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    METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A PYLON, AND ENGINE FASTENER FOR IMPLEMENTING SAID METHOD
    1.
    发明申请
    METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A PYLON, AND ENGINE FASTENER FOR IMPLEMENTING SAID METHOD 有权
    安装PYLON飞机发动机的方法和实施方法的发动机紧固件

    公开(公告)号：US20140033729A1

    公开(公告)日：2014-02-06

    申请号：US14110864

    申请日：2012-03-30

    申请人： Pierre-Alain Jean-Marie Philippe Hugues Chouard ,  Maryline Besnard

    发明人： Pierre-Alain Jean-Marie Philippe Hugues Chouard ,  Maryline Besnard

    IPC分类号： F02C7/20

    CPC分类号： F02C7/20 ,  B64D27/26 ,  B64D2027/266

    摘要： A method for mounting an aircraft engine on a pylon includes positioning at least a first shear pin either in a first opening provided in a front engine fastener which is previously attached to the engine using connecting rods, or in a first bore provided in a front surface of the pylon; prepositioning the assembly including the engine and the front engine fastener relative to the pylon by placing the first shear pin opposite a receiving cavity, the receiving cavity being either the first bore, if the first shear pin has been positioned in the first opening, or the first opening, if the first shear pin has been positioned in the first bore; and inserting the first shear pin into the receiving cavity.

    摘要翻译： 一种用于将飞机发动机安装在挂架上的方法包括至少将第一剪切销定位在设置在前发动机紧固件中的第一开口中，所述第一开口预先使用连接杆附接到发动机，或者在设置在前表面中的第一孔中 的塔 或者将第一剪切销定位在第一开口中，或者将第一剪切销定位在第一开口中时，接收腔是第一孔，或者， 如果第一剪切销已经定位在第一孔中，则首先打开; 并将第一剪切销插入接收腔。