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    Turbojet engine nacelle with downstream section
    1.
    发明授权
    Turbojet engine nacelle with downstream section 有权
    涡轮喷气发动机舱与下游段

    公开(公告)号：US09341083B2

    公开(公告)日：2016-05-17

    申请号：US14524099

    申请日：2014-10-27

    Applicant: AIRCELLE

    Inventor： Hazem Kioua ,  Vincent Peyron ,  Laurent Georges Valleroy

    IPC: B64D29/06 ,  F01D25/24 ,  F02K1/72 ,  B64D33/04

    CPC classification number: F01D25/24 ,  B64D29/06 ,  B64D33/04 ,  F02K1/72 ,  F05D2220/30

    Abstract: A turbofan engine nacelle has a downstream section which includes at least one front frame. The front frame is attached to a stationary portion of the nacelle, and the downstream section is provided with at least one rail or slide which extends in a longitudinal direction of the nacelle and is capable of engaging with at least one corresponding slide or rail of an attachment pylon of the turbofan engine. The front frame is connected to the rail or slide of the downstream section by means of at least one swiveled connecting rod.

    Abstract translation: 涡轮风扇发动机舱具有包括至少一个前框架的下游部分。 前框架连接到机舱的静止部分，并且下游部分设置有至少一个轨道或滑块，其沿着机舱的纵向方向延伸并且能够与至少一个相应的滑轨或轨道接合 涡扇发动机的附件塔。 前框架通过至少一个可旋转的连接杆连接到下游部分的导轨或滑块。

    Assembly centering device for turbojet engine nacelle
    3.
    发明授权
    Assembly centering device for turbojet engine nacelle 有权

    公开(公告)号：US10087781B2

    公开(公告)日：2018-10-02

    申请号：US14730687

    申请日：2015-06-04

    Applicant: AIRCELLE

    Inventor： Hazem Kioua ,  Xavier Raymond Yves Lore ,  Olivier Conet ,  Xavier Holay

    IPC: F01D25/24 ,  B64D29/06

    Abstract: The present disclosure relates to a centering device for a nacelle of a turbojet engine providing the flush centering of an outer downstream panel of a thrust reverser with respect to a cowl of a fan casing. The centering device includes, in one single piece: a sub plate allowing the fixing of the centering device to the fan casing; a first positioning arm integrally formed with the sub plate, protruding upstream, in such a manner as to form, with respect to a directing axis (A) of the nacelle; a first radial abutment designed for guiding the cowl of the fan casing; and a second positioning arm, integrally formed with the sub plate, protruding downstream, in such a manner as to form, with respect to the directing axis (A) of the nacelle, a second radial abutment designed for guiding the outer downstream panel.

    DEVICE FOR CONNECTING A THRUST REVERSER FRONT FRAME TO A FAN CASING AND NACELLE INCORPORATING SUCH A DEVICE
    4.
    发明申请
    DEVICE FOR CONNECTING A THRUST REVERSER FRONT FRAME TO A FAN CASING AND NACELLE INCORPORATING SUCH A DEVICE 有权
    用于连接逆向前框架的风扇装置和装置的装置

    公开(公告)号：US20130227962A1

    公开(公告)日：2013-09-05

    申请号：US13860726

    申请日：2013-04-11

    Applicant: AIRCELLE

    Inventor： Serge Bunel ,  Vincent Peyron ,  Hazem Kioua ,  Jerome Lescure

    IPC: F01D25/28

    CPC classification number: F01D25/28 ,  F01D25/243 ,  F02K1/56 ,  F02K1/766 ,  F02K1/80 ,  F05B2240/911 ,  F05D2230/60 ,  F05D2250/411 ,  F05D2260/30 ,  F05D2260/50 ,  F16B2/14 ,  F16L23/036 ,  F16L37/101 ,  Y02T50/671

    Abstract: A device for connecting a thrust reverser front frame to a fan casing includes a crenulated flange secured to the front frame, an annular component to accept this flange secured to the fan casing, and a crenulated annulus of a shape that complements the flange and pivot-mounted on the annular component. The crenulated flange, the annular component and the crenulated annulus are designed in such a way that a rotation of the annulus with respect to the annular component has the effect of locking this flange against this annular component through the collaboration between the respective crenulations of the flange and of the annulus.

    Abstract translation: 用于将推力反向器前框架连接到风扇壳体的装置包括固定到前框架的螺旋形凸缘，用于接收固定到风扇壳体上的该凸缘的环形部件，以及与凸缘和枢轴连接部分互补的形状的圆环， 安装在环形部件上。 齿形凸缘，环形部件和棘轮环形空间被设计成使得环形件相对于环形部件的旋转具有通过凸缘的相应齿形部之间的协作将该凸缘锁定在该环形部件上的作用 和环带。

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