CN111036810B - 一种高温合金锻造及热处理方法 - Google Patents
一种高温合金锻造及热处理方法 Download PDFInfo
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- CN111036810B CN111036810B CN201911266620.9A CN201911266620A CN111036810B CN 111036810 B CN111036810 B CN 111036810B CN 201911266620 A CN201911266620 A CN 201911266620A CN 111036810 B CN111036810 B CN 111036810B
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- 238000005242 forging Methods 0.000 title claims abstract description 74
- 239000000956 alloy Substances 0.000 title claims abstract description 33
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 32
- 238000010438 heat treatment Methods 0.000 title claims abstract description 17
- 238000000034 method Methods 0.000 title claims abstract description 15
- 238000004321 preservation Methods 0.000 claims abstract description 24
- 238000000137 annealing Methods 0.000 claims abstract description 19
- 230000032683 aging Effects 0.000 claims abstract description 17
- 239000002994 raw material Substances 0.000 claims abstract description 10
- 239000006104 solid solution Substances 0.000 claims abstract description 10
- 229910000601 superalloy Inorganic materials 0.000 claims description 21
- 239000000243 solution Substances 0.000 claims description 7
- 238000011056 performance test Methods 0.000 claims description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 238000005457 optimization Methods 0.000 abstract 1
- 239000010936 titanium Substances 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 5
- 239000013078 crystal Substances 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000004090 dissolution Methods 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 229910001247 waspaloy Inorganic materials 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QISGROBHHFQWKS-UHFFFAOYSA-N [C].[Nb] Chemical compound [C].[Nb] QISGROBHHFQWKS-UHFFFAOYSA-N 0.000 description 1
- VQYPKWOGIPDGPN-UHFFFAOYSA-N [C].[Ta] Chemical class [C].[Ta] VQYPKWOGIPDGPN-UHFFFAOYSA-N 0.000 description 1
- CYKMNKXPYXUVPR-UHFFFAOYSA-N [C].[Ti] Chemical compound [C].[Ti] CYKMNKXPYXUVPR-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 235000013619 trace mineral Nutrition 0.000 description 1
- 239000011573 trace mineral Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/003—Selecting material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/06—Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/002—Hybrid process, e.g. forging following casting
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Forging (AREA)
Abstract
Description
试样编号 | 加热温度 | 变形量 | 晶粒度 | 试样编号 | 加热温度 | 变形量 | 晶粒度 |
1 | 1000℃ | 10% | 5-6级 | 5 | 1140℃ | 10% | 4.5级 |
2 | 1000℃ | 30% | 6级 | 6 | 1140℃ | 30% | 4级 |
3 | 1040℃ | 10% | 6级 | 7 | 1160℃ | 10% | 3.5级 |
4 | 1040℃ | 30% | 6级 | 8 | 1160℃ | 30% | 3级 |
编号 | 保温温度 | 保温时间 | 晶粒度 | 编号 | 保温温度 | 保温时间 | 晶粒度 |
1 | 1000℃ | 60min | 6.5级 | 5 | 1140℃ | 60min | 5级 |
2 | 1000℃ | 120min | 6.5级 | 6 | 1140℃ | 120min | 4级 |
3 | 1040℃ | 60min | 6级 | 7 | 1160℃ | 60min | 5级 |
4 | 1040℃ | 120min | 6级 | 8 | 1160℃ | 120min | 2级 |
试样编号 | 加热温度 | 变形量 | 保温温度 | 保温时间 | 晶粒度 |
1 | 1060℃ | 10% | 1080 | 60min | 5级 |
2 | 1060℃ | 30% | 1080 | 60min | 5-6级 |
3 | 1100℃ | 10% | 1120 | 60min | 4.5级 |
4 | 1100℃ | 30% | 1120 | 60min | 4级 |
Claims (6)
Priority Applications (1)
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CN201911266620.9A CN111036810B (zh) | 2019-12-11 | 2019-12-11 | 一种高温合金锻造及热处理方法 |
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CN201911266620.9A CN111036810B (zh) | 2019-12-11 | 2019-12-11 | 一种高温合金锻造及热处理方法 |
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CN111036810A CN111036810A (zh) | 2020-04-21 |
CN111036810B true CN111036810B (zh) | 2022-05-13 |
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Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111549259B (zh) * | 2020-05-25 | 2021-06-04 | 中国科学院金属研究所 | 一种镍钴基高温合金涡轮盘及其制备方法 |
CN113234964B (zh) * | 2021-05-19 | 2021-12-03 | 山西太钢不锈钢股份有限公司 | 一种镍基耐蚀合金及其加工方法 |
CN113234963B (zh) * | 2021-05-19 | 2021-12-17 | 沈阳航空航天大学 | 室温以及低温环境用镍铬基超合金及其制备方法 |
CN113759090B (zh) * | 2021-09-23 | 2022-07-19 | 湖南大学 | 消除锻造和热处理影响的锻造试验方法 |
CN114317904B (zh) * | 2022-01-05 | 2024-01-19 | 无锡派克新材料科技股份有限公司 | 一种航空发动机用沉淀硬化高温合金锻件成型方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6233500B1 (en) * | 1997-06-19 | 2001-05-15 | The United States Of America As Represented By The Secretary Of The Air Force | Optimization and control of microstructure development during hot metal working |
CN104732012A (zh) * | 2015-02-13 | 2015-06-24 | 西北工业大学 | Gh4169合金锻件晶粒度与锻造热力参数关系的建立方法 |
CN105631160A (zh) * | 2016-01-30 | 2016-06-01 | 西北工业大学 | Tc4合金锻件室温力学性能的预报方法 |
CN107245683A (zh) * | 2017-06-08 | 2017-10-13 | 太原钢铁(集团)有限公司 | 镍基合金径锻组织控制方法 |
CN109504875A (zh) * | 2018-11-05 | 2019-03-22 | 贵州大学 | 一种获得高性能钛合金不同层次组织的热处理方法 |
-
2019
- 2019-12-11 CN CN201911266620.9A patent/CN111036810B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6233500B1 (en) * | 1997-06-19 | 2001-05-15 | The United States Of America As Represented By The Secretary Of The Air Force | Optimization and control of microstructure development during hot metal working |
CN104732012A (zh) * | 2015-02-13 | 2015-06-24 | 西北工业大学 | Gh4169合金锻件晶粒度与锻造热力参数关系的建立方法 |
CN105631160A (zh) * | 2016-01-30 | 2016-06-01 | 西北工业大学 | Tc4合金锻件室温力学性能的预报方法 |
CN107245683A (zh) * | 2017-06-08 | 2017-10-13 | 太原钢铁(集团)有限公司 | 镍基合金径锻组织控制方法 |
CN109504875A (zh) * | 2018-11-05 | 2019-03-22 | 贵州大学 | 一种获得高性能钛合金不同层次组织的热处理方法 |
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Denomination of invention: A method for forging and heat treatment of superalloy Effective date of registration: 20221219 Granted publication date: 20220513 Pledgee: Guizhou Branch of Export Import Bank of China Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2022520000055 |
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Denomination of invention: A Method for Forging and Heat Treatment of High Temperature Alloys Effective date of registration: 20231109 Granted publication date: 20220513 Pledgee: Guizhou Branch of Export Import Bank of China Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2023520000064 |