Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle
    1.
    发明授权
    Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle 有权
    用于具有滑动盖的推力反向器的锁定/解锁装置和用于飞机发动机机舱的自适应喷嘴

    公开(公告)号:US08833055B2

    公开(公告)日:2014-09-16

    申请号:US13801813

    申请日:2013-03-13

    Applicant: Aircelle

    CPC classification number: F02K1/766 F02K1/09 F02K1/72 Y02T50/671

    Abstract: A locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle is provided that includes a fixed pin secured to a fixed structure of the reverser, a first sleeve secured to the sliding cover and able to accommodate the pin, a second sleeve slidably mounted on the first sleeve, a third sleeve secured to the adaptive nozzle and slidably mounted on the second sleeve, first locking means able to lock the first sleeve with respect to the pin, second locking means able to lock the second sleeve with respect to the first sleeve, and third locking means able to lock the third sleeve with respect to the second sleeve.

    Abstract translation: 提供一种用于具有滑动盖和自适应喷嘴的​​推力反向器的锁定/解锁装置,其包括固定到反向器的固定结构的固定销,固定到滑动盖并能够容纳销的第一套筒,可滑动地 安装在第一套筒上,第三套筒固定到自适应喷嘴并可滑动地安装在第二套筒上,第一锁定装置能够相对于销锁定第一套筒,第二锁定装置能够相对于第二套筒锁定第二套筒 第一套筒和第三锁定装置能够相对于第二套筒锁定第三套筒。

    Thrust reverser having a lockable variable nozzle section
    2.
    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

    Applicant: Aircelle

    Abstract: 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.

    Abstract translation: 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。

    LOCKING/UNLOCKING DEVICE FOR A THURST REVERSER WITH A SLIDING COVER AND ADAPTIVE NOZZLE FOR AIRCRAFT ENGINE NACELLE
    3.
    发明申请
    LOCKING/UNLOCKING DEVICE FOR A THURST REVERSER WITH A SLIDING COVER AND ADAPTIVE NOZZLE FOR AIRCRAFT ENGINE NACELLE 有权
    用于具有滑盖的颠倒装置和用于飞机发动机的自适应喷嘴的​​锁定/解锁装置

    公开(公告)号:US20140000238A1

    公开(公告)日:2014-01-02

    申请号:US13801813

    申请日:2013-03-13

    Applicant: AIRCELLE

    CPC classification number: F02K1/766 F02K1/09 F02K1/72 Y02T50/671

    Abstract: A locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle is provided that includes a fixed pin secured to a fixed structure of the reverser, a first sleeve secured to the sliding cover and able to accommodate the pin, a second sleeve slidabiy mounted on the first sleeve, a third sleeve secured to the adaptive nozzle and slidably mounted on the second sleeve, first locking means able to lock the first sleeve with respect to the pin, second locking means able to lock the second sleeve with respect to the first sleeve, and third locking means able to lock the third sleeve with respect to the second sleeve.

    Abstract translation: 提供一种用于具有滑动盖和自适应喷嘴的​​推力反向器的锁定/解锁装置,其包括固定到反向器的固定结构的固定销,固定到滑动盖并能够容纳销的第一套筒,第二套筒可滑动 安装在第一套筒上,第三套筒固定到自适应喷嘴并可滑动地安装在第二套筒上,第一锁定装置能够相对于销锁定第一套筒,第二锁定装置能够相对于第二套筒锁定第二套筒 第一套筒和第三锁定装置能够相对于第二套筒锁定第三套筒。

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