Science topic
Welding - Science topic
A forum to discuss welding processes and procedures
Questions related to Welding
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.
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.
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.
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
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.
I am not getting proper steps for rotary friction welding
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.
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/
for example, calculate the percentage of welding nugget elements AISI 304 to carbon Steel
thanks for your attention.
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.
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?
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.
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?
I am using apparent heat method for simulation
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.
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).
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.
In FSW welding simulation in Abaqus, I need some articles to check the difference between friction application methods (penalty - kinetic friction and static friction).
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
Asking for help: Dear academic experts, does anyone have data on girth weld failure?
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?
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.
Simulation of metal flow and thermal changes in weld zone during and immediate after welding process
We are try to HARDOX weld with FSW ? Is it possible ? I'm curious your opinion can you share me?
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).
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.
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,
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.
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?
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.
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.
Magnetic pulse welding of tubes: Ensuring the stability of the inner diameter
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
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?
Is it possible to estimate the fluid flow behavior in the weld pool by analyzing the temperature distribution in the fusion zone?
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.
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
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?
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.
Hi Guys,
LM25TF material is welded with Aluminum extrusion 6061 T6 material?
Please suggest i can use any LM material for 6061T6..
Thanks
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.
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%
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.
By adding a tungsten electrode and adding a gas hoseBy adding a tungsten electrode and adding a gas hose
Among unidirectional, bi-directional, alternating bead or any other type of weld deposition pattern which does show best combination of mechanical properties?
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.
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.
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
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.
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?
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?
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?
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:
please suggest me about this question....
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.
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.
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?
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.
Using Abaqus how to analyze diffusion rate in resistance spot welding
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
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
Requesting inputs for Type 5 cracking, or cracking in the base metal region near the weld, observed in Ferritic Stainless Steel.