发明名称 Thrust reverser-cascade two door pre-exit
摘要 A thrust reverser for a fan jet engine enclosed by an engine nacelle. The nacelle has a forward section fixed to the aircraft structure and a rearward translatable section attached to the forward section. The nacelle forming a secondary fan nozzle. A pair of blocker doors are pivotally attached to the rearward translatable nacelle section. Drag links are pivotally attached to the forward nacelle section and one of the drag link connects to each blocker door. A cascade ring is fixedly attached to the rear nacelle section and is translatable therewith for positioning within the opening between the nacelle portions when the rearward section is in a translated position. An air motor with drive connections to a plurality of ball-screw actuators provides the means for uniformly translating the rearward section. A recess in the inner surface of the rearward section is provided for the stowing of the links in a position out of the engine gas flow stream when the rearward section is in its stowed forward position.
申请公布号 US4185798(A) 申请公布日期 1980.01.29
申请号 US19780885774 申请日期 1978.03.13
申请人 ROHR INDUSTRIES INC 发明人 DICKENSON, ROBERT
分类号 F02K1/60;(IPC1-7):B64C15/04 主分类号 F02K1/60
代理机构 代理人
主权项
地址