A hybrid electric propulsion system and method are provided. More specifically, the present disclosure relates to a control system for a hybrid electric propulsion system of an aircraft configured to rapidly and automatically take action in response to a rapid electrical load change on a torque source, such as an engine. A method for operating a hybrid electric propulsion system of an aircraft is also provided.
提供了一种混合电动推进系统和方法。更具体地,本公开涉及用于飞行器的混合电动推进系统的控制系统,其被构造为响应于扭矩源(例如发动机)上的快速电负载变化而快速且自动地采取动作。还提供了用于操作飞行器的混合电动推进系统的方法。
Fault tolerant hybrid electric propulsion system for aircraft
用于飞行器的容错性混合电动推进系统
2023-06-27
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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