发明名称 REDUCED WEIGHT NOZZLE ACTUATION MECHANISM
摘要 13DV09910 A fluid supply and synchronizing mechanism are provided for a jet engine exhaust nozzle. The exhaust nozzle has flaps which are moved by flap mounted actuators which move with the flaps. The fluid supply includes a supply tube, a return tube and a strut for each actuator. The two tubes and strut are connected to each actuator for movement with the actuator. The strut prevents flexing of the tubes during movement The synchronizing mechanism interconnects the flaps so that movement of any one flap is transmitted to all other flaps thereby retaining nozzle symmetry.
申请公布号 CA2062925(A1) 申请公布日期 1992.10.16
申请号 CA19922062925 申请日期 1992.03.12
申请人 GENERAL ELECTRIC COMPANY 发明人 NASH, DUDLEY O.
分类号 F02K1/08;F02K1/12;F02K1/15;(IPC1-7):F02K1/12;F02K1/18 主分类号 F02K1/08
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