Science topic

Heat Treatment - Science topic

Heat treating is a group of industrial and metalworking processes used to alter the physical, and sometimes chemical, properties of a material. The most common application is metallurgical. Heat treatments are also used in the manufacture of many other materials, such as glass. Heat treatment involves the use of heating or chilling, normally to extreme temperatures, to achieve a desired result such as hardening or softening of a material. Heat treatment techniques include annealing, case hardening, precipitation strengthening, tempering and quenching.
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Hello, how do I measure the time in stress relief heat treatment? I saw in articles that, for example, they took an hour, which is very difficult to get a thigh in this case. How many seconds should I take for each hour?
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Thank you for your response.
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For fully research the new topic in heat treatment technologies.
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Dear Dr. Rayuth Keat
Regarding your query I recommend for you to stand on the update solid base reference; IFHTSE 2024: Proceedings of the 29th International Federation for Heat Treatment and Surface Engineering World Congress [1]. This proceeding contains more than 50 titles In line with Heat Treating Global Market Report 2025 [2]. Best regards....
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Quenching and partitioning
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Thank you for this interested question as it is one of a nowadays topics. In Q&T treatment, greater strength, toughness and hardness properties which are important for materials used in high-wear applications may obtain. While with Q&P treatment a better combination of strength and plasticity of steels can achieve. Therefore, it is not easy to prefer one treatment over the other until the targeted properties are determined.
Your feedback is welcome
Best regards
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Hi all,
sorry for double-posting, but the "discussion topic" doesn't seem to get enough attention. We have recently started to work with Al single crystals for surface science experiments. Unfortunately, after a few cleaning cycles the crystal surface gets cloudy or "milky". Our typical cleaning cycle involves 1 kV Ar sputtering (ion current around 3-5 uA) x 30-60 min followed by annealing to 600-700 K (time varies, but typically not less than 15 min with somewhat fast ramping up and down, but no quenching). A high resolution XPS does not show any considerable amount of adsorbates or anything unusual whatsoever (some traces of oxygen which were there even for the mirror-like surface, some traces of carbon). Therefore, I suspect the crystal experienced some faceting/graining of the surface which resulted in that the surface has become mesoscopically rough. LEED spots have possibly become somewhat broader but this is really hard to estimate. Unfortunately, we had no time to perform AFM measurements on this surface. But it looks indeed as an annealing protocol is vitally important to keep the surface nice and well-defined. Therefore, I wonder if anyone else has experienced the same problem with Al (or maybe other crystals, too?) and/or knows how to overcome this issue? Maybe someone could share an annealing protocol or give a link to such a protocol if published? Tips and tricks? All meaningful opinions are welcome!
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We had a similar milky structure formation after sputter and annealing procedure of Pd(001) cleaning. The surface had a spiral texture as well. We heated this sample to 1200 degrees Celcius for 10 minutes by slowly raising the temperature all the while observing the sample, and noticed that at around 1200, the milky surface texture was gone and the smooth surface resurfaced.
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I have a sample of free nickel and high nitrogen stainless had a heat treatment till 1050 for 1 hour then water quenched I test it by magnet then I find it had attraction to what can cause that
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Thank you sir
My sample free nickel and 0.5 nitrogen attracted to magnet and I ask for what make that happen
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"TLDR: A comprehensive investigation into the structural, magnetic, and dielectric properties of Ba1−xCoxFe12O19 ferrites sheds light on their potential applications in various industries.
This study, conducted using the heat treatment method at 1100°C, reveals intriguing insights. XRD analysis confirms the formation of M-type hexaferrites alongside a BaFe2O4 phase, providing crucial crystallographic details. Moreover, VSM measurements demonstrate the tunability of magnetic properties with cobalt substitutions, while dielectric measurements uncover frequency-dependent conductivity behaviors.
These findings not only deepen our understanding of these materials but also hint at their potential in automotive, sensors, and biomedical applications. Read the full article for insights into the future of materials science:
"New study delves into the properties of Ba1−xCoxFe12O19 ferrites: structural insights, magnetic behaviour, and dielectric properties explored.
Tailoring magnetic saturation and understanding electrical conductivity opens doors for applications in automotive, sensors, and beyond.
#Research
#Engineering
#MaterialsScience
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Exploring the structural, magnetic, and dielectric properties of Ba₁₋ₓCoₓFe₁₂O₁₉ hexaferrites involves analyzing how cobalt substitution affects the crystal structure, magnetic ordering, and dielectric response. Key areas of study include:
  1. Structural Properties: X-ray diffraction (XRD) can reveal changes in lattice parameters and phase purity with varying Co concentrations.
  2. Magnetic Properties: Magnetization measurements (e.g., using a SQUID magnetometer) can show how Co affects saturation magnetization and coercivity.
  3. Dielectric Properties: Impedance spectroscopy can assess how cobalt doping influences dielectric constants and losses, potentially enhancing high-frequency performance.
These studies contribute to understanding the potential applications of hexaferrites in electronics and magnetic devices.
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I make polycrystalline diamond with tape casting followed by HPHT sintering. When i sintered the samples up till May, the sintering was good. When i sintered the samples in June and July at the same conditions, the sintering was not good. I used the same slurry making conditions, tape casting conditions, debinding conditions, heat treatment conditions, and sintering conditions.
The only changed parameter i can think of may be humidity, as humidity is very high in June, July and August in Korea.
What tests should i perform and at what stages? How to overcome this issue?
Thank you.
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Thank you so much Mr. Tobias Makuochukwu Onyia for your time and very detailed response to my query.
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I am preparing polycrystalline diamond (PCD) with tape casting. The powder is 8~12 um.
After drying of tapes, I place several tapes in Ta cup without warm-pressing. Next, debinding is carried out. There are no cracks visible with naked eye. SEM analysis shows all the organics are evaporated.
After debinding, WC-Co substrate (4 um average particle size of WC) is placed in cup over debinded tapes. Heat treatment is done in vacuum above 1000 C for surface graphitization to help in sintering.
After that, high pressure high temperature sintering is carried out. When surface is observed after polishing, there are whitish parts on the dark gray diamond surface, mostly in circles. These discolored parts are mostly near the edge of sample, and sometimes inwards too, for example, in the center of a sample. Sometimes, these discolors are distributed throughout the sample.
What may the reason of these discolors?
Additionally, mostly there are also cracks near the edge of sample. What could be the reason for these cracks?
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Thank you Mr. Vinodh Sekar for your detailed reply.
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The AlSi7Mg sample was additive manufacturing by the PBF method and heat treated 480℃-6h and 550℃-6h.
When the residual stress of the top view and the side view(Figure) was measured by XRD, the following results were obtained.
As-built
Top : 47.4 MPa
Side : 134.9 MPa
480℃-6h
Top : -33.7 MPa
Side : 2.1 MPa
550℃-6h.
Top : -38.8 MPa
Side : -36.1 MPa
So, I have some questions about the results.
1. In case as-built sample, why is there such a big difference between Top and Side?
2. In case 480℃-6h heat treatment, after heat treatment, the Top changed greatly from tension to compression stress, but why didn't the Side change like this?
3. After heat treatment, Why tensile stress change to compressive stress?
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For this and to get some feedback, kindly refer to the preprint article given at the link; http://dx.doi.org/10.13140/RG.2.2.23849.40808
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Dear ResearchGate Community,
I am currently undertaking a project focused on measuring the residual stress of different materials post-cold and heat treatments, as well as under various machining conditions with different coolant supplies. However, I find myself in need of guidance regarding the most appropriate method for conducting these measurements.
I would greatly appreciate any professional advice or recommendations you may have on this matter.
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You may get quite a good information by referring to the preprint article available at link; http://dx.doi.org/10.13140/RG.2.2.23849.40808
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We would like to inactivate lactoperoxydase without denaturating immunoglobulins in milk.
Heat treatment does successfully but denaturate proteins.
What molecule or reagent, or substance we could add to inactivate lactoperoxyadse and preserve the immunoglobulines. Thank you
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Dear Zohra, Thank you so much for your answer, should I work with the supernatant or the pellet ? what temperature ? what rpm ?
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I am preparing a research project related to materials for rocket engine nozzles. In the research I would like to use sheets of pure Mo, TZN and Mo-La. Please help me in selecting heat treatment parameters for the given materials so as to improve the mechanical properties of the materials.
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MO Alloy depends on the composition contained, several types of MO Alloy have different composition contained, then the specifications are different so the parameters depend on the MO Alloy itself.MO Alloy depends on the composition contained, several types of MO Alloy have different composition contained, then the specifications are different so the parameters depend on the MO Alloy itself.
Just like when u cook some NPI, NPI specification depend on contained.. we can check by using SEM (Scanning Electron Microscope)
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The process of heat-treating steel samples for homogenization is crucial for achieving desired material properties, such as uniformity and strength. However, determining the optimal duration of heat treatment considers various factors. Firstly, the size of the steel samples plays a significant role, as larger samples typically require more time for heat to penetrate and achieve homogenization throughout the material. Conversely, smaller samples may require shorter durations. Secondly, the method of heating employed can also impact the duration of the heat treatment. Electric furnaces, resistive heating setups, induction heating, and salt bath systems each have distinct heat transfer mechanisms and heating rates, which can affect the time required for homogenization. Understanding how these factors interact and vary across different sample sizes and heating methods is essential for efficiently and effectively conducting heat-treatment processes in steel manufacturing and research contexts.
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There are numerous standards regarding this domain and you have to highlight your selected heat treatment and the specific property that you want to obtain, in which the main factor is time for the temperature to homogenize in the bulk of the samples, however, cooling rate is also equally important if not more. Seek ASM volumes for help/further guidance.
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I want to perform an untargeted lc-ms analysis of bacterial metabolite. Generally, we break down the cell of this bacteria by dissolving the pellet with methanol and then give heat treatment for 30 minutes at 55 degrees celsius to extract carotenoid.
But as heat treatment may destroy heat-labile metabolites, that is why I want to go for probe sonication. I have taken stationary phase culture and dissolved the culture in PBS buffer. Then I have done the sonication process (40% amplitude with 30 sec on/off for 20 minutes).
PBS buffer composition (100 ml, 1X PBS, pH- 7.4)
NaCl- 0.8 gm
KCl- 0.02 gm
Na2HPO4- 0.144 gm
KH2PO4- 0.0245 gm
What procedure should I follow to break the cell so that metabolites remain intact?
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Treat cells with lysozymes at 4 oC for 12hr than optimize the optical density at 600nm of cells for better results
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After heating the Ni-based superalloy at 1200°C and cooling it very slowly in the furnace, two types of eutectic structures were observed. While in the similar sample that was cooled in air, such a structure is not observed. What could be the cause?
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A certain amount of time is necessary for the formation of different crystalline phases during cooling of the melt. The more thermodynamically stable this phase is, the less time is necessary for its crystallization. With very rapid cooling, there is not enough time for the formation of all the crystalline phases and solid material remains amorphous (metallic glasses form from metal melts). Air cooling is not the fastest way of cooling, but it is fast enough that not all possible crystalline phases can form. On the other hand, with extremely slow cooling in the oven, practically everything that can crystallize from this melt crystallizes.
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What are the benefits of Partial Solution Heat Treatments of Nickel-based Superalloys?
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Thank you Milad Foumani.
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As we are using alkali activated slag for injection, we need it with flowability for about 10 minutes. Usually these materials are known to set quickly. I am asking if there is any type of retarder working on AAS ?
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This paper will definitely help you:
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i isolated sterols from plants methanolic extract. when run by TLC , found it is not active under UV and it is sterol by doing acidic methanolic spray with heat treatment 100 c approximately and also chemical test was positive for phytosterol. I would like to know mass of the compound which GC/LC MS Technique is suitable to know mass of the compound. and how should should i know my compound was volatile or nonvolatile.
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Yes, it is better to know if the compound is volatile and thermally stable before you can run direct GC-MS . Also, run UV spectra from 200-400 nm to check if it has any absorbance in the range. If non-active you can only use HPLC with an ELSD detector to determine the purity first. There are other ways to find the structure such as NMR.
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which heat treatment is suitable for aluminium 7075 metal matrix composites.and also may i know the steps/ procedure of the heat treatment ?
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Thank you sir
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Presenting noteworthy outcomes from a recent study on X-type samarium-cadmium co-substituted hexaferrite. The compositions, denoted as Ba2-xSmxCo2CdyFe28-yO46, were meticulously prepared through a precise heat treatment process at 1340 °C. Characterization techniques, including FTIR, XRD, SEM, VSM, Mössbauer, and low-frequency dielectric measurements, were employed for thorough analysis. The XRD analysis revealed the prominent presence of X, accompanied by hematite. Magnetic properties exhibited a range of MS values from 67.01 Am2/kg to 50.43 Am2/kg, and Hc values varied from 2.95 kA/m to 6.17 kA/m. Notably, the pure sample displayed a high MS value of 67.01 Am2/kg, while compositions with x = 0.06 and y = 0.3 demonstrated a remarkably low Hc value of 2.95 kA/m. The multi-domain nature of the prepared hexaferrites was confirmed by Mr/Ms < 0.5. Hysteresis loops showcased narrow profiles, affirming their magnetically soft characteristics. Mössbauer spectra of select samples (S1, S3, and S5) revealed the presence of doublets. Significantly low values of coercivity, retentivity, and loss tangent in Sm–Cd substituted samples suggest their potential application in designing electromagnets, transformer cores, electric motors, and as viable candidates for lossless low-frequency applications.
#MaterialScience
#Research
#Hexaferrite
#MagneticProperties
#ScientificInnovation
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If you are looking for better proof or evidence of your magnetic samples, I suggest that you take first-order reversal curve (FORC) analysis. We perform this analysis and other magnetic measurements for researchers affordably. Please contact me if you need more information. Email: amirh.montazer@gmail.com
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In our research, we explored Cu-Cr co-substituted M-type barium hexaferrites synthesized through a green approach with mentha leaves extract. The hexaferrite series, BaCuxCrxFe12‐2xO19, underwent heat treatment at 1100 °C, revealing M-phase formation and a secondary BaFe2O4 phase. Raman spectroscopy confirmed successful Cu-Cr substitution, maintaining hexagonal shapes observed in FESEM images. All samples exhibited hard magnetic properties, with x = 0.2 composition showing maximum Ms of 68.99 Am2/kg and minimum Hc of 0.1 T. Cole-Cole graphs indicated peak position shifts with Cu-Cr substitutions, offering insights into grain and grain boundary roles. These findings suggest promising applications of these hexaferrites in lossless, low-frequency scenarios.
#research
#hexaferrites
#M_phase
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Good Work 👍
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Conducted an extensive study on hexaferrites, substituting Erbium into X-type Ba2Co2ErxFe28-xO46 through a precise heat treatment process. XRD analysis highlighted phase variations, showcasing distinct X, W-type, and α-Fe2O3 phases in x = 0.0 samples, while Er-substituted samples exhibited the presence of X and W phases. The room temperature Mössbauer spectra, meticulously fitted with five sextets, elucidated a variation in saturation magnetization (MS). The pinnacle magnetic properties, with MS at 52.29 Am2/kg and anisotropy field-Ha at 1370 kA/m, were observed for x = 0.12 composition. Further, a comprehensive exploration of dielectric responses, from low frequency (20 Hz–2 MHz) behaviors attributed to grain boundaries to higher frequencies associated with grain contributions, was conducted. The findings suggest potential applications in filters owing to the soft ferrite behavior and low dielectric loss tangent exhibited by the substituted compositions. This research contributes valuable insights to the field of materials science and magnetism.
The study focuses on the preparation and characterization of Erbium-substituted hexaferrites (Ba2Co2ErxFe28-xO46) using a heat treatment method. Key aspects include XRD investigation revealing phase variations, Mössbauer spectroscopy explaining saturation magnetization (MS) variation, and identification of optimal magnetic properties at x = 0.12 (MS: 52.29 Am2/kg, anisotropy field-Ha: 1370 kA/m). The research delves into dielectric responses, attributing low-frequency behavior to grain boundary contributions and high-frequency behavior to grain contributions. The findings suggest potential applications in filters due to soft ferrite behavior and a low dielectric loss tangent exhibited by the substituted compositions.
#MaterialsScience #Research #Hexaferrites #MagneticProperties #DielectricAnalysis #Innovation
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Good work 👏
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The research investigates Cu-Cr co-substituted M-type barium hexaferrites synthesized using a green approach with mentha leaves extract. The hexaferrite samples, prepared through heat treatment, were analyzed for structural, thermal, magnetic, Raman spectroscopic, and dielectric properties. XRD findings revealed M-phase formation with a secondary phase. Raman analysis confirmed successful Cu-Cr substitution, maintaining hexagonal shape seen in FESEM images. All samples exhibited hard magnetic nature, with x=0.2 composition showing maximum Ms of 68.99 Am2/kg and lowest Hc of 0.1 T. Cole-Cole graphs indicated shifts in peaks position with Cu-Cr substitutions and increasing frequency, suggesting potential for lossless, low-frequency applications.
#GreenEnergy
#Magnetism
#HexaferriteResearch
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Great work 👍
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In this study, X-type samarium-cadmium co-substituted hexaferrites with compositions Ba2-xSmxCo2CdyFe28-yO46 were synthesized via a simple heat treatment technique at 1340 °C. Characterization using FTIR, XRD, SEM, VSM, Mössbauer, and low-frequency dielectric measurements revealed the presence of the X phase along with hematite in the prepared samples. Magnetic properties exhibited variations in saturation magnetization (MS) from 67.01 Am2/kg to 50.43 Am2/kg and coercivity (Hc) from 2.95 kA/m to 6.17 kA/m, with the pure sample showing high MS (67.01 Am2/kg) and the x = 0.06, y = 0.3 composition displaying low Hc (2.95 kA/m), confirming a multi-domain nature. Hysteresis loops indicated that the samples belong to magnetically soft materials, and Mössbauer spectra displayed doublets in selected samples. The low values of coercivity, retentivity, and loss tangent in Sm–Cd substituted samples suggest their potential use in electromagnets, transformer cores, electric motors, and as candidates for lossless low-frequency applications.
#Research
#Magnetism
#Innovation
#MaterialsScience
#Technology 
#Hexaferrite
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Informative
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Lanthanum-substituted strontium cobalt hexaferrites were synthesized via heat treatment, with calcination at 950°C and 1050°C. X-ray diffraction confirmed M-type hexagonal ferrite and hematite phases. Magnetic analysis indicated increased saturation magnetization with higher lanthanum substitution, showcasing the controllable magnetic properties in the Sr-Co hexaferrite system.
#HexaferritesSynthesis
#CalcinationTemperatureEffect
#XRDAnalysis
#StructuralProperties
#MagneticProperties
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Nice work
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A series of lanthanum-substituted strontium cobalt hexaferrites were synthesized via a simple heat treatment method. X-ray diffraction revealed the presence of M-type hexagonal ferrite and hematite phases in all samples. Magnetic hysteresis loops at room temperature indicated an increase in saturation magnetization with higher lanthanum substitution. This suggests tunable magnetic properties, vital for applications like magnetic devices. The chosen calcination temperatures (950 °C and 1050 °C) and duration (3 hours) during heat treatment influence crystalline structure and magnetic behavior. Overall, the study demonstrates the controllable magnetic properties of the synthesized hexaferrites, crucial for potential technological applications.
#Hexaferrites #LanthanumSubstitution #XRDAnalysis #CrystalStructure #HeatTreatment #SaturationMagnetization
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Good 👍🏻
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In this study, we synthesized a series of Erbium-substituted X-type hexaferrites, Ba2Co2ErxFe28-xO46 (x = 0.00, 0.04, 0.08, 0.12, 0.16, and 0.20), employing a heat treatment method at 1350 °C for 6 hours. X-ray diffraction (XRD) analysis revealed the presence of X, W-type, and α-Fe2O3 phases in the x = 0.00 sample, while Er-substituted samples exhibited the presence of X and W phases. The room temperature Mössbauer spectra were fitted with five sextets, providing insights into the local magnetic environments. The observed variation in saturation magnetization (MS) finds support in Mössbauer spectroscopy, with the highest values of MS (52.29 Am2/kg) and anisotropy field (Ha) (1370 kA/m) identified in the x = 0.12 composition. Additionally, a maximum relative area (~69%) for spin-up sites (k+a+b) was also observed for x = 0.12 composition.
#materialsceince #hexaferrite #research
DOI*
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Nice
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Any Suggestion. Thank you.
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Look for this manuscript "Twinning-induced sluggish evolution of texture during recrystallization in AISI 316L stainless steel after cold rolling"
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Wood based activated charcoal powder (2 ~ 20 μm) was subjected to heat treatment at 850℃ for 4 hours under a nitrogen atmosphere. After cooling down to room temperature, remove from the furnace. After encountering air, activated carbon powder undergoes spontaneous combustion.
What is the cause of this? How can it be avoided?
P.S. I am very sure that when taking out the activated carbon from the high temperature furnace, the activated carbon has already cooled completely.
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The reason for the spontaneous combustion of activated carbon is a decrease in the activation energy of the reaction with oxygen, the replacement of nitrogen with air. To reduce spontaneous combustion, you can reduce the oxygen content in the air using a vacuum. For example, keep activated carbon in a vacuum desiccator. To increase the activation energy, it can be kept in a desiccator over calcium carbonate.
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In all research paper i found the Aluminium alloy D16AT and 2024T4 having same chemical composition . They are subjected to same heat treatment process. Are they different or same ???
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Igor Milosevic Thank you sir for your response.
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what is the formula is used for creating a anti flacking cycle
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Team can you any one suggest What is the recommended heat treatment process for Low carbon steel used for low temperature with impact property at -46 degree centigrade?
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Thank you Raj for your valuable inputs
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Hello
I electrospun PVA and then heat-treated it. Now, after the heat treatment, the fibers stick to the foil and do not separate. Do you have a suggestion for removing PVA from the foil?
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Neda Askarzadeh, I think in removing electrospun PVA from the foil, you ll damage it and probably will not be able to test. Try to heat it without foil to avoid the effects of the foil during the heating process.
PVA is water soluble try to put foil in hot water it should remove it easily.
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I am working on the regulation of pore size and volume of activated carbon.
Please recommend me some articles on regulating pore size and volume of activated carbon by CVD and heat treatment. Thank you very much
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thank you @Shandilya
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How can I calculate the time my precursors need to be in the oven for the solid state reaction?
The reaction I expect to happen is:
BaO + TiO2 ----> BaTiO3
And is with air flux.
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Thanks for the answer. With this information can I define the optimal heating rate? Since the time that I calculated with the reaction rate equation is the time that my material will be in the oven at the necessary temperature
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Please I need inputs or materials on different alpha variants that one could possibly get during heat treatment of Ti64. thank you in advance
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Dear friend Moyosore Fakoya
In SEM images of Ti-6Al-4V, the alpha phase appears with a darker color as its atomic number is lower than the beta phase, which appears brighter ( SEM images of Chips-Ti64-3TiB...). Researchers have examined the microstructure of Ti-6Al-4V using backscattered electron imaging (BEI) and found that both lamellar and bimodal microstructures were obtained after post-process heat treatment (Microstructural Modeling of the α + β Phase in Ti-6Al-4V ...).
I hope this helps! Let me know if you have any other questions.
Source:
(1) Microstructural Modeling of the α + β Phase in Ti-6Al-4V ... - Springer. https://link.springer.com/article/10.1007/s11663-019-01675-0.
(4) How to distinguish the aplha phases in SEM images of different Heat .... https://www.researchgate.net/post/How_to_distinguish_the_aplha_phases_in_SEM_images_of_different_Heat_treatment_Ti64.
(5) The influence of heat treatment on the microstructure and properties of .... https://www.sciencedirect.com/science/article/pii/S1359645418309674.
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For protein extraction i found a protocol that separate phosvitin from egg yolk using ultrafiltration trough 10 MWCO then uses the filtrate. But phosvitin molecular weight is 35 KDa. So how it is possible to collect phosvitin in the filtrate? Another protcol uses heating temperature to seperate phosvitin but i want to compare phosvitin stability before and after heat treatment. So heating during extraction is not a good option for me.
Any suggestion will be helpful.
Thanks.
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Rohit Kumar thanks for your answer but i want to compare the heat stability of the protein before and after treatment, so using the heat for extraction affect my results.
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As received sample is rolled well in 10 passes with 5% reduction in each pass while its breaking after solution heat treatment like brittle material in one or two passes.
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There could be several reasons why an aluminum alloy breaks after solution heat treatment during rolling in one or two passes, while it rolls well in the as-received condition. Here are a few possible explanations:
  1. Over-aging: If the aluminum alloy is over-aged, it can become brittle and prone to cracking. During solution heat treatment, the alloy is heated to a high temperature and then rapidly quenched to achieve a homogeneous microstructure. If the heat treatment is not properly controlled or the quench rate is too slow, the alloy may become over-aged, leading to cracking during subsequent processing.
  2. Work hardening: Rolling is a form of cold working, which can cause the aluminum alloy to become work hardened. If the alloy is already work hardened before rolling, it can become more prone to cracking. Solution heat treatment followed by rapid quenching is intended to soften the alloy, but if the quench is not effective or the cooling rate is too slow, the alloy may retain some of its work-hardened properties, making it more susceptible to cracking during subsequent processing.
  3. Surface defects: If the aluminum alloy has surface defects, such as scratches, cracks, or pits, these can act as stress concentrators during rolling, leading to cracking. Solution heat treatment may reveal or exacerbate these defects, making the alloy more prone to cracking during rolling.
  4. Improper rolling conditions: Rolling must be performed under the correct conditions, such as the right temperature, speed, and pressure. If the rolling conditions are not properly controlled, the aluminum alloy may become overheated or over-pressured, leading to cracking.
To determine the exact cause of the cracking, it would be necessary to perform a detailed analysis of the alloy and the processing conditions.
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I tried exposing it to 540C for 50h, it resulted in homogenisation, but no grain growth. I want centimeter sized grains
what should I do here?
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The heat treatment process that can be used to obtain centimeter-sized crystals in hot rolled Al 7075 is called "homogenization" or "annealing".
The homogenization process involves heating the material to a temperature of around 480°C for several hours, followed by a controlled cooling process. This process helps to eliminate any inhomogeneity in the material that may have been caused during the hot rolling process, resulting in a more uniform structure.
After homogenization, the material can be annealed by heating it to a temperature of around 400°C for several hours and then slowly cooling it down to room temperature. This annealing process helps to further refine the structure of the material, which can lead to the formation of larger crystals.
It is important to note that the specific temperature and time parameters for the homogenization and annealing processes may vary depending on the specific properties and characteristics of the Al 7075 alloy being used. Therefore, it is recommended to consult with a materials expert or manufacturer to determine the most appropriate heat treatment process for your specific application.
regards
raghd
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How does the morphology of different thickness alloy films changes upon heat treatment at the same temperature??
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After being heated to the same temperature, different alloy films of varying thickness can change in a variety of ways in terms of morphology. Changes that might occur include:
1. Grain growth-During heat treatment, the alloy film's grains may expand in size as a result of the atoms increased mobility. The texture, roughness of the surface, and mechanical characteristics of the film may alter as a result. The initial grain size, heat treatment duration, and temperature can all affect how much grain grows.
2. Surface diffusion-High temperatures can cause the atoms on the alloy film's surface to disperse and rearrange, changing the surface morphology. The surface composition and morphology may change as a result of the selective diffusion of one phase to the surface during the heat treatment, for instance, if the alloy film comprises many phases.
3. Stress relief-As a result of the deposition process, alloy films could have residual stresses. Heat treatment may result in changes to the film's morphology by relaxing the stress. For instance, when under stress, a film with a columnar grain structure can change to one with a more equiaxed grain structure.
4. Phase transformation-Heat treatment may cause a phase transformation in some alloy films, changing the shape and composition of the film. For instance, at a particular temperature, a film with a metastable phase can shift to a stable phase, resulting in modifications to the crystal structure and surface morphology.
The composition of the alloy, the deposition technique, and the heat treatment conditions are only a few of the variables that will affect how precisely the morphology of varied thickness alloy films changes when heated at the same temperature.
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I found some samples of proteins preparared for gel electrophoresis in the freezer that have already been heat treated in Laemmli + mercaptoethanol. They have been frozen for some months. Others have been kept in the fridge after treatment for a similar time.
Can these still be used for protein separation and analysis by western blots?
any advice appreciated.
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Hello Jaleel,
In my experience, samples that have been heat-treated in Laemmli buffer do not give a nice profile when they are kept at -20°C and reloaded after a few days. I have observed partially degraded proteins and smears in these conditions. When I have to reload samples at different times I keep them in Laemmli but I make aliquots and I heat only the aliquot I want to use. I don't know the reason for the discrepancies with the other answers, maybe it depends on the proteins you're looking at or maybe their samples have not been heated before conservation at -20°C. Some gel/staining systems (precast gels for instance) also make small bands and smears less visible.
To summarize, maybe you will be lucky because your proteins are sturdy and resist that treatment but be careful, maybe do a Ponceau a Coomassie staining to check the general state of your samples and take your results with a grain of salt.
Best,
Olivier
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For a sample of zeolite which has undergone heat treatments (ion exchange, impregnation) presents a drx diagram without peaks, but during the reaction gave an acceptable yield; explanations thank you.
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For appropriate answer you must define concrete type of zeolite that you use (there is more than 250 zeolite structure today), substances used for ion-exchange and impregnation, and the temperature used for heat treatment. Moreover, even amorphous alumosilicates, that can be obtained after amorhisation of zeolites under specified conditions, could be catalytically active.
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Hy everyone, i would like to know when the porous volume of a zeolite diminshes following heat treatments such as ion exchange and impregnation does this mean that we lose some of its cristallinity? thanks for answering to my question please
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Thank you Professor Ahmad Al Khraisat for answering me. I found it really explainful.
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After heat treatment of 17-4 PH stainless steel, there is a change in r-values (Plastic strain ratio) of the steel. What can be the possible reasons behind this change, as no deformation is involved in this phenomenon. May be change in microstructure, phase change, dislocation density distribution or grain orientations ?
Kindly provide your valuable suggestions.
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Geoffrey Robert Warburton Thankyou for your answer Sir.
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I am doing heat treatment of ZA27, wanted to change the quench media. Air , water and an oil.
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Hot oils are used at high temperatures and ensure that the core and surface temperature of a part don’t vary too much during quenching. This way there’s lowered risk of distortion and cracking. While the quench with hot oils takes longer, they provide a more uniform cooling through a part’s cross-section. They work great with highly-hardenable alloys.
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I want to do solution heat treatment of a specific series of aluminum alloys, so I Should follow the literature or decide according to the size of my Al alloy.
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Temperature and soaking time matters if the size ( product dimensions, especially the thickness) is too big.
A.V.Sethuraman
Foundry Consultant
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I am using a tube furnace to anneal the sample in presence of Argon. Can I do sudden cooling after the heat treatment over at such high temperature? Will it be any problem to the furnace?
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If the tube in your furnace is Al2O3 ceramic then no, but if tube is stainless steel or fused silica then yes.
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Fe with 10-12%Al forms alpha solid solution. but Al does not dissolve any Fe Why ?
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from Hume-Rothery rules of substutional solid solubility we have Relative Valence factor which says Less Valence metals dissolves less(or even zero) of High Valence metal and Vice Versa. Al is +3 while Fe is +2.
I agree with Shivkumar Khaple sir.
thanks & regards,
atomic radius of Iron and Aluminium are 0.126 nm, 0.184 nm
g.sudhakar
phd(materials engg)
hcu
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Need to know below details.
Which certification body offers NADCAP certification?
Requirements to get NADCAP?
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Hello Vignesh,
PRI (The Performance Review Institute) is the accreditation body that administers audits to the NADCAP standard. The standard covers not just equipment, but also quality systems, calibrations, pyrometry, etc. A NADCAP audit is extensive and rigorous. Depending on the maturity of your organization and quality system it can be a challenging task to pass the audit.
I'm sorry I can't offer more specific direction on how to start the certification process, it's been a number of years since I was directly involved in a NADCAP audit.
-Jason
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Is there any guidebook for their heat treatment process?
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Yes it has an annealing affect.it reduces the residual compressive stresses of cemented carbides.It will reduce the fracture toughness and flexural strength.Annealing in contrast will usually counter the strengthening effects of added reinforcements.Please do some review of annealing effects on cermets.
Depending on the annealing temperature and isothermal dwell time results can vary.
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hello everyone. In accordance with the Ti-Cu phase diagram, welding these two metals, forms brittle IMCs like Ti2Cu and TiCu. does anybody know if there is any post-heat treatment cycle to remove or at least decrease these IMCs?
thank you for your favor.
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No, heat treatment below 400°C will not affect the microstructure of the material. It only serves to reduce the residual stresses.
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Dear Sir
i want to take wear test in my polymer spcimen so i want to fabricate my conterface material medical grade 316L stainless steel. but i did not get clear idea from liteatures so kindly help me how to fabricate 316L counter face...
1.what heat treatment need
2.heat treatment temperture
3.cooling method
i hope you have positive response
(Urgent)
Best Thanks
S.Sathishkumar
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  • Tribocorrosion performance of 316L stainless steel enhanced ... https://www.sciencedirect.com › science › article › piiby X Ji · 2022 · Cited by 1 — Original Article. Tribocorrosion performance of 316L stainless steel enhanced by laser clad 2-layer coating using Fe-based amorphous powder.
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In the martensitic stainless steel solidification process, delta ferrite is the first phase nucleating from the liquid. Sometimes this phase remains in the matrix after completing solidification. In order to improve the mechanical properties of these steel, heat treatment process is necessary. In my project, I have observed a significant amount of delta ferrite in the matrix of martensitic stainless steel in the as-welded condition. After tempering (tempering temperature was below As), the amount of this phase reduced significantly. Surprisingly, despite the tempered martensite formation, hardness increased! I think the reason can be attributed to delta ferrite decomposition. I assume that delta ferrite decomposed to carbides during the first stage of tempering and then transformed into austenite at the end of heating cycle. This austenite later transformed into fresh martensite upon air cooling; as a result, the hardness increased and delta ferrite decreased. It is worthy noted that FE-SEM investigations showed the formation of fresh martensite from the bulk of delta ferrite.
Is this assumption true and does it have a chance of happening?
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I'm planning to implement controlled cooling method for forged parts instead of normalizing process. I need to know how to design metallic box and implementation method.
Kindly share your valuable feedbacks.
Regards,
Vignesh
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The exposure time in vermiculite depends on many factors: the material, the dimensions of the parts, their temperature, the number of parts in one box, etc. Usually the exposure is several hours.
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i want to use abaqus to simulate the heat treatment with a furnace. so i build the blocks and furance.i use the abaqus cavity radiation to simulate the heating processing in furance.
when i do a data check,the abaqus always prompts : "Error in job cavityradiation: The sum of 15170 viewfactor matrix rows are less than one, indicating an open cavity; however, no ambient temperature has been defined. The facets with small row sums belong to elements identified in element set ErrElemVFSmallSumStep1Inc0. If this is a closed cavity this error may indicate a need to refine your mesh. You may choose to increase the value of VTOL to allow your analysis to run without refining the mesh. However the accuracy of the results may be significantly affected so this is not recommended unless you are sure that VTOL value you set is acceptable for your model.
Job cavityradiation: Abaqus/Standard aborted due to errors."
can you tell why? and what should i do to solve the problem? thank you very much
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Check if increasing the VTOL parameter in the *RADIATION VIEW FACTOR option solves the problem. Check also if the accuracy of the results is changed.
Best.
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I am going to make thin film involving a TiO2 nanocomposite But i had some questions that a RG search couldn't help me with. I wanted to pick between tritonx-100 or PEG
1) I have no idea how much of the powder or triton will i use to make the paste, and should I use PEG or triton?
2) I can't find the recommended temperature for heat treatment after the thin film is made
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In [1], the article contains practical procedure for obtaining the function of addition different percents of PEG or triton in terms of their impacts on the TiO2 film properties. Hope it helpful to start with it.
Best regards
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I am planning to measuring residual stress using Nanoindentation.
And I need the stress-free sample for reference.
The sample that I want to measure is AlSi10Mg , makes Additive Manufacturing.
so, how to make stree-free sample?
heat treatment? , how can i decide to proper heat treatment temperature?
Electric Discharge Machining?
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It is quite hard to produce a truly stress-free sample. Stress relief annealing of AlSi10Mg is tricky as you might change the hardness of your samples, see Mertens, et al 2015 - THERMAL TREATMENTS OF AlSi10Mg PROCESSED BY LASER BEAM MELTING (Hardness was reduced by ~ 10 % due to the 250°C/2h heat treatment)
Non precipitation hardenable alloys are typically annealed at 200°C till 300°C and then slowly cooled e.g. in the furnace (GDA Merkblatt W7). Whereby, a higher temperature should be able to achieve a lover stress level. If your samples have the capability of a precipitation hardening and your residual stress is related to a fast cooling steep, "up-hill quenching" (e.g. -196°C and then heating up in a steam bath) might be suitable. (see ASM Handbook vol. 4 Heat Treatment)
The proper temperature depends on the condition (amount of Mg and Si in solution or/and the precipitations) of your samples.
Every machining (even EDM) is able to introduce residual stresses close to the surface. Therefore, you might be better of with a chemical enchant or rather electrolytic polishing before the testing and after your stress relief treatment.
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I have a question and would appreciate it very much if you could guide me.
I have started preliminary work on fabrication of nanofiltration using polysulfone as the support and the polyamide as the top layer. The polyamide layer is made by interfacial polymerization of piperazine and TMC. The SEM micrographs of the membranes clearly show the formation of the polyamide layer. However, the membrane does not show any rejections of MgSO4. I have tested different operation conditions (pressure, flow rate) and have also modified the fabrication by heat treatment and longer dipping time. However, no rejection is observed. I cannot understand what the problem is. Thank you very much.
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dear colleague :
you made an error in the quantity(amaount) only between the support and the polyamine ???? check the 2 procedures and make a comparison: 1- support larger than polyamide 2- support smaller than polyamine this is where you can understand your error.
best regards
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Why can not grain size be reduced by heat treatment in cobalt base superalloys such as FSX-414?
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Decrease in grain size by heat treatment alone is possible when the material undergoes phase transformation, such as austenite to ferrite+ pearlite as in carbon steels. Nickel base and cobalt base alloys do not undergo phase transformations (phase stability is what makes the alloys suitable for high temperature applications). Therefore, reduction in grain size is not easy by heat treatment alone unless mechanical working (such as forging, rolling etc) precedes. However, grain growth can occur during solution treatment.
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I am doing subzero heat treatment after quenching for en24 steel. And after subzero heat treatment am tempering it for 450c. So is it ok to go for 6 hours for subzero heat treatment or do we have to go for 24 hours only? 
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the grade of the steel is important in order to compromise properties.... but totally 24 hours is suitable
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While doing heat treatment to SLM parts, Do we need to perform heat treatment along with the build plate or after removing parts (using wire cut EDM) from the build plate?
My main concern is to study the effect of heat treatment on mechanical properties and residual stresses
Can anyone explain this? (It will be helpful to my work if you provide an answer with the journal also)
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I invite you to check our paper, in which we compared the effect of stress relief with parts attached to the building platform on, among others, residual stress in laser powder bed fused IN718 alloy.
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Recently, I am working on a study about PWHT. I curious on when did PWHT first appear? How did PWHT develop with history time ? Which research institutions have made outstanding contributions in this regard?
hope to update the knowledge of PWHT, looking foward for your reply.
Thanks in advance.
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Please check the attached file, I hope it would help
Thanks
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PWHT (post weld heat treatment) is widely used to eliminate welding residual stress, but how to evaluate the effectiveness? what are the commonly used methods to measure welding residual stress in a component in or to be in service? Any standards?
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You could also check the Blind Hole Drilling technique for components in service. The technique is a bit old-fashioned maybe and less accurate than XRD but the equipment can easily be carried on site. Also, take in mind that it is semi-destructive cause you drill a small hole on the sample. Maybe in some cases can be repaired with cladding or even not depending on the application. Good luck!
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Trying to optimize mechanical properties of cast steel through heat treatment and would like to find any theoretical methods to generate a hypothesis defining final mechanical properties.
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Yes it is a sophisticated topic, for that I recommend you to go through the methodology included in the experimental procedure section in [1] that leading to determination the maximum austenite grain size during normalizing for a given temperature. In [2] the growth behavior and the effects of the holding time and heating temperature on the grain sizes were investigated and analyzed to predict the austenite growth using the Sellar's model.
Best regards
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Whereas strength is proportional to density in metal case.
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Because density is not directly related with the UTS. In addition, heat treatment actually reduce UTS and hardness.
On the other hand, density depends on the processing parameters.
Finally, the heat treatment is applied for stress relief.
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Hello Researchers,
As from literature it was seen that aluminium alloy Al5083 can only be strengthened by work hardening and micro-alloying. Similarly, I want to know what are the only possible processes through which AZ91 can be strengthened.
Moreover, If you suggest the process with the any limitations it would add supplementary to my work.
Thank you
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Yes can understand is not an easy job.
So is it better to move towards solid state techniques.
Kind Regards,
Roshan
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With the development of large size heavy section pressure vessel, local post wed heat treatment(PWHT) instead of furnace PWHT must be used. Absloutely, there are differences between furnace PWHT and local PWHT. For example, the structural constraints, the temperature distribution field will be significantly different. Obviously,The effect of PWHT will also be different. So, my questions are :What's the essential difference between furnace post weld heat treatment (PWHT) and local PWHT?How does this difference affect the release of residual stress and the change of microstructure and properties?
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Vadim Verlotski ,I‘m sorry I forgot to state that the materials I want to study are low alloy steels and stainless steels,such as Cr-Mo-V steel,9% Cr steel ,304 stainless steel ,316 stainless steel,etc. According to what I have learn, it is hard to release the welding residual stress completely by PWHT (including furnace PWHT). That's why I curious about the stress relief mechanism of PWHT. Meanwhile, that's also my motivtion for the topic of the disscussion. In other words, I want to know the difference of stress reilef mechaism between furnace PWHT and local PWHT.
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Dear All
Modulus of rupture (MOR) and modulus of elasticity (MOE) are two parameters in heat-treated woods. In the following paper, the Authors used time, temperature, and relative humidity or wood species parameters for determining the MOR and MOE by Artificial Neural Networks (ANNs).
Are there mathematical equations and formulas for determining MOR and MOE with time, temperature, and relative humidity in standard codes and other papers?
Best regards
Mehdi Nikoo
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I hope you are doing fine, and thanks for answering my question. I saw equations based on the F, L, h, and b variables.
The data consists of three input variables time, temperature, and relative humidity, and two output variables, the MOR and MOE. I modeled the MOR and MOE, and I need equations or methods that have used these three variables to compare my results.
Could you please kindly send your opinions?
Best regards
Mehdi Nikoo
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Respected fellows.
why we can not do direct aging heat treatment after homogenizing heat treatment on Fe-Ni superalloys? what is the purpose of (Solid) solution treatment which is different then aging?
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The purpose of homogenization treatment is different from solution treatment and therefore heat treatment temperature and times of the two treatments may differ. While through homogenization treatment we want to get rid of coring or solute concentration gradient in a cast alloy, in solution treatment our aim it to get all the solutes needed for precipitation hardening into the solution so that we can achieve maximum precipitate volume fraction during aging treatment.
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I have coated conductive glass with TiO2 using dip coating, the precursor I used was titanium butoxide, and I prepared 0.1 M solution with this precursor ( Propanol as solvent), the main problem is that even under various heat treatment ranges ( from 400 C for 2h to - 500 C for 24 h )I can not get anatase and the Raman spectra show the spectrum of the substrate only like there is no coating or no crystallinity. But the layer can be seen under SEM and the thickness is less than 100 nm.
Is there any suggestion on how to obtain anatase? Changing the precursor can help?
PS: I can not increase the annealing temperature to more than 500 C, because of the substrate.
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These are interesting documents to check them as well. My Regards
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Can we synthesis SeO2 (powder) Just by heat treatment of Se (powder) in Oxygen environment? And if yes at what temperature and for how much time it should be treated?
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Dear Abdul, thank you for asking this very interesting chemical question. Simply burning elemental selenium in air or oxygen is not sufficient to make selenium dioxide. You need to have a small amount of nitric acid as catalyst. An easier and more reliable method involves the reaction of elemental selenium with concentrated nitric acid. Selenium powder is added in small portions to concentrated HNO3 and the resulting solution is evaporated to dryness in the fume hood. Final purification can be achieved by sublimation at ca. 315 °C. Please note that SeO2 is quite hygroscopic. For more basic information please have a look at this rather old (1945) article:
Selenium Dioxide: Preparation, Properties, and Use as Oxidizing Agent
Please check if this review article is accessible through your institution, as it is not available as public full text on RG.
Good luck with your work and best wishes, Frank Edelmann
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Al A356
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@M.Amin Ezazi,
but it have to consider this temp. in kelvin not in celsius .
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to make ybco thin films by FF-MOD method during the process of formation of ybco on the substrate in the furnace we use wet O2 atmosphere from room temperature to 850⁰c , could someone please explain me why ?
Thanks in advance.
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thank you for this interesting question.
Wet oxidation process results in faster oxide growth, and strongly assists the stability of the as-deposited film against the ambient. But the main role of using wet oxygen process is the changing of the electrical property from semiconducting to metallic behavior in film resistivity vs. temperature.
Best regards
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I've been using the same 1" tube furnace to carbonize my polymer nanofibers. I follow a typical protocol where I first stabilize the sample in a box furnace (in air) at 280 C then use the tube furnace under 60 sccm UHP N2 at 1000 C (ramp 5 C/min) for 1 hour. This gave me no problem before and only recently I started seeing 2 things:
1) no sample is left after carbonization. There are sometimes some white flakes left in the crucible, but my sample is supposed to be black after carbonization.
2) the outlet end of the tube is contaminated with some white material, I'm not sure what. The sample I start with is brown color.
I have a suspicion this started happening when we installed a metal gasket with rubber O-rings on both ends of the tube. Before, we just had a rubber stopper with glass tube going through to supply the gas. However, I'm not sure how that could remove all of my samples and contaminate the tube with white stuff.
Anyone have any insights on what could have happened?? Thank you!!
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Infact, I stumbled into this as a result of my sample loss in the tube furnace as explained by Sooyoun Yu. I think I should apply some stabilisation firstly as she advised before taking to the tube furnace. I will like to know she finally solved the issue.
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I would like to simulate the microstructural evolution of a super alloy during and after heat treatments and thermomechanical treatments using the JMAK model. And I am looking for some free software that can help me.
Thanks!
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During pasteurization, proteins present in suspension in liquid egg whites are impacted by pH, the temperature of pasteurization, and tithe me the product is held hot. I am looking for a simple, portable test/equipment to measure the amount of opaqueness of the liquid egg whites after the heat treatment.
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You might try refractive index. It may not be a "direct" measure of scatter, precisely, but the chemical changes that cause scatter would likely also change the angle of a laser as it passes through the medium. That might be less sensitive to dimensional variation in the sample.
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Hi All,
I am trying to heat-kill some bacteria for an experiment, but do not want them to rapture (ie. maintaining their cell wall structure). does anyone have a quick and easy-to-do protocol for this, please?
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Hi Priscilla,
The temperature and length of heat treatments for killing bacteria depends on the bacterial species you are using, and on the growth conditions. Robustness of bacterial envelope greatly varies across species (i.e. between Gram- and Gram+). Moreover, for bacterial species able to sporulate, heat treatments are necessarily harsher and longer, if one wants to eliminate all viable spores. The physiological status of the bacterial population can also affect thermal sensitivity; for instance, actively replicating bacteria vs bacteria in stationary phase or in biofilms can respond very differently to heat.
As a reference, for Escherichia coli happily growing at exponential phase in rich medium, 5 minutes at 70 degrees might suffice to kill the entire population without affecting cell structure of most bacteria (there will always be some lysis).
What I would do is checking different temperatures and treatment lengths for your specific bacteria in the concrete conditions you are planning to use, and then check cell viability (by plating) and integrity (by microscopy), in order to choose the conditions that maximize killing without significantly affecting cell integrity.
Good luck!
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How to modify whey protein and/or casein functional property so that they form crosslink at ambient temperature or without heat treatment in solution/colloidal state.
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Deformed steel structures can be repaired with heat straitening technique. However, column straitening is a difficult task as deformation will lead to eccentricity and during heat straitening one has to ensure that
this is not aggravated further . At times columns are heavy structural members with bending at two places which poses another threat. This requires extremely careful planning to avoid failure during heat treatment. As a result most of the time these are uneconomically replaced. Do we have any new trend in restoration of bended/deformed columns.
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quite interesting case of column which was hit by a heavy earth mover and the same resulted in bending of the same. In this form lot of eccentricity has developed but the column is still intact and no distress in the entire structure. Probably highly indeterminacy compounded with very high factor of safety of the structure has resulted in the functionality of the deformed column.
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I need to deposit the anatase TiO2 layer on ITO and FTO glasses, considering the experimental parameters, I found the optimum heat treatment temperature for 450 C. However, the substrate can not bear higher than 200 C. Is it possible to decrease crystallization temperature by playing with experimental parameters? which parameter is more effective in decreasing crystallization temperature?
PS. I used Titanium butoxide as a precursor and propanol as a solvent.
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Dear Mahsa,
this is a very interesting technical question. Unfortunately I cannot provide you with a qualified expert answer, as we work in organometallic chemistry. However, I just came across the following potentially useful review article which might help you in your analysis:
Low-temperature crystallization of solution-derived metal oxide thin films assisted by chemical processes
Luckily this very instructive review article has been posted by the authors as public full text on RG. Thus it can be freely accessed and downloaded as pdf file. I'm sure it will be of interest for you.
Good luck with your research and best wishes, Frank Edelmann
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I want to know some research projects that I can work for in my academic curriculum in materials engineering
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You can work with aquatic quantum materials discovered by me. At a concentration near the critical concentration of the formation of spherical micelles of ionic surfactants and in the region of the conformational transition of polyelectrolytes in water, quantum fluctuations of stretching and torsional modes of water appear, which create pulsating cavities for micelles and coils. It is necessary to study these phase transitions and investigate the energy of thermal and quantum fluctuations. For full details read my articles and patents.
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when Ti/Nb etc strong carbide formers are added to steel to prevent Cr- carbide precipitation (SENSITIZING), especially in case of Stainless steels, why these steels are more prone to high- temperature grain growth? True that GB precipitates of Cr-Carbides would no longer act to pin grain boundary, but would not fine precipitates of Ti/Nb carbides also act somewhat to retard grain growth ? and why is that Nb-Stainless steels (980-1065 C)need narrower solution annealing range than Ti-Stainless steel (955-1065 C)?
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In general, there are two phenomena that explain the observed behavior of
contacting grains leading to growth. In the first place, mass diffusion across the
grains contacting boundaries followed by particles contacting boundaries migration and this step requires higher activation energy. So the mass transport by diffusion rout at any annealing temperature is strongly related to the grains surface energy. Now, the heat of formation of chromium carbides is less than titanium carbide and much less than niobium carbide and so the surface energy of grains (grains boundaries energy) becomes much higher with chromium carbides. This means that mass diffusion between grains crossing the contacting boundaries for growth become higher in the order niobium; titanium and chromium carbides and thus the growth rate follow the same trend. Therefore the stabilized steels with Ti and/or Nb are more prone to grain growth during solution annealing.
Best regards
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is it necessity to homogenize cast ingot of wrought superalloys (such as Hastelloy X, haynes 25 etc.)? if hot forging or hot rolling were done without homogenizing heat treatment what is happen?
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It is important to avoid cracks during the following conformation processes.
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I did carbonization of PAN Electrospun nanofiber at 900 C under the flow of nitrogen but SEM images of Carbonized samples are showing bead formation and fiber reduction from 700 nm to 150 nm. what could be the reason behind the formation of beads after heat treatment is it possible such a huge reduction in fiber diameter
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Milad Razbin
Thank you sir for your answer.
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I have magnetic beads coated with polystyrene material ( Invitrogen Dynabeads, cat 65011). When running these beads on the flow cytometer two SSC populations appear. Ideally, if we are using beads we must see a small concentrated population. I would like to mention that my experiment involves the vortexing of beads and heat treatments.
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Hi Sandeep Poonia,
I would suggest you validate your vortex speeds and heat treatment first. Because what I see on your graphs is too much debris. You should also check your beads (storage conditions, expiration date, transport conditions etc.) Also try using SSLog/FSLİn graphs you may be able to see a better image of beads. You need to validate your protocol (gain and voltage settings) for better images.
Hope this information is helpful for you,
Best wishes,
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Develope a detailed heat treatment cycle
Plz guide me
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I want to use dried fungi biomass but I have no idea how can I kill fungi spores with less damaging fungi biomass. I was thinking about putting broth media which I cultured fungi in into the water bath for 75°C 40min and dry in with a freeze dryer. Does it gonna work?
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Dear sir, you dont mention what you need work in fungal biomass. I think that fungal conidia (spore) dose not has negative effect on the biomass function when its found with mycelia.
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I have some samples and I need to do heat treatment on them to release the residual stress after 3d printing and make better the ductility for the tensile test.
I heated them in a vacuum furnace with the 750-degree celsius for 2 hours.
As the container was graphite, we put a thin layer of Zironica powder under them. but the result was awful. as I am not familiar with metallurgy and this process too much, anybody can give me some advice and guidance on why it happened to my samples?
It seems, under the samples that are in the contact with the powder, has the blue color(dark blue), and another area is the yellowish color like gold and it seems, the shape of one of my samples changes because of heating.
this result is strange because the color changed in the vacuum furnace without any gas inside.
The first image is all samples after heating.
The second image is under one of the samples that have close contact with Zironica powder
(The white part is the Zironica powder that remained on the samples)
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The problem with heat treatment of titanium alloys is that this material oxidizes even at very low oxygen partial pressures. Even the best vacuum furnaces fail to prevent oxidation of elements such as titanium, aluminum, zirconium and vanadium, as you have seen. Oxidation of zirconium and aluminum always produces white oxides (your white powder that adheres to the samples). Titanium can form both white and blue oxide layers (blue oxide is formed at a low oxygen partial pressure), while vanadium forms yellow and brown oxides. All of these colors are present on your samples, which indicates a fairly intense oxidation of the samples in your vacuum oven.
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Hello colleagues.
I am analyzing some phase transitions during heat treatment of calcium phosphate materials. Although I am having trouble to fit the data properly. I am using profex, and I an allowing some variation on the lattices parameters because the heat expansion. I have never done Rietveld refinement in HT-XRD data before, so I am wondering if there's anyway that I can set the temperature of the cif file data to consider it when fitting the data.
Thank you!
Best regards from Brazil.
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Hello Kim Doyeon !
I am so sorry, I've just read your reply!
Thank you very much for your inputs, I finally fixed the problem!
Kind regards,
João.
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How have people set up loading/boundary conditions for a quenching heat treatment model simulation? Do you apply loads or boundary conditions? Do you use an interface condition such as surface film condition and apply a film coeff (your HTC value)? I havn't been able to find any papers that really explicitly lay out how the setup is done.
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The heating temperature before quenching can be set in the Load module as predefined field. for the HTC, we can use the surface film condition-f(T) in the interaction module。
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High-S, especially resulfurized steels are discouraged from Boriding. What can a 0.1% Sulfur (and 0.5% Mn in ~0.1%C steel with Minor Cr, W, Ni alloys, all below 0.5%) do harm to boriding layer? Is it forming soft phases? Low-melting eutectic? brittle but mechanically weak phase? Or a combination thereof?
Can any separate chemical agents be treated on steel surface to make it fit for boronizing?
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Toughness also increases with addition of sulphur.
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I have performed solution heat treatment at 1050 C for 1 hrs followed by water quenching. A layer (black) is formed. How I can remove the layer as I have to perform chemical etching on the sample and until that the layer is removed chemical etching cannot be performed over the sample. Kindly provide your valuable suggestions....My material is 17-4 PH stainless steel.
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Hi all,
I want to know how two carbide material will sandwich with each other. Let me make my question more elaborative. Let say, X2C and Y2C carbide materials are there, now I want to make X2C-CY2 (X2C2Y2) out of them. Is there any specific process to do the same like any chemical reaction with solvent (with heat treatment also) or any other procedure?
Any small suggestion is highly appreciable.
Thanks in advance.
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Thanks again. yea, this a question not a discussion, next time I will be aware of that.
I want to prepare metal carbide composite. I have Cobalt metal carbide Co2C and Co3C and now I want to make the composite like Co2C-CCo3 i.e. want to make a common carbon bond. Or might be a common carbon layer one side will be Co2C and other side will be Co3C. Is there any reaction or procedure to make it?
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Thickness and diameter shrinkage percentage of the Al2O3 sample (after sintering):
Diameter 20%
Thickness 18%
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thanks for your important question
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I have found out that in some research journals, people have reported solution heat treatment of 17-4 PH stainless steel at 1040 C for 30 min and quenching in air ( Air cooling) whether some of them reported heating at 1040 for 1 hr than water quenched. Kindly answer me which process to be adopted to perform solution heat treatment in case of 17-4 PH stainless steel ??
Do I really have to go for 1hr of solution heat treatment or 30 min will be enough along with which type of quenching is required ( water or Air quenching) ??
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The recommended heat-treatment of 17-4 PH stainless steel is as follows: Solution treatment is performed at 1040 °C for 1 h followed by water quenching. subsequently, aging could be conducted at low temperatures followed by air cooling to enhance precipitation and the relevant mechanical properties.
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I have seen some journals mentioned stress relieving heat treatment for Al12Si alloy but the procedure is same as annealing/normalizing
Can anyone explain the procedure for stress relieving heat treatment and the difference between those?
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Stress relieving can be considered as a category of annealing. In the stress relieving the work piece is heat treated at a lower temperature (below recrystallization or transformation temperature) and its sole purpose is to eliminate the internal residual stress generated by previous forming operations. No phase or microstructural change occurs in this process, only stresses are eliminated.
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I studied journals on SLM (Selective Laser Melting) produced Al12Si components
In that many authors used Solution heat treatment/ annealing.
but for AlSi10Mg they used T6 heat treatment
why can't we use the same T6 for Al12Si?
Your answers help me a lot
Thanks in Advance
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Thank you for answering
What I understand from the above two answers is
by looking phase diagram, at AA temperature (150-1800 C), the solubility of Si in Aluminum gets zero but in Al10SiMg because of Mg content Si is not precipitated and forms Mg2Si
Correct me if I am wrong
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We prepared Ti-6Al-7Nb alloy by investment centrifugal casting. The elongation we obtained is relatively low but yield strength and ultimate tensile strength are high enough as desired.
Several ways we have done to improve/optimize mechanical properties especially elongation such as heat treatment process, gating system design, process parameter adjustment etc. However, elongation is still low, below 8%. How to improve elongation for minimum 8%? Is it possible for investment centrifugal casting method?
Thank you very much.
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Dear Idham Damisih,
To improve the elongation it is necessary to grind the structure. By centrifugal casting a fine surface structure can be achieved. In depth, the structural grains grow together due to the cooling rate.
If the cooling rate can be increased, the structure will also improve. Then it is necessary to carry out ternic processes to reduce internal stresses. Doug approach to improving and crushing the structure is by plastic hot deformation (rolling, stamping or pressing).
I wish you success!
Emil Yankov