The invention discloses an aero-engine mounting and connecting structure, and relates to the field of aviation safety, the aero-engine mounting and connecting structure comprises a bottom beam, the top of the bottom beam is fixedly connected with a top beam, a plurality of connecting beams are fixedly connected between the bottom beam and the top beam at equal intervals, and a front fulcrum mounting groove is formed in the position, close to the front portion, of the top of the bottom beam in a penetrating mode; the rear portion of the bottom of the bottom beam is fixedly connected with a rear fulcrum connecting block, the top of the top beam is provided with a redundant structure, the redundant structure comprises two first redundant rods and two second redundant rods, the front portion of the top of the top beam is fixedly connected with a first fixing block, and the top of the first fixing block is rotationally connected with a first hanging rod. The rear portion of the top of the top beam is fixedly connected with a second fixing block, and the two sides of the second fixing block are rotationally connected with second hanging rods. By arranging the redundant structure, when the top beam or the bottom beam is broken accidentally, the fixing plate can still be connected with the unbroken part, the connection stability is ensured, and the flight safety is greatly improved.
本发明公开了一种航空发动机的安装连接结构,本发明涉及航空安全领域,包括底梁,所述底梁的顶部固定连接有顶梁,底梁和顶梁之间等距固定连接有若干个连接梁,底梁的顶部靠前部贯穿开设有前支点安装槽,底梁的底部靠后部固定连接有后支点连接块,顶梁的顶部设置有冗余结构,所述冗余结构包括两根冗余杆一和两根冗余杆二,顶梁的顶部靠前部固定连接有第一固定块,第一固定块的顶部转动连接有吊杆一,顶梁的顶部靠后部固定连接有第二固定块,第二固定块的两侧均转动连接有吊杆二。本发明通过设置冗余结构,当顶梁或底梁意外断裂,固定板仍可与未断裂部分连接,确保连接稳定性,极大提升飞行安全性。
Mounting and connecting structure of aero-engine
一种航空发动机的安装连接结构
2025-04-08
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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