The present invention relates to an aircraft propulsion assembly and an aircraft comprising such an assembly, the aircraft propulsion assembly comprising an engine pylon having a top surface, an internal engine component, a possibly stationary top fairing of the engine pylon, and at least one hood, and at least one hood rotationally hinged on a rotational axis defined by at least two hinged hinges, the aircraft propulsion assembly configured such that the rotational axis of the at least two hinged hinges is positioned above the top surface of the engine pylon. Advantageously, the nacelle rectifier can thus be assembled around the internal components of the engine without an external component consisting of a fan rectifier, and the structure of the engine pylon is not changed in addition to the arrangement of the hinge fittings of the movable hood.

    本发明涉及一种飞行器推进组件和包括这种组件的飞行器,该飞行器推进组件包括发动机挂架、内部发动机部件、发动机挂架的可能的固定式顶部整流罩、以及至少一个发动机罩,该发动机挂架具有顶面,该至少一个发动机罩在由至少两个铰接铰链限定的旋转轴线上旋转铰接,所述飞行器推进组件被配置成使得所述至少两个铰接铰链的所述旋转轴线定位在所述发动机挂架的所述顶面上方。有利地,因此可以在没有由风扇整流器构成的外部部件的情况下围绕发动机的内部部件组装短舱整流器,并且除了可移动式发动机罩的铰链配件的布置之外,不改变发动机挂架的结构。


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    Title :

    Aircraft propulsion assembly and aircraft comprising such assembly


    Additional title:

    飞行器推进组件和包括这种组件的飞行器


    Contributors:

    Publication date :

    2024-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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