Thrust reverser having a lockable variable nozzle section
    1.
    发明授权
    Thrust reverser having a lockable variable nozzle section 有权
    具有可锁定可变喷嘴部分的推力反向器

    公开(公告)号:US08919668B2

    公开(公告)日:2014-12-30

    申请号:US13741868

    申请日:2013-01-15

    申请人: Aircelle

    摘要: The present disclosure relates to a thrust reverser including at least one translatably movable cowl capable of alternately shifting between a closed position in which same ensures the aerodynamic continuity of the nacelle and which covers the deflecting means, and an open position in which same opens a passage in the nacelle and uncovers the deflecting means, said thrust reverser likewise including at least one variable nozzle section arranged in the extension of the movable thrust-reversing cowl and provided with at least one locking means capable of engaging with a complementary locking means of the movable reversing cowl so as to optionally mechanically link the movable nozzle section of the movable reversing cowl.

    摘要翻译: 本发明涉及一种推力反向器,其包括至少一个可平移的可移动的整流罩,其能够在闭合位置之间交替地移动,在闭合位置中,该闭合位置确保机舱的空气动力学连续性并且覆盖偏转装置,并且打开位置打开通道 在所述机舱中并且露出所述偏转装置,所述推力反向器同样包括设置在所述可移动推翻反向罩的延伸部中的至少一个可变喷嘴部分,并且设置有至少一个锁定装置,所述至少一个锁定装置能够与可移动 可逆换向罩,以便可选地机械连接可移动的反向罩的可动喷嘴部分。