Aircraft fly-by-wire systems and related vehicle electrical systems are provided. A vehicle electrical system includes a bus arrangement having a plurality of buses, a first control module coupled toa first subset of the buses, a second control module coupled to a second subset of the buses, and a third control module coupled to a third subset of the buses. The first subset includes a first bus,a second bus, a third bus, and a fourth bus, the second subset includes the third bus, the fourth bus, a fifth bus, and a sixth bus, and the third subset includes the first bus, the second bus, the fifth bus and the sixth bus.
本发明提供了飞行器电传操纵系统及相关交通工具电气系统。交通工具电气系统包括总线布置,该总线布置包括多条总线;第一控制模块,该第一控制模块耦接到总线的第一子组;第二控制模块,该第二控制模块耦接到总线的第二子组;以及第三控制模块,该第三控制模块耦接到总线的第三子组。第一子组包括第一总线、第二总线、第三总线和第四总线,第二子组包括第三总线、第四总线、第五总线和第六总线,第三子组包括第一总线、第二总线、第五总线和第六总线。
Redundant fly-by-wire control system with fault elasticity
具有故障弹性的冗余电传操纵系统
2020-11-10
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |