METHOD FOR CONTROLLING A HYBRID TURBINE ENGINE
개요
발명자
Philippe DELBOSC; Benoît Lucien MICHAUD
IPC 분류
CPC 분류
A method for controlling a hybrid turbine engine for an aircraft uses an energy storage assembly having a plurality of capacitive components. The turbine engine having a low-pressure shaft, a high-pressure shaft, and at least one power conversion device mounted on the low-pressure shaft or high-pressure shaft. The method includes precharging the capacitive components until a mean voltage reaches a first partial charge value, balancing the voltages of the capacitive components, charging the capacitive components until the mean voltage reaches a high value, and converting electrical energy stored in the storage assembly into mechanical energy delivered to the low-pressure shaft and/or to the high-pressure shaft in order to assist with maneuvering the aircraft.
원문 (중국어)
A method for controlling a hybrid turbine engine for an aircraft uses an energy storage assembly having a plurality of capacitive components. The turbine engine having a low-pressure shaft, a high-pressure shaft, and at least one power conversion device mounted on the low-pressure shaft or high-pressure shaft. The method includes precharging the capacitive components until a mean voltage reaches a first partial charge value, balancing the voltages of the capacitive components, charging the capacitive components until the mean voltage reaches a high value, and converting electrical energy stored in the storage assembly into mechanical energy delivered to the low-pressure shaft and/or to the high-pressure shaft in order to assist with maneuvering the aircraft.