An engine pylon for fastening an engine of an aircraft and a corresponding aircraft. The invention relates to an engine pylon and a corresponding aircraft. The engine pylon has a structure for securing an aircraft engine beneath a wing and having two lateral surfaces. The structural body has a channel between these lateral faces passing therethrough, and the engine pylon has a spreader housed in the channel and hingedly fastened to each lateral face, where a first end of the spreader has a first hole and where a second end of the spreader has two second holes, and a rod housed in the channel and hingedly fastened to each lateral face, where the first end of the spreader has a second hole and where the second end of the spreader has a second hole. Each second bore forms a connection point with the engine, and a lever is hingedly secured to the first bore and has two third bores, each forming a connection point with the engine. Thus, such an engine pylon has the ability to attach the engine, with reduced vertical volume and less resistance.

    用于紧固飞行器的发动机的发动机吊挂架和相应的飞行器。本发明涉及发动机吊挂架和相应的飞行器。该发动机吊挂架具有用于将飞行器发动机紧固在机翼下方并具有两个侧向面的结构体。结构体具有在这些侧向面之间穿其而过的通道,并且发动机吊挂架具有吊具和杆,该吊具容置在通道中并且以铰接方式紧固到每个侧向面,其中吊具的第一端具有第一孔,并且其中吊具的第二端具有两个第二孔,每个第二孔形成与发动机的连接点,杆以铰接方式紧固到第一孔并具有两个第三孔,每个第三孔形成与发动机的连接点。因此,这种发动机吊挂架具有附接该发动机的能力,具有减小的竖直体积和较小的阻力。


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    Titel :

    Engine pylon for fastening engine of aircraft and corresponding aircraft


    Weitere Titelangaben:

    用于紧固飞行器的发动机的发动机吊挂架和相应的飞行器


    Beteiligte:

    Erscheinungsdatum :

    15.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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