发明授权
US3979067A Actuating means for a thrust vectoring gas turbine engine exhaust nozzle 失效
用于推力矢量燃气涡轮发动机排气喷嘴的致动装置

Actuating means for a thrust vectoring gas turbine engine exhaust nozzle
摘要:
A thrust vectoring gas turbine exhaust nozzle is provided with cooperating variable internal coverging-diverging flaps to provide nozzle flow path area control. A vertical take-off and landing capability is obtained by deployment of a rotating bonnet-type deflector which diverts the exhaust stream downward around one side of the exhaust nozzle. Actuating means are provided to rotate the nozzle throat simultaneously with deflector rotation to produce efficient turning of the exhaust stream in the lift mode. The actuation means also simultaneously controls the nozzle flow path area and external exhaust expansion in the cruise mode.
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