| 摘要 |
<p>Means for mounting an engine (4) to an aircraft are provided which reduce the dynamic response of the airframe due to engine vibration. A mount comprises at least one strut (22) extending between the engine (4) and the airframe which is attached to the airframe by means of damping elements (26, 38, 40, 48, 50, 39, 41, 49, 51).</p> |
