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    • 1. 发明申请
    • METHOD FOR ATTACHMENT OF A PRE-ASSEMBLED POWERPLANT AND PYLON ASSEMBLY TO AN AIRCRAFT
    • 用于安装预先组装的动力飞轮和飞镖组装给飞机的方法
    • US20160167808A1
    • 2016-06-16
    • US14907345
    • 2014-07-16
    • Bombardier Inc.
    • Alexandros IliopoulosKevin ShephardRoger-Andre BergeronGeorge Bradley
    • B64F5/00G05B15/02B64D27/26
    • G05B15/02B64D27/26B64F5/10
    • A method for installing a pre-assembled powerplant and pylon assembly on an aircraft comprises determining a first length of a first link, determining a second length of a second link, determining a first distance occupyable by the first link between the pylon and the aircraft, determining a second distance occupyable by the second link between the pylon and the aircraft, determining a first result by subtracting the first distance from the first length, determining a second result by subtracting the second distance from the second length, and determining a third result by adding the first result and the second result. If the third result is less than or equal to zero, the first link is installed between the pylon and the aircraft before the second link If the third result is greater than zero, the second link is installed between the pylon and the aircraft before the first link.
    • 一种用于在飞行器上安装预组装的动力装置和塔架组件的方法,包括确定第一连杆的第一长度,确定第二连杆的第二长度,确定由所述塔架和所述飞机之间的第一连杆占据的第一距离, 确定由所述吊架和所述飞机之间的第二连杆占据的第二距离,通过从所述第一长度减去所述第一距离来确定第一结果,通过从所述第二长度减去所述第二距离来确定第二结果,并且通过 添加第一个结果和第二个结果。 如果第三个结果小于或等于零,则在第二个链路之前,第一个链路安装在塔架和飞机之间如果第三个结果大于零,则第二个链路在第一个链路之前安装在塔架和飞机之间 链接。