FIELD: gas- turbine engine engineering. SUBSTANCE: nozzle has adapter 1 mounted on housing 2 and having two side walls 3 and shutters 5 and 6 the front ends of which are connected to side walls 3 through levers 7, the middle part of the shutters being connected with the side walls through telescopic ties. Hollow central body 4 is interposed between shutters 5 and 6. The space of the central body is in communication with the atmosphere through passageways made in side walls 3 and with the flowing part of the nozzle through lateral slots made in the surface of the central body and facing shutters 5 and 6. EFFECT: improved design. 2 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
PLANAR NOZZLE WITH CENTRAL BODY | 1995 |
|
RU2153591C2 |
AIR-JET ENGINE EXIT TWO-DIMENSIONAL NOZZLE | 2001 |
|
RU2187681C1 |
TWO-DIMENSIONAL EXIT NOZZLE FOR AIR-JET ENGINE | 2001 |
|
RU2182672C1 |
OUTPUT DEVICE OF A TURBOJET ENGINE | 2023 |
|
RU2807307C1 |
STEALTH SHORT TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2705416C2 |
SUPERSONIC AIRCRAFT | 2020 |
|
RU2753443C1 |
FLAT OUTPUT DEVICE OF THREE-LOOP GAS TURBINE ENGINE OF VARIABLE CYCLE | 2018 |
|
RU2686535C1 |
TURBOJET ENGINE NOZZLE FLAPS SYNCHRONIZING SYSTEM | 2006 |
|
RU2317432C1 |
NOISE-SUPPRESSING NOZZLE OF AIR-JET ENGINE | 2019 |
|
RU2732360C1 |
SUPERSONIC LOW-PROFILE PLANE OF VERTICAL TAKE-OFF AND LANDING | 2018 |
|
RU2682054C1 |
Authors
Dates
1995-08-27—Published
1990-05-03—Filed