FIELD: air transport.
SUBSTANCE: suction system includes as minimum one air-breathing by-pass engine, high pressure compressor with high pressure area in internal circuit, dropout line and charging turbine set. The engine has internal and external circuits and main flow. Dropout line is purposed for air venting from high pressure area of by-pass engine and for turbine driving of charging turbine set by vented air. Compressor is purposed for creation of suction force required for boundary-layer suction. Pressure line of charging turbine set compressor is opened into main flow of by-pass engine in low pressure area.
EFFECT: increase in reliability, energy efficiency of the system.
5 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR SUCTION OF BOUNDARY LAYER AND FOR MONITORING OF SHOCK BOUNDARY LAYER FOR AIRCRAFT | 1999 |
|
RU2168445C2 |
| AIRBORNE VEHICLE PART | 2005 |
|
RU2362708C2 |
| AIRCRAFT | 2005 |
|
RU2389648C2 |
| TRANSPORT AIRCRAFT WITH BLUNTED TAIL SECTION OF FUSELAGE | 1994 |
|
RU2094307C1 |
| AIRCRAFT WITH GAS TURBINE ENGINE PROVIDED WITH TURBULENCE EJECTION PROPULSORS | 2013 |
|
RU2567914C2 |
| AIRCRAFT POWER PLANT | 2023 |
|
RU2815564C1 |
| FLYING VEHICLE | 2004 |
|
RU2261823C1 |
| STREAMLINED BODY, PRIMARILY FOR AIRCRAFT | 2010 |
|
RU2496680C1 |
| AIRCRAFT WITH TURBOJET ENGINE WITH OPPOSITE ROTATION FANS | 2013 |
|
RU2641955C2 |
| PERFORATED OUTER SURFACE OF ROTATION BODY WITH COMBINED HOLES AND SUCTION CHANNEL | 2020 |
|
RU2734664C1 |
