| 摘要 |
A rear suspension ( 10 ) for an aircraft engine assembly comprises a structure comprising two three-point shackles ( 12, 12 ') and one two-point shackle ( 14 ). One of the hinge pins in waiting on the two-point shackle ( 14 ), preferably the hinge pin ( 26 ) fixed to the engine yoke joint, is mounted with clearance and with a damping ring acting as a spring to prevent vibrations of the engines as long as the hinge pin ( 26 ) is not engaged. Each of the suspension connecting pins ( 10 ) is a ball joint connection, the beam ( 16 ) of the suspension ( 10 ) being provided with five aligned orifices ( 24, 24 a , 28, 24', 24 a').
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