CN103433364A - Thermal-bulging forming method of high-temperature alloy rectangular section ring unit - Google Patents
Thermal-bulging forming method of high-temperature alloy rectangular section ring unit Download PDFInfo
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- CN103433364A CN103433364A CN2013103888566A CN201310388856A CN103433364A CN 103433364 A CN103433364 A CN 103433364A CN 2013103888566 A CN2013103888566 A CN 2013103888566A CN 201310388856 A CN201310388856 A CN 201310388856A CN 103433364 A CN103433364 A CN 103433364A
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- bulging
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- temperature alloy
- ring unit
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- 239000000956 alloy Substances 0.000 title claims abstract description 35
- 238000000034 method Methods 0.000 title claims abstract description 33
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 32
- 238000009792 diffusion process Methods 0.000 claims description 5
- 238000010586 diagram Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000005096 rolling process Methods 0.000 description 4
- 230000007613 environmental effect Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 208000037656 Respiratory Sounds Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000000205 computational method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000029087 digestion Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000011112 process operation Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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CN201310388856.6A CN103433364B (en) | 2013-09-01 | 2013-09-01 | The Thermal expansion manufacturing process of high temperature alloy square-section annular part |
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CN201310388856.6A CN103433364B (en) | 2013-09-01 | 2013-09-01 | The Thermal expansion manufacturing process of high temperature alloy square-section annular part |
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CN103433364A true CN103433364A (en) | 2013-12-11 |
CN103433364B CN103433364B (en) | 2015-08-05 |
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CN201310388856.6A Active CN103433364B (en) | 2013-09-01 | 2013-09-01 | The Thermal expansion manufacturing process of high temperature alloy square-section annular part |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115069902A (en) * | 2022-06-13 | 2022-09-20 | 中国航发北京航空材料研究院 | Method for reducing quenching residual stress of large 7050 aluminum alloy annular forging |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2647463Y (en) * | 2003-09-23 | 2004-10-13 | 克拉玛依康佳实业有限责任公司 | Expanding shape machine |
CN101020284A (en) * | 2007-03-05 | 2007-08-22 | 贵州安大航空锻造有限责任公司 | Blank making method of high-temperature alloy large-scale special-shaped section ring blank |
RU2323058C1 (en) * | 2006-07-12 | 2008-04-27 | ООО Научно-внедренческий центр "Машины и оборудование для энергетики" | Outer thread forming method on end portion of tube blank |
CN101279349A (en) * | 2008-04-23 | 2008-10-08 | 贵州航宇科技发展有限公司 | Rolling forming method of nickel-base superalloy tapered ring forgings |
CN102500705A (en) * | 2011-11-24 | 2012-06-20 | 贵州安大航空锻造有限责任公司 | Method for thermally bulging high-temperature alloy rectangular ring rolled member |
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2013
- 2013-09-01 CN CN201310388856.6A patent/CN103433364B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2647463Y (en) * | 2003-09-23 | 2004-10-13 | 克拉玛依康佳实业有限责任公司 | Expanding shape machine |
RU2323058C1 (en) * | 2006-07-12 | 2008-04-27 | ООО Научно-внедренческий центр "Машины и оборудование для энергетики" | Outer thread forming method on end portion of tube blank |
CN101020284A (en) * | 2007-03-05 | 2007-08-22 | 贵州安大航空锻造有限责任公司 | Blank making method of high-temperature alloy large-scale special-shaped section ring blank |
CN101279349A (en) * | 2008-04-23 | 2008-10-08 | 贵州航宇科技发展有限公司 | Rolling forming method of nickel-base superalloy tapered ring forgings |
CN102500705A (en) * | 2011-11-24 | 2012-06-20 | 贵州安大航空锻造有限责任公司 | Method for thermally bulging high-temperature alloy rectangular ring rolled member |
Non-Patent Citations (1)
Title |
---|
张涛 等: "TA15 钛合金小圆角梯形截面环热成形技术", 《张涛 等》 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115069902A (en) * | 2022-06-13 | 2022-09-20 | 中国航发北京航空材料研究院 | Method for reducing quenching residual stress of large 7050 aluminum alloy annular forging |
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CN103433364B (en) | 2015-08-05 |
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PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Thermal-bulging forming method of high-temperature alloy rectangular section ring unit Effective date of registration: 20170425 Granted publication date: 20150805 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: 2017990000341 |
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PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20200915 Granted publication date: 20150805 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: 2017990000341 |
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PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Hot bulging forming method of Superalloy rectangular section annular parts Effective date of registration: 20200921 Granted publication date: 20150805 Pledgee: Guanshanhu sub branch of Guiyang Bank Co.,Ltd. Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2020980006270 |
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PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230322 Granted publication date: 20150805 Pledgee: Guanshanhu sub branch of Guiyang Bank Co.,Ltd. Pledgor: Guizhou Aviation Technical Development Co.,Ltd. Registration number: Y2020980006270 |