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
Title |
Year |
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