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发动机安装节(Engine Mount)主要连接发动机和吊挂,有效地将动力装置产生的载荷传递到飞机。本文规定了民用飞机发动机安装节设计的适航要求、拆卸要求、互换性要求、强度要求、容差要求、选材等设计准则和设计方法。
Engine Mount The engine mount mainly connects the engine and the hanger, effectively transmitting the load generated by the power unit to the aircraft. This article stipulates the design criteria and design methods of airworthiness, disassembly, interchangeability, strength, tolerance requirements, material selection, etc. of civil aircraft engine mounting design.