|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-031/00 B64D-031/06 B64D-027/24 F01D-007/02 F01D-015/10 F01D-021/00 F02K-001/18 F02C-007/32 F02C-009/20 B64C-011/30 B64D-027/10 B64D-027/02|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 7 인용 특허 : 15|
A control for a hybrid turbo electric aero-propulsion system prioritizes and optimizes the operating parameters, according to a desired optimization objective, for and across a number of different control optimization subsystems of the hybrid turbo electric aero-propulsion system. The control subsystems may include, for example, a propulsion control optimization subsystem and a power plant control optimization subsystem. The optimizations may be based on a system model, which is developed and updated during the operation of the hybrid turbo electric aero...
1. A control system for a turbo electric aero-propulsion system comprising a turbine engine, a generator to receive rotational energy from the turbine engine, an energy storage subsystem to receive electrical input from the generator, the energy storage subsystem comprising one or more of: an energy storage device, a power converter, and an inverter, a motor to receive electrical input from the energy storage subsystem, and a fan that may be driven by either the engine or the motor, the control system having one or more processors comprising: a propulsio...