A propulsion assembly for an aircraft and a corresponding aircraft. The present invention relates to a propulsion assembly and an aircraft having such a propulsion assembly, the propulsion assembly having: a jet engine having an intermediate shell and a core shell aft of the intermediate shell, the intermediate shell having a rear surface; the attachment hanging frame is provided with a front wall and two lateral walls; a front engine accessory, the front engine accessory having a front fitting, the front fitting being hingedly fastened to the rear surface via two lateral fastening points and rigidly fastened to the front wall via an upper fastening region; and an intermediate engine accessory comprising, on each side, a front link and a rear link wherein each of the links is hingedly mounted between the front accessory and the lateral wall. With this arrangement, the volume of the engine accessory is reduced in the bypass flow.

    用于飞行器的推进组件和相应的飞行器。本发明涉及一种推进组件和具有这种推进组件的飞行器,推进组件具有:喷气发动机,喷气发动机具有中间外壳和在中间外壳后方的芯部外壳,中间外壳具有后表面;以及附接挂架,附接挂架具有前壁和两个侧向壁;前发动机附件,前发动机附件具有前配件,前配件经由两个侧向紧固点以铰接方式紧固到后表面,并且经由上紧固区以刚性方式紧固到前壁;以及中间发动机附件,中间发动机附件在每侧上包括前连杆和后连杆,其中,所述连杆中的每一个以铰接方式安装在前配件与侧向壁之间。利用这种布置,发动机附件的体积在旁路流中减小。


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    Title :

    Propulsion assembly for aircraft and corresponding aircraft


    Additional title:

    用于飞行器的推进组件和相应的飞行器


    Contributors:

    Publication date :

    2024-10-01


    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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