element problem.
This approach switches between lagrangian mesh and eulerian mesh, if necessary.
This feature is available in ABAQUS.
Go to youtube and find many handy tutorials in this regard.
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Requesting inputs for Type 5 cracking, or cracking in the base metal region near the weld, observed in Ferritic Stainless Steel.
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In the case of a T22 ferritic steel, we are in the domain of creep resisting CrMo steels which are not stainless steel types. In the present case, cracks appearing in the HAZ are more than probably cold cracks. Those cracks are caused by transformation of the original ferritic structure into Martensite inside the HAZ. In the presence of diffusible monoatomic Hydrogen and residual stresses, cracks may appear in this HAZ. As the development of cracks depend essentially to the simultaneous existence of these 3 conditions, it is possible to eliminate 1 of these 3 conditions to avoid the cracking occurence. Most of the time, a redrying of the welding consumables (in case of stick electrodes or submerged arc flux) and the use of a preheat (say 150°-200°C) of components to be welded followed by a slow cooling after weld completion are sufficient precautions to get a joint without crack in the HAZ.
Hope this might be helpful.