发明授权
US5082182A Thrust vectoring exhaust nozzle 失效
THRUST VECTORING EXHAUST NOZZLE

Thrust vectoring exhaust nozzle
摘要:
An axisymmetric thrust vectoring exhaust nozzle includes a plurality of divergent flaps (30) each supported at the upstream end by a universal joint (32) and at the downstream end by a load link (34) connected to a unison ring (36) positioned by actuators (45).
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