CN113836715B - Forging deformation process test method - Google Patents

Forging deformation process test method Download PDF

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CN113836715B
CN113836715B CN202111107139.2A CN202111107139A CN113836715B CN 113836715 B CN113836715 B CN 113836715B CN 202111107139 A CN202111107139 A CN 202111107139A CN 113836715 B CN113836715 B CN 113836715B
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deformation
forging
bar
strain field
sampling
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CN113836715A (en
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向伟
袁武华
吴正刚
翟瑞志
徐邹圆
谢静
罗恒军
尹卫东
尹慧
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China National Erzhong Group Deyang Wanhang Die Forging Co ltd
Hunan University
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China National Erzhong Group Deyang Wanhang Die Forging Co ltd
Hunan University
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    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2111/00Details relating to CAD techniques
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
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  • Forging (AREA)
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Abstract

The invention provides a forging deformation process test method, which comprises the following steps: A. performing numerical simulation on the bar upsetting process to obtain the equivalent strain field distribution condition of the forging; B. determining a region with the same deformation amount as the engineering deformation amount corresponding to the equivalent strain field according to the strain field distribution condition, and determining a sampling region in the region; C. repeating step A, B to obtain a proper bar diameter and thickness and a sampling area; D. c, blanking according to the diameter and thickness of the bar obtained in the step C, and forging a upsetting cake according to the set deformation to obtain a forging piece; E. sampling in a sampling area and carrying out mechanical property test to obtain the relation between the deformation and the tissue property. The invention samples and detects in the sampling area with the deformation corresponding to the equivalent strain field and the engineering deformation being uniform and consistent, avoids the influence of different deformation on the tissue performance, and can accurately establish the relationship between the deformation and the tissue performance so as to guide the actual production and obtain the optimal tissue performance of the forging.

Description

锻造变形工艺试验方法Forging deformation process test method

技术领域Technical field

本发明涉及锻造试验技术领域,尤其是一种锻造变形工艺试验方法。The invention relates to the technical field of forging testing, in particular to a forging deformation process testing method.

背景技术Background technique

钛合金、钢及高温合金等金属材料锻件,特别是新型的金属材料锻件,为了获得最佳的组织性能,通常需要进行锻造工艺试验研究,以获取最佳的锻造工艺参数。现有的锻造变形工艺试验,往往需要先计算工程变形量,再结合数值模拟计算等效应变量,找出工程应变与等效应变对应关系,确定合适的变形量窗口,对于有复杂变形过程的试验,往往难以准确判断变形量或等效应变,更不容易建立变形量与组织性能间关系,往往造成试验结果可能与实际规律出现偏差。In order to obtain the best structural properties for metal material forgings such as titanium alloys, steels and high-temperature alloys, especially new metal material forgings, it is usually necessary to conduct forging process experiments and studies to obtain the best forging process parameters. Existing forging deformation process tests often need to first calculate the engineering deformation, and then use numerical simulation to calculate the equivalent variables, find out the corresponding relationship between the engineering strain and the equivalent strain, and determine the appropriate deformation window. For tests with complex deformation processes, , it is often difficult to accurately judge the amount of deformation or equivalent strain, and it is even more difficult to establish the relationship between the amount of deformation and tissue properties, which often results in test results that may deviate from the actual rules.

发明内容Contents of the invention

本发明所要解决的技术问题是提供一种锻造变形工艺试验方法,容易建立工程应变与等效应变对应关系,从而准确建立变形量与组织性能间关系,以指导实际生产,获取最佳的锻件组织性能。The technical problem to be solved by the present invention is to provide a forging deformation process test method that can easily establish the corresponding relationship between engineering strain and equivalent strain, thereby accurately establishing the relationship between deformation amount and structural properties to guide actual production and obtain the best forging structure. performance.

本发明解决其技术问题所采用的技术方案是:锻造变形工艺试验方法,包括以下步骤:The technical solution adopted by the present invention to solve the technical problem is: a forging deformation process test method, which includes the following steps:

A、选取棒料作为试验材料,对棒材镦饼过程进行数值模拟,镦饼变形达到工程变形量后,得到锻件的等效应变场分布情况;A. Select the bar as the test material and conduct a numerical simulation of the bar forging process. After the forging deformation reaches the engineering deformation amount, the equivalent strain field distribution of the forging is obtained;

B、根据应变场分布情况,确定等效应变场对应的变形量与工程变形量相同的区域,在该区域内确定取样区域;B. According to the distribution of the strain field, determine the area where the deformation amount corresponding to the equivalent strain field is the same as the engineering deformation amount, and determine the sampling area within this area;

C、重复步骤A、B,在数值模拟过程中反复优化迭代得到合适的棒料直径和厚度,并得到等效应变场对应的变形量与工程变形量均匀一致的取样区域;C. Repeat steps A and B, repeatedly optimize and iterate during the numerical simulation process to obtain the appropriate bar diameter and thickness, and obtain a sampling area where the deformation amount corresponding to the equivalent strain field is uniform and consistent with the engineering deformation amount;

D、根据步骤C得到的棒料直径和厚度下料,并根据设定的变形量进行镦饼锻造,得到锻件;D. Cut the material according to the diameter and thickness of the bar obtained in step C, and perform upsetting forging according to the set deformation amount to obtain the forging;

E、在锻件上取样并进行力学性能测试,取样位置位于步骤C中的取样区域;E. Take samples from the forgings and conduct mechanical property tests. The sampling location is located in the sampling area in step C;

F、根据力学性能测试结果统计分析,得出变形量与组织性能关系,识别最佳性能,确定最佳锻造变形量工艺参数。F. Based on the statistical analysis of the mechanical property test results, the relationship between deformation and organizational properties is obtained, the best performance is identified, and the optimal forging deformation process parameters are determined.

进一步地,步骤A中,棒料的直径大于或等于200mm,长度大于或等于50mm。Further, in step A, the diameter of the bar is greater than or equal to 200mm, and the length is greater than or equal to 50mm.

进一步地,步骤A中,工程变形量为10%至80%。Further, in step A, the engineering deformation amount is 10% to 80%.

本发明的有益效果是:本发明在等效应变场对应的变形量与工程变形量均匀一致的取样区域进行取样检测,避开了不同变形量对组织性能影响,可以准确建立变形量与组织性能间关系,以指导实际生产,获取最佳的锻件组织性能。The beneficial effects of the present invention are: the present invention conducts sampling and detection in a sampling area where the deformation amount corresponding to the equivalent strain field is uniform and consistent with the engineering deformation amount, avoiding the impact of different deformation amounts on tissue performance, and can accurately establish the deformation amount and tissue performance relationship to guide actual production and obtain the best structural properties of forgings.

附图说明Description of the drawings

图1是棒材示意图;Figure 1 is a schematic diagram of the bar;

图2是镦饼变形后的锻件示意图;Figure 2 is a schematic diagram of the forging after deformation;

图3是本发明中实例20%工程变形量对应的横截面等效应变场的分布示意图;Figure 3 is a schematic distribution diagram of the cross-sectional equivalent strain field corresponding to 20% engineering deformation in the example of the present invention;

图4是本发明中实例20%工程变形量对应的取样区域示意图;Figure 4 is a schematic diagram of the sampling area corresponding to 20% engineering deformation in the example of the present invention;

图5是本发明中实例50%工程变形量对应的横截面等效应变场的分布示意图;Figure 5 is a schematic distribution diagram of the cross-sectional equivalent strain field corresponding to 50% engineering deformation in the example of the present invention;

图6是本发明中实例50%工程变形量对应的取样区域示意图。Figure 6 is a schematic diagram of the sampling area corresponding to 50% engineering deformation in the example of the present invention.

具体实施方式Detailed ways

下面结合附图和实施例对本发明进一步说明。The present invention will be further described below in conjunction with the accompanying drawings and examples.

本发明的锻造变形工艺试验方法,包括以下步骤:The forging deformation process test method of the present invention includes the following steps:

A、选取棒料作为试验材料,如图1所示,棒料的直径大于或等于200mm,长度大于或等于50mm,利用最常见的镦粗锻造对材料的变形进行试验。A. Select the bar as the test material. As shown in Figure 1, the diameter of the bar is greater than or equal to 200mm and the length is greater than or equal to 50mm. The most common upsetting forging is used to test the deformation of the material.

对棒材镦饼过程进行数值模拟,镦饼变形达到工程变形量后,得到如图2所示的锻件,确定锻件的等效应变场分布情况,工程变形量可以在10%至80%之间。数值模拟在数值模拟软件中进行,可以模拟棒材的镦饼过程,可以方便地调节各种参数如棒材尺寸、锻造变形量、锻造压力、锻造温度等,得到不同性能的锻件。此外,数值模拟软件还可以自动生成锻件的等效应变场分布图。Numerical simulation is performed on the bar forging process. After the forging deformation reaches the engineering deformation amount, the forging is obtained as shown in Figure 2. The equivalent strain field distribution of the forging is determined. The engineering deformation amount can be between 10% and 80%. . Numerical simulation is carried out in numerical simulation software, which can simulate the forging process of bars. Various parameters such as bar size, forging deformation, forging pressure, forging temperature, etc. can be easily adjusted to obtain forgings with different properties. In addition, the numerical simulation software can also automatically generate the equivalent strain field distribution map of the forging.

B、根据锻件的应变场分布情况,确定等效应变场对应的变形量与工程变形量相同的区域,在该区域内确定取样区域。由于数值模拟是模拟理想状况下的锻造过程,而实际锻造过程中受到摩擦力等因素的影响,导致数值模拟与实际锻造情况存在一定的差异,使得等效应变场对应的变形量与工程变形量不能完全相同,因此,通过人工确定效应变场对应的变形量与工程变形量相同的区域。B. According to the strain field distribution of the forging, determine the area where the deformation amount corresponding to the equivalent strain field is the same as the engineering deformation amount, and determine the sampling area within this area. Since numerical simulation simulates the forging process under ideal conditions, and the actual forging process is affected by friction and other factors, there is a certain difference between the numerical simulation and the actual forging situation, making the deformation amount corresponding to the equivalent strain field different from the engineering deformation amount. They cannot be exactly the same. Therefore, the area where the deformation amount corresponding to the effect strain field is the same as the engineering deformation amount is manually determined.

C、重复步骤A、B,在数值模拟过程中反复优化迭代得到合适的棒料直径和厚度,并得到等效应变场对应的变形量与工程变形量均匀一致的取样区域。即多次调节棒料直径和厚度以及其他锻造工艺参数,得到较佳的锻造工艺参数,且通过多次确定等效应变场对应的变形量与工程变形量均匀一致的取样区域,保证了取样区域的准确性以及取样区域的大小满足取样要求。此外,还可以确定多种工程变形量对应的取样区域。C. Repeat steps A and B, repeatedly optimize and iterate during the numerical simulation process to obtain the appropriate bar diameter and thickness, and obtain a sampling area where the deformation amount corresponding to the equivalent strain field is uniform and consistent with the engineering deformation amount. That is, the diameter and thickness of the bar and other forging process parameters are adjusted multiple times to obtain better forging process parameters, and the sampling area is ensured by repeatedly determining the deformation amount corresponding to the equivalent strain field and the engineering deformation amount to be uniform. The accuracy and size of the sampling area meet the sampling requirements. In addition, the sampling areas corresponding to various engineering deformations can also be determined.

D、根据步骤C得到的棒料直径和厚度下料,并根据设定的变形量进行镦饼锻造,得到锻件。锻造工艺与步骤C中优化迭代得到的锻造工艺相同,减小数值模拟与实际锻造的误差,提高试验的准确性。D. Cut the bar according to the diameter and thickness obtained in step C, and perform upsetting forging according to the set deformation amount to obtain the forging. The forging process is the same as that obtained by the optimization iteration in step C, which reduces the error between numerical simulation and actual forging and improves the accuracy of the test.

E、在锻件上取样并进行力学性能测试,取样位置位于步骤C中的取样区域。通过在等效应变场对应的变形量与工程变形量均匀一致的取样区域进行取样,消除了实际锻造过程中的各种因素对样品性能的影响,保证试样的工程变形量与等效应变场对应的变形量均匀一致,避开了不同变形量对组织性能影响,可以准确建立变形量与组织性能间关系,以指导实际生产,获取最佳的锻件组织性能。E. Take samples from the forgings and conduct mechanical property tests. The sampling location is located in the sampling area in step C. By sampling in a sampling area where the deformation amount corresponding to the equivalent strain field is consistent with the engineering deformation amount, the influence of various factors in the actual forging process on the sample performance is eliminated, and the engineering deformation amount and the equivalent strain field of the sample are ensured. The corresponding deformation amount is uniform, avoiding the influence of different deformation amounts on the structural properties. The relationship between the deformation amount and the structural properties can be accurately established to guide actual production and obtain the best structural properties of forgings.

F、根据力学性能测试结果统计分析,得出变形量与组织性能关系,识别最佳性能,确定最佳锻造变形量工艺参数。F. Based on the statistical analysis of the mechanical property test results, the relationship between deformation and organizational properties is obtained, the best performance is identified, and the optimal forging deformation process parameters are determined.

下面以某TB18钛合金为例对本发明进一步说明The present invention will be further explained below by taking a certain TB18 titanium alloy as an example.

实施例一Embodiment 1

A、选取棒料作为试验材料,对棒材镦饼过程进行数值模拟,设定工程变形量20%,镦饼变形达到工程变形量后,得到锻件的等效应变场分布情况;A. Select the bar as the test material, conduct a numerical simulation of the bar forging process, set the engineering deformation amount to 20%, and obtain the equivalent strain field distribution of the forging after the forging deformation reaches the engineering deformation amount;

B、根据应变场分布情况,确定等效应变场对应的变形量与工程变形量相同的区域,在该区域内确定取样区域;B. According to the distribution of the strain field, determine the area where the deformation amount corresponding to the equivalent strain field is the same as the engineering deformation amount, and determine the sampling area within this area;

C、重复步骤A、B,在数值模拟过程中反复优化迭代得到棒料规格为φ300×70mm,棒料厚度由70mm变形至56mm即达到设定的工程变形量,得到如图3所示的锻件的等效应变场分布图,图3显示大部分区域等效应变分布在0.218~0.243,该效应变分换算出的变形量为19.6%~21.5%,与工程变形量基本一致,因此可将等效应变在0.218~0.243的区域作为取样区域,该取样区域如图4所示,呈圆环形。C. Repeat steps A and B, and repeatedly optimize and iterate during the numerical simulation process to obtain the bar specification of φ300×70mm. The bar thickness is deformed from 70mm to 56mm to reach the set engineering deformation amount, and the forging shown in Figure 3 is obtained. The equivalent strain field distribution diagram of The area where the effective strain is between 0.218 and 0.243 is used as the sampling area. The sampling area is shown in Figure 4 and is circular.

D、锯切TB18钛合金棒料φ300×70mm,锯切后的棒料厚度公差控制在±1mm以内,采用步骤C优化后的锻造工艺对棒料进行墩饼锻造,直到棒料的厚度减小至56mm,此时工程变形量为20%。D. Saw the TB18 titanium alloy bar φ300×70mm. The thickness tolerance of the bar after sawing is controlled within ±1mm. Use the forging process optimized in step C to forge the bar until the thickness of the bar is reduced. to 56mm, at which time the engineering deformation is 20%.

E、对锻件进行热处理,然后在如图4所示的取样区域内进行取样,并对样品进行力学性能测试。E. Heat treat the forgings, then take samples in the sampling area as shown in Figure 4, and conduct mechanical property tests on the samples.

F、根据力学性能测试结果统计分析,得出变形量与组织性能关系,识别最佳性能,确定最佳锻造变形量工艺参数。F. Based on the statistical analysis of the mechanical property test results, the relationship between deformation and organizational properties is obtained, the best performance is identified, and the optimal forging deformation process parameters are determined.

实施例二Embodiment 2

A、选取棒料作为试验材料,对棒材镦饼过程进行数值模拟,设定工程变形量50%,镦饼变形达到工程变形量后,得到锻件的等效应变场分布情况;A. Select the bar as the test material, conduct a numerical simulation of the bar forging process, set the engineering deformation to 50%, and obtain the equivalent strain field distribution of the forging after the forging deformation reaches the engineering deformation;

B、根据应变场分布情况,确定等效应变场对应的变形量与工程变形量相同的区域,在该区域内确定取样区域;B. According to the distribution of the strain field, determine the area where the deformation amount corresponding to the equivalent strain field is the same as the engineering deformation amount, and determine the sampling area within this area;

C、重复步骤A、B,在数值模拟过程中反复优化迭代得到棒料规格为φ300×70mm,棒料厚度由70mm变形至35mm即达到设定的工程变形量,得到如图5所示的锻件的等效应变场分布图,图5显示大部分区域等效应变分布在0.705~0.734,该效应变分换算出的变形量为50.5%~52%,与工程变形量基本一致,因此可将等效应变在0.705~0.734的区域作为取样区域,该取样区域如图6所示,呈圆环形。C. Repeat steps A and B, and repeatedly optimize and iterate during the numerical simulation process to obtain the bar specification of φ300×70mm. The bar thickness is deformed from 70mm to 35mm to reach the set engineering deformation amount, and the forging shown in Figure 5 is obtained. The equivalent strain field distribution diagram of The area where the effective strain is between 0.705 and 0.734 is used as the sampling area. The sampling area is shown in Figure 6 and is circular.

D、锯切TB18钛合金棒料φ300×70mm,锯切后的棒料厚度公差控制在±1mm以内,采用步骤C优化后的锻造工艺对棒料进行墩饼锻造,直到棒料的厚度减小至35mm,此时工程变形量为50%。D. Saw the TB18 titanium alloy bar φ300×70mm. The thickness tolerance of the bar after sawing is controlled within ±1mm. Use the forging process optimized in step C to forge the bar until the thickness of the bar is reduced. to 35mm, at which time the engineering deformation is 50%.

E、对锻件进行热处理,然后在如图6所示的取样区域内进行取样,并对样品进行力学性能测试。E. Heat treat the forgings, then take samples in the sampling area as shown in Figure 6, and conduct mechanical property tests on the samples.

F、根据力学性能测试结果统计分析,得出变形量与组织性能关系,识别最佳性能,确定最佳锻造变形量工艺参数。F. Based on the statistical analysis of the mechanical property test results, the relationship between deformation and organizational properties is obtained, the best performance is identified, and the optimal forging deformation process parameters are determined.

以上所述仅为本发明的优选实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention and are not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention shall be included in the protection scope of the present invention.

Claims (3)

1. The forging deformation process test method is characterized by comprising the following steps of:
A. selecting a bar as a test material, performing numerical simulation on a bar upsetting process, and obtaining the equivalent strain field distribution condition of the forging after upsetting deformation reaches engineering deformation;
B. determining a region with the same deformation amount as the engineering deformation amount corresponding to the equivalent strain field according to the strain field distribution condition, and determining a sampling region in the region;
C. repeating the step A, B, and adjusting the diameter and the thickness of the bar stock for a plurality of times in the numerical simulation process to obtain the proper diameter and the thickness of the bar stock, and obtaining a sampling area with the deformation corresponding to the equivalent strain field and the engineering deformation being uniform and consistent;
D. c, blanking according to the diameter and thickness of the bar obtained in the step C, and forging a upsetting cake according to the set deformation to obtain a forging piece;
E. c, sampling on the forging piece and carrying out mechanical property test, wherein the sampling position is positioned in the sampling area in the step C;
F. and according to the statistical analysis of the mechanical property test result, obtaining the relation between the deformation and the tissue property, identifying the optimal performance, and determining the technological parameters of the optimal forging deformation.
2. The forging deformation process test method as recited in claim 1, wherein: in the step A, the diameter of the bar stock is larger than or equal to 200mm, and the length is larger than or equal to 50mm.
3. The forging deformation process test method as recited in claim 1, wherein: in the step A, the engineering deformation amount is 10 to 80 percent.
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Publication number Priority date Publication date Assignee Title
CN118761234B (en) * 2024-09-03 2024-12-03 陕西宝元特材科技有限公司 Elastic modulus optimization method and device for titanium alloy bars based on deformation characteristics analysis

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09220634A (en) * 1996-02-15 1997-08-26 Kagoshima Zunou Center:Kk Apparatus for simulating experiment of plastic working
CN1928879A (en) * 2006-09-14 2007-03-14 中国船舶重工集团公司第十二研究所 Optimizing method for forging modeling process
CN101294265A (en) * 2008-05-12 2008-10-29 中国航空工业第一集团公司北京航空材料研究院 A test method for forging process parameters of titanium alloy
CN102831265A (en) * 2012-08-10 2012-12-19 南昌航空大学 Method for analyzing and preventing forging through flow and coarse-grain defects
CN104636565A (en) * 2015-02-17 2015-05-20 扬州大学 Magnesium alloy one-off die forging forming process optimizing method based on machinability analysis
CN105512426A (en) * 2015-12-25 2016-04-20 常州大学 Design method for reducing discharging quantity of spider cold forging blank
CN109948215A (en) * 2019-03-12 2019-06-28 本钢板材股份有限公司 A kind of hot stamping process formulation method
CN112948986A (en) * 2019-12-11 2021-06-11 宝武特种冶金有限公司 Titanium alloy forging process parameter optimization method combined with finite element numerical simulation program
CN113409894A (en) * 2021-06-04 2021-09-17 燕山大学 Prediction method for microstructure change of near-alpha type titanium alloy aviation die forging

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8591674B2 (en) * 2011-11-11 2013-11-26 GM Global Technology Operations LLC Making ductility-enhanced magnesium alloy sheet materials

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09220634A (en) * 1996-02-15 1997-08-26 Kagoshima Zunou Center:Kk Apparatus for simulating experiment of plastic working
CN1928879A (en) * 2006-09-14 2007-03-14 中国船舶重工集团公司第十二研究所 Optimizing method for forging modeling process
CN101294265A (en) * 2008-05-12 2008-10-29 中国航空工业第一集团公司北京航空材料研究院 A test method for forging process parameters of titanium alloy
CN102831265A (en) * 2012-08-10 2012-12-19 南昌航空大学 Method for analyzing and preventing forging through flow and coarse-grain defects
CN104636565A (en) * 2015-02-17 2015-05-20 扬州大学 Magnesium alloy one-off die forging forming process optimizing method based on machinability analysis
CN105512426A (en) * 2015-12-25 2016-04-20 常州大学 Design method for reducing discharging quantity of spider cold forging blank
CN109948215A (en) * 2019-03-12 2019-06-28 本钢板材股份有限公司 A kind of hot stamping process formulation method
CN112948986A (en) * 2019-12-11 2021-06-11 宝武特种冶金有限公司 Titanium alloy forging process parameter optimization method combined with finite element numerical simulation program
CN113409894A (en) * 2021-06-04 2021-09-17 燕山大学 Prediction method for microstructure change of near-alpha type titanium alloy aviation die forging

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
司家勇 ; 韩鹏彪 ; 高帆 ; 张继 ; .TiAl合金高温锻造开坯过程数值模拟研究.材料工程.2009,(03),第22页至第26页,第31页. *
宗师等.燃气轮机用GH4698合金涡轮盘锻造工艺.锻造与冲压.2020,(第第7期期),第18页至第22页. *
白林振 ; 陈慧琴 ; .镦拔对Al-Zn-Mg-Cu合金变形和组织的影响.锻压技术.2011,(04),第134页至第147页. *

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