A lever for adjusting an output of a hybrid power device of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts an output of the hybrid power device between at least two modes of operation. In a first subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, output first electrical energy from a motor/generator driven by the mechanical output of the engine, and drive a propulsion mechanism by the mechanical output of the engine. In a second subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, receive second electrical energy at the motor/generator, drive the mechanical output through the motor/generator using the second electrical energy, and drive the propulsion mechanism through the mechanical output.
用于调节飞行器的混电动力装置的输出的杆包括配置为在整体位置范围内移动的杆。杆的移动在至少两种操作模式之间调节混电动力装置的输出。在整体位置范围内的第一位置子集中,混电动力装置被配置为操作具有机械输出的发动机,从由发动机的机械输出驱动的马达/发电机输出第一电能,以及通过发动机的机械输出来驱动推进机构。在整体位置范围内的第二位置子集中,混电动力装置被配置为操作具有机械输出的发动机,在马达/发电机处接收第二电能,使用第二电能通过马达/发电机驱动机械输出,以及通过机械输出来驱动推进机构。
Hybrid control system across multiple operating modes
跨多个操作模式的混合控制系统
2024-09-20
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Operating Modes and Control Aspects for a Special Hybrid Drivetrain
British Library Conference Proceedings | 1995
|Operating modes and control aspects for a special hybrid drivetrain
Tema Archive | 1995
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