公开(公告)号：US4456203A

公开(公告)日：1984-06-26

申请号：US403957

申请日：1982-08-02

申请人： John D. Louthan

发明人： John D. Louthan

IPC分类号： B64D33/04 ,  B64C15/02

CPC分类号： B64D33/04

摘要： An aircraft propulsion system is disclosed having an exhaust nozzle structure having an exhaust deflection structure extending within an exhaust duct to direction exhaust flow along selected flow paths. In its preferred embodiment, the exhaust deflection structure is a variable geometry deflection structure having a distal end portion which is movable, relative to adjacent aircraft structure, within an exhaust duct whereby the exhaust deflection structure is positionable as an extension of an upper, aft wall portion of the exhaust duct. In the preferred embodiment, the exhaust nozzle structure includes a guide structure or nozzle segment, connected to the exhaust deflection structure, which is translatably mounted to adjacent aircraft structure for permitting fore and aft movement of the nozzle segment along the aircraft structure.

摘要翻译： 公开了一种具有排气喷嘴结构的飞行器推进系统，该排气喷嘴结构具有在排气管道内延伸的排气偏转结构，沿着选定的流动路径排向流动方向。 在其优选实施例中，排气偏转结构是可变几何偏转结构，其具有可相对于相邻的飞行器结构在排气管道内移动的远端部分，由此排气偏转结构可定位成上，后壁的延伸部 排气管道的一部分。 在优选实施例中，排气喷嘴结构包括连接到排气偏转结构的引导结构或喷嘴段，其可平移地安装到相邻的飞行器结构，以允许喷嘴段沿着飞行器结构的前后移动。