| 摘要 |
An engine assembly for aircraft including a turboshaft engine, an attachment strut, and a plurality of engine mounts interposed between the attachment strut and the turboshaft engine. The plurality of engine mounts include two forward mounts arranged in a staggered manner in relation to each other in a vertical direction of the turboshaft engine, the first forward mount configured to assure uniquely taking up of stresses brought to bear along the transversal direction of the turboshaft engine, and the second forward mount configured to assure uniquely taking up of stresses brought to bear along the transversal and vertical directions.
|
