Aircraft engine mounting device attachment arrangement
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United States of America Patent
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Sep 7, 2010
Grant Date -
Mar 20, 2008
app pub date -
Jul 18, 2007
filing date -
Sep 20, 2006
priority date (Note) -
In Force
status (Latency Note)
Importance
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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