RU92003195A - AIRCRAFT WITH FLOW LAMINARIZATION SYSTEM - Google Patents
AIRCRAFT WITH FLOW LAMINARIZATION SYSTEMInfo
- Publication number
- RU92003195A RU92003195A RU92003195/11A RU92003195A RU92003195A RU 92003195 A RU92003195 A RU 92003195A RU 92003195/11 A RU92003195/11 A RU 92003195/11A RU 92003195 A RU92003195 A RU 92003195A RU 92003195 A RU92003195 A RU 92003195A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- combustion chamber
- aircraft
- auxiliary circuit
- turbine
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims 5
- 238000010438 heat treatment Methods 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU92003195A RU2084377C1 (en) | 1992-11-02 | 1992-11-02 | Power plant of flying vehicle with laminar-flow control system of aerodynamic surfaces |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU92003195A RU2084377C1 (en) | 1992-11-02 | 1992-11-02 | Power plant of flying vehicle with laminar-flow control system of aerodynamic surfaces |
Publications (2)
Publication Number | Publication Date |
---|---|
RU92003195A true RU92003195A (en) | 1997-01-27 |
RU2084377C1 RU2084377C1 (en) | 1997-07-20 |
Family
ID=20131316
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU92003195A RU2084377C1 (en) | 1992-11-02 | 1992-11-02 | Power plant of flying vehicle with laminar-flow control system of aerodynamic surfaces |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2084377C1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10361390B4 (en) | 2003-12-29 | 2008-05-08 | Airbus Deutschland Gmbh | Method and device for extracting the boundary layer |
DE102004024057B3 (en) | 2004-05-13 | 2005-09-15 | Airbus Deutschland Gmbh | Aircraft, has fluid duct system connected to pumping device that is driven, by cabin exhaust air, for production of low pressure for suction of boundary layer though valve, where device is jet pump whose driving jets are generated by air |
DE102004024016A1 (en) | 2004-05-13 | 2005-12-22 | Airbus Deutschland Gmbh | Air suction arrangement for aircraft, has branch line to draw bleed air from high-pressure region of engine so as to drive turbine of turbo-supercharger |
CN103184936B (en) * | 2011-12-31 | 2016-08-03 | 朱晓义 | A kind of electromotor and a kind of aircraft |
RU2523510C1 (en) * | 2013-02-19 | 2014-07-20 | Николай Евгеньевич Староверов | Method of gas turbine engine afterburning |
-
1992
- 1992-11-02 RU RU92003195A patent/RU2084377C1/en active
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