EXHAUST DEVICE OF AIR-JET VECTORED-THRUST ENGINE Russian patent published in 2006 - IPC F02K1/38 

Abstract RU 2276740 C2

FIELD: air-jet engines.

SUBSTANCE: invention relates to ejector exhaust devices of vectored-thrust air-jet engines. Proposed exhaust device of air-jet engine has nozzle and ejector arranged after nozzle. Ejector contains chamber and circular air intake with ports and controlled gates installed for overlapping the ports to prevent ingress of atmospheric air. Controlled gates are arranged in each port being operated by independent drives to overlap opposite ports or one port, or three ports simultaneously, or partial closing of one port.

EFFECT: enlarged operating capabilities of aircraft engines.

9 dwg

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RU 2 276 740 C2

Authors

Dates

2006-05-20Published

2000-12-13Filed