RU2000113307A - COMPRESSOR OF A GAS TURBINE ENGINE - Google Patents
COMPRESSOR OF A GAS TURBINE ENGINEInfo
- Publication number
- RU2000113307A RU2000113307A RU2000113307/06A RU2000113307A RU2000113307A RU 2000113307 A RU2000113307 A RU 2000113307A RU 2000113307/06 A RU2000113307/06 A RU 2000113307/06A RU 2000113307 A RU2000113307 A RU 2000113307A RU 2000113307 A RU2000113307 A RU 2000113307A
- Authority
- RU
- Russia
- Prior art keywords
- gas turbine
- turbine engine
- compressor
- bypass valves
- bypass
- Prior art date
Links
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000113307A RU2189499C2 (en) | 2000-05-26 | 2000-05-26 | Gas-turbine engine compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000113307A RU2189499C2 (en) | 2000-05-26 | 2000-05-26 | Gas-turbine engine compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2000113307A true RU2000113307A (en) | 2002-04-10 |
RU2189499C2 RU2189499C2 (en) | 2002-09-20 |
Family
ID=20235239
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2000113307A RU2189499C2 (en) | 2000-05-26 | 2000-05-26 | Gas-turbine engine compressor |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2189499C2 (en) |
-
2000
- 2000-05-26 RU RU2000113307A patent/RU2189499C2/en active
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