首页> 外国专利> Aeromotor fastener with inclined fixing element, aeromotor fastener including the aeromotor fastener and method for fixing the motor to the aeromotor pad by using the aeromotor fastener

Aeromotor fastener with inclined fixing element, aeromotor fastener including the aeromotor fastener and method for fixing the motor to the aeromotor pad by using the aeromotor fastener

机译:具有倾斜的固定元件的航空发动机紧固件,包括该航空发动机紧固件的航空发动机紧固件以及通过使用该航空发动机紧固件将电动机固定到航空发动机垫的方法

摘要

The invention relates to an engine clamp (50) for connecting an engine and an aircraft mast (54) D. the engine clamp (50) comprises a first top cap (56), which has two parallel wings (72, 72), (52) between the wings (72, 72) of the first top cap (56) and is connected with the first top cap (56). The first starting part (56) is connected by the first connecting system (58)-Fixings (80.1-80.4)Connect the first cap (56) to the mast (54)Including the first and second fixed elements (80.1, 80.2) (...) (...) located between the wings In the presence of a connector (52, 56) of the first connection system (58, 50) connected to the first connection, tilt the first cover (56) at an angle of 10 ° to 45 ° so that it can be installed and removed.The inclined fixing element restores the side force. According to the invention, before the engine is fixed to the mast, the connecting piece () and the first cover () are connected to the first cover (), and the engine is fixed to the mast through the fixing piece (80.1-80.4).
机译:本发明涉及用于连接发动机和飞机桅杆(54)D的发动机夹具(50)。发动机夹具(50)包括第一顶盖(56),其具有两个平行的翼(72、72),(第一顶盖(56)的翼部(72、72)之间形成有与图52所示的第一顶盖(56)连接的第一顶盖(56)。第一起始部件(56)通过第一连接系统(58)连接-固定件(80.1-80.4)将第一盖(56)连接到桅杆(54),包括第一和第二固定元件(80.1,80.2)( ...)(...)位于机翼之间...在与第一连接器相连的第一连接系统(58,50)的连接器(52,56)存在的情况下,将第一盖(56)倾斜一定角度倾斜角度为10°至45°,以便可以安装和卸下它。倾斜的固定元件可恢复侧向力。根据本发明,在将发动机固定至桅杆之前,将连接件(1)和第一盖()连接至第一盖(),并且通过固定件将发动机固定至杆(80.1-80.4)。 )。

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