RU96110803A - MULTI-STAGE TURBINE ROTOR - Google Patents
MULTI-STAGE TURBINE ROTORInfo
- Publication number
- RU96110803A RU96110803A RU96110803A RU96110803A RU96110803A RU 96110803 A RU96110803 A RU 96110803A RU 96110803 A RU96110803 A RU 96110803A RU 96110803 A RU96110803 A RU 96110803A RU 96110803 A RU96110803 A RU 96110803A
- Authority
- RU
- Russia
- Prior art keywords
- stage turbine
- turbine rotor
- disks
- shaft
- rotor
- Prior art date
Links
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU96110803A RU2130124C1 (en) | 1996-05-28 | 1996-05-28 | Multistage turbine rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU96110803A RU2130124C1 (en) | 1996-05-28 | 1996-05-28 | Multistage turbine rotor |
Publications (2)
Publication Number | Publication Date |
---|---|
RU96110803A true RU96110803A (en) | 1998-08-20 |
RU2130124C1 RU2130124C1 (en) | 1999-05-10 |
Family
ID=20181228
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU96110803A RU2130124C1 (en) | 1996-05-28 | 1996-05-28 | Multistage turbine rotor |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2130124C1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2904048B1 (en) * | 2006-07-19 | 2012-12-14 | Snecma | COMBUSTION CHAMBER WALL VENTILATION SYSTEM IN TURBOMACHINE |
FR2904037B1 (en) * | 2006-07-19 | 2010-11-12 | Snecma | VENTILATION OF A DOWNWARD CAVITY OF CENTRIFUGAL COMPRESSOR WHEEL |
FR2904047B1 (en) * | 2006-07-19 | 2013-03-01 | Snecma | COMBUSTION CHAMBER WALL VENTILATION SYSTEM |
RU2532390C1 (en) * | 2013-09-10 | 2014-11-10 | Открытое акционерное общество "Авиадвигатель" | High-pressure turbine rotor |
RU2614018C1 (en) * | 2016-03-22 | 2017-03-22 | Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") | Rotor shaft bearing of low-pressure compressor of turbojet engine (versions), cylinder constituent of rotor shaft, external tightening component of rotor shaft |
RU2661566C2 (en) * | 2016-12-28 | 2018-07-17 | Акционерное общество "ОДК-Авиадвигатель" | Multistage turbine rotor |
US11629596B1 (en) | 2021-10-08 | 2023-04-18 | Pratt & Whitney Canada Corp. | Rotor assembly for a gas turbine engine and method for assembling same |
-
1996
- 1996-05-28 RU RU96110803A patent/RU2130124C1/en active
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