An aircraft engine nacelle is provided with a thrust reverser having a movable injection structure. -said nacelle (1) comprises a thrust reverser (7) having a translatably movable cowl (10) and a jet structure (9) also translatably movable and forming, together with the cowl (10), a movement assembly (17) configured to be alternately movable into a closed position in which the jet structure (9) can be moved in parallel and into an open position (P2) in which the jet structure (9) can be moved in parallel with the cowl (10); the injection structure (9) is inserted into a housing (18) formed in the nacelle (1) and the fairing (10) closes an injection opening (12) in the nacelle (1), and an open position in which the fairing (10) releases the injection opening (12) in the nacelle (1) and the injection structure (9) is located in the injection opening (12), the positioning of the injection structure (9) in the housing (18) in the closed position makes it possible, in particular, to create a space in the injection opening (12) and to reduce the size of the thrust reverser (7).

    设置有具有活动喷射结构的推力反向器的飞行器发动机短舱。‑所述短舱(1)包括推力反向器(7),该推力反向器(7)具有能够平移地移动的整流罩(10)和也能够平移地移动并且与整流罩(10)一起形成移动组件(17)的喷射结构(9),所述移动组件(17)构造成能够交替地移动到关闭位置和打开位置(P2)中,在关闭位置中,喷射结构(9)被插入到形成在短舱(1)中的外壳(18)中,并且整流罩(10)关闭短舱(1)中的喷射开口(12),在打开位置中,整流罩(10)释放短舱(1)中的喷射开口(12),并且喷射结构(9)位于该喷射开口(12)中,喷射结构(9)在关闭位置中在外壳(18)中的定位使得特别是在喷射开口(12)中营造出空间并减小推力反向器(7)的尺寸成为可能。


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    Title :

    Aircraft nacelle provided with thrust reverser having movable injection structure


    Additional title:

    设置有具有活动喷射结构的推力反向器的飞行器发动机短舱


    Contributors:

    Publication date :

    2023-12-15


    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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