Flight control systems, flight control methods, and aircraft are provided. An aircraft including an electric propulsion engine, a combustion turbine engine, a flight controller for generating a first control signal indicative of a climb request, a second control signal indicative of a cruise request and a third control signal indicative of a descent request, and an aircraft propulsion controller operative to engage the electric propulsion engine and the combustion turbine engine in response to the first control signal and disengage the electric propulsion engine in response to the second control signal and wherein the electric propulsion engine may be engaged in a regenerative mode to charge a battery in response to the third control signal.
提供了飞行控制系统、飞行控制方法和飞机。一种飞机,包括电动推进发动机;燃气涡轮发动机;飞行控制器,用于生成指示爬升请求的第一控制信号、指示巡航请求的第二控制信号和指示下降请求的第三控制信号;以及飞机推进控制器,可操作为响应于第一控制信号而占用电动推进发动机和燃气涡轮发动机,并且响应于第二控制信号而解除占用电动推进发动机,并且其中,电动推进发动机可以响应于第三控制信号以再生模式被占用,以为电池充电。
HYBRID JET ELECTRIC AIRCRAFT
混合喷气电动飞机
2021-11-09
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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