FIELD: axisymmetric swivel nozzles for turbo-jet engines.
SUBSTANCE: proposed swivel axisymmetric nozzle has fixed body with spherical tip and swivel unit which is turnable relative to axle mounted across longitudinal axis of engine; it is made in form of supersonic adjustable nozzle with pneumatic systems connected with respective systems of engine by means of pneumatic and hydraulic change-over systems which are located in area of axis of turn of swivel unit.
EFFECT: extended range of operation; enhanced operational reliability.
3 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET ENGINE AXIS SYMMETRICAL TURNING NOZZLE | 2017 |
|
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