An exhaust nozzle assembly includes, but is not limited to, a nozzle body configured to be fluidly coupled with an engine and to receive a jet produced by the engine. An outer cover covers the nozzle body. A movable component is disposed and configured to have an effect on either the jet or an exhaust plume when the movable component moves. A linkage is coupled to the movable component and adapted for coupling to an actuator. The linkage transmits the force to the moveable component from the actuator. There is a gap between an inner surface of the outer cover and an outer surface of the nozzle body. The linkage is smaller than the actuator. The gap is smaller than a smallest dimension of the actuator and larger than the linkage. The linkage is partially disposed within the gap, and the exhaust nozzle assembly is free of the actuator.

    一种排气喷嘴组件包括但不限于喷嘴主体,该喷嘴主体被配置为与发动机流体地耦合并且接收由发动机产生的射流。外罩覆盖喷嘴主体。可移动部件被设置和配置为当可移动部件移动时对射流或排气羽流具有影响。联动装置耦合到可移动部件并适于耦合到致动器。联动装置将力从致动器传递到可移动部件。在外罩的内表面和喷嘴主体的外表面之间存在间隙。联动装置小于致动器。间隙小于致动器的最小尺寸并大于联动装置。联动装置部分地设置在间隙内,并且排气喷嘴组件中没有致动器。


    Access

    Download


    Export, share and cite



    Title :

    EXHAUST NOZZLE ASSEMBLY, PROPULSION SYSTEM EMPLOYING EXHAUST NOZZLE ASSEMBLY, AND AIRCRAFT EMPLOYING PROPULSION SYSTEM


    Additional title:

    排气喷嘴组件、采用其的推进系统和采用该系统的飞机


    Contributors:

    Publication date :

    2021-10-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT