The invention provides a support structure suitable for a satellite orbital transfer engine. The support structure comprises an engine mounting flange, a support supporting rod assembly and a fastener, the support supporting rod assembly comprises a connector and a supporting rod, a supporting rod lug joint is arranged at one end of the supporting rod, the other end of the supporting rod is connected with the connector, and the supporting rod lug joint of the supporting rod is connected with the engine mounting flange through the fastener. The flange plate is simple in structure and easy and convenient to operate, the lightweight design is achieved, the structural weight is reduced, the production cost is reduced, good heat resistance, humidity resistance, structural rigidity and strengthare achieved, and when the position of an engine is changed, the engine can be installed by repairing a flange plate.
本发明提供了一种适用于卫星变轨发动机的支架结构,包括发动机安装法兰、支架撑杆组件、以及紧固件,所述支架撑杆组件包括接头与支撑杆,所述支撑杆的一端设置有撑杆耳接,支撑杆的另一端连接接头,所述支撑杆的撑杆耳接通过紧固件连接发动机安装法兰。本发明结构简单,操作简便,实现了轻量化设计,减轻了结构重量,降低了生产成本,具有良好的耐热性、耐湿性、结构刚度以及强度,在发动机位置有所变化时,可以通过修配法兰盘实现发动机安装。
Support structure suitable for a satellite orbital transfer engine
适用于卫星变轨发动机的支架结构
2020-06-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Orbital Transfer Vehicle Engine Technology
NTIS | 1991
|Orbital transfer vehicle engine integration study
NTRS | 1985
|Orbital transfer vehicle engine integration study
NTRS | 1984
|Orbital Transfer Vehicle Engine Integration Study
NTIS | 1984
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