Invention Grant
US07789344B2 Aircraft engine mounting device attachment arrangement 有权
飞机发动机安装装置附件装置

Aircraft engine mounting device attachment arrangement
Abstract:
An aircraft engine mounting device attachment arrangement includes a fitting perforated with two orifices, and two ball joints respectively housed in the orifices. The arrangement also includes two anti-rotation systems used to lock the ball joints in their orifices, the system including a main plate traversed by an external ring of the ball joint and including tappets cooperating with notches provided on the ring, the system including a main plate traversed by a main plate of the ball joint and including tappets cooperating with notches provided on the ring. In addition, the plates are connected rigidly to each other.
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