公开(公告)号：US07021585B2

公开(公告)日：2006-04-04

申请号：US10874349

申请日：2004-06-24

申请人： Philippe Loewenstein ,  Frédéric Darcy ,  Marc Tesniere

发明人： Philippe Loewenstein ,  Frédéric Darcy ,  Marc Tesniere

IPC分类号： B64D27/00

CPC分类号： B64D27/26 ,  B64D2027/266 ,  B64D2027/268

摘要： A turbine engine mount to a pylon of an aircraft includes a bracket arranged to be attached to the pylon, and a lever attached in its central part to the bracket via a first connection and two thrust links each joined aft to the lever by a second connection. The lever includes a central part with two arms, and the bracket includes an integral attachment lug placed between the two arms and connected to the arms via a pivot pin to form the first connection. The lever is laterally connected to the bracket via pivot pins passing through the lever and mounted with a clearance to form connections on standby.

摘要翻译： 涡轮发动机安装到飞机的吊架包括布置成附接到塔架的托架和通过第一连接件连接到其托架的杠杆的杠杆和通过第二连接件与杠杆接合的两个推力连杆 。 杠杆包括具有两个臂的中心部分，并且支架包括放置在两个臂之间并且经由枢轴销连接到臂的一体式附接耳，以形成第一连接。 杠杆通过穿过杠杆的枢轴销横向连接到支架，并安装有间隙以形成待机连接。