RU2003113572A - METHOD OF PROCESSING MONOCOLES - Google Patents
METHOD OF PROCESSING MONOCOLES Download PDFInfo
- Publication number
- RU2003113572A RU2003113572A RU2003113572/02A RU2003113572A RU2003113572A RU 2003113572 A RU2003113572 A RU 2003113572A RU 2003113572/02 A RU2003113572/02 A RU 2003113572/02A RU 2003113572 A RU2003113572 A RU 2003113572A RU 2003113572 A RU2003113572 A RU 2003113572A
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- RU
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- workpiece
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- processing
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Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2003113572/02A RU2247011C2 (en) | 2003-05-08 | 2003-05-08 | Method for working one-piece impellers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2003113572/02A RU2247011C2 (en) | 2003-05-08 | 2003-05-08 | Method for working one-piece impellers |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2003113572A true RU2003113572A (en) | 2005-01-27 |
RU2247011C2 RU2247011C2 (en) | 2005-02-27 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2003113572/02A RU2247011C2 (en) | 2003-05-08 | 2003-05-08 | Method for working one-piece impellers |
Country Status (1)
Country | Link |
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RU (1) | RU2247011C2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2482940C1 (en) * | 2011-10-28 | 2013-05-27 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Method of machining gas turbine engine blisk |
CN112404913A (en) * | 2020-10-13 | 2021-02-26 | 中国航发沈阳黎明航空发动机有限责任公司 | Titanium alloy blisk blade processing technology method |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2625860C1 (en) * | 2016-11-07 | 2017-07-19 | Научно-производственная Ассоциация "Технопарк авиационных технологий" (НПА "Технопарк АТ") | Method of manufacture of integrally-machined rotor of gas turbine engine |
CN106513804B (en) * | 2016-11-29 | 2019-07-05 | 中国航发沈阳黎明航空发动机有限责任公司 | A kind of high temperature alloy entirety leaf joint blade milling method |
RU2648174C1 (en) * | 2017-06-06 | 2018-03-22 | Акционерное общество "ОДК-Авиадвигатель" | Method of treatment of a radial end groove on the parts of a gas turbine engine (options) |
-
2003
- 2003-05-08 RU RU2003113572/02A patent/RU2247011C2/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2482940C1 (en) * | 2011-10-28 | 2013-05-27 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Method of machining gas turbine engine blisk |
CN112404913A (en) * | 2020-10-13 | 2021-02-26 | 中国航发沈阳黎明航空发动机有限责任公司 | Titanium alloy blisk blade processing technology method |
Also Published As
Publication number | Publication date |
---|---|
RU2247011C2 (en) | 2005-02-27 |
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