RU2016146883A3 - - Google Patents
Download PDFInfo
- Publication number
- RU2016146883A3 RU2016146883A3 RU2016146883A RU2016146883A RU2016146883A3 RU 2016146883 A3 RU2016146883 A3 RU 2016146883A3 RU 2016146883 A RU2016146883 A RU 2016146883A RU 2016146883 A RU2016146883 A RU 2016146883A RU 2016146883 A3 RU2016146883 A3 RU 2016146883A3
- Authority
- RU
- Russia
Links
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2016146883A RU2662755C2 (en) | 2016-11-29 | 2016-11-29 | Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2016146883A RU2662755C2 (en) | 2016-11-29 | 2016-11-29 | Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor |
Publications (3)
Publication Number | Publication Date |
---|---|
RU2016146883A RU2016146883A (en) | 2018-05-29 |
RU2016146883A3 true RU2016146883A3 (en) | 2018-05-29 |
RU2662755C2 RU2662755C2 (en) | 2018-07-30 |
Family
ID=62557568
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2016146883A RU2662755C2 (en) | 2016-11-29 | 2016-11-29 | Place of mounting of working blades of booster rotors and compressor of aviation engines of fifth generation; booster rotor and rotor of high pressure compressor of first generation aviation engine, with working blades, fixed with help of swallowtail type locks in ring grooves of these devices; method of assembling place of mounting working blades of booster rotors and compressor |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2662755C2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2740442C2 (en) * | 2019-06-27 | 2021-01-14 | федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королёва" | Axle compressor blisk and rotor of low-pressure compressor of aircraft gas turbine engine |
CN117346635B (en) * | 2023-12-06 | 2024-03-12 | 成都格瑞特高压容器有限责任公司 | Outer diameter measuring device and measuring method for cylindrical gas cylinder |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU641129A1 (en) * | 1976-03-03 | 1979-01-05 | Куйбышевский Ордена Трудового Красного Знамени Авиационный Институт Имени Академика С.П.Королева | Turbomachine blade |
US5518369A (en) * | 1994-12-15 | 1996-05-21 | Pratt & Whitney Canada Inc. | Gas turbine blade retention |
FR2945074B1 (en) * | 2009-04-29 | 2011-06-03 | Snecma | REINFORCED BLOW OF BREATHING BLADE |
RU2570087C1 (en) * | 2014-08-22 | 2015-12-10 | Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" | Impeller of rotor of gas turbine engine with dampening of vibration oscillations |
-
2016
- 2016-11-29 RU RU2016146883A patent/RU2662755C2/en active IP Right Revival
Also Published As
Publication number | Publication date |
---|---|
RU2662755C2 (en) | 2018-07-30 |
RU2016146883A (en) | 2018-05-29 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20181130 |
|
NF4A | Reinstatement of patent |
Effective date: 20210713 |