An aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other
一种发动机、飞行器的技术,应用在发动机组件领域,能够解决尺寸增大、后发动机附接件总宽度大、发动机整体性能空气动力扰动等问题,达到质量减小、减小总质量的效果
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[0055] figure 2 Shown is an aircraft 200 comprising two wing system units 2 ( figure 2 Only visible is the fuselage 3 of one wing system unit 2) each supporting an engine assembly 5 according to the invention. The engine assembly 5 comprises a twin-flow catamaran engine 10 , such as a turbojet engine, and a mounting pylon 4 for the engine 10 .
[0056] image 3 One of the engine assemblies 5 is shown in more detail. Shown are wing system units 2 , turbojet engines 10 and mounting pylons 4 . Furthermore, mounting means 8 for the pylon 4 are arranged on the wing system unit 2 and mounting means 7a, 7b, 7c for the turbojet engine 10 are arranged on the pylon. These mounting means 7a, 7b, 7c, the pylon 4 and the turbojet 10 form the engine assembly 5 according to the invention.
[0057] The mounting means 8 positioned at the junction between the pylon 4 and the wing system unit 2 are formed in a conventional manner. Therefore, the mounting device 8 will not be described in...
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