发明申请
US20090302153A1 ELECTRICAL SYSTEM AND ELECTRICAL ACCUMULATOR FOR ELECTRICAL ACTUATION AND RELATED METHODS 有权
用于电动执行的电气系统和电气蓄能器及相关方法

ELECTRICAL SYSTEM AND ELECTRICAL ACCUMULATOR FOR ELECTRICAL ACTUATION AND RELATED METHODS
摘要:
An electrical system for driving flight control actuators, electrical accumulator, and methods for managing electrical power for an aircraft electrical system and methods of retrofitting an aircraft electrical system with an electrical accumulator are provided. The electrical system can include a bidirectional accumulator positioned in electrical communication with the plurality of flight control actuators to absorb excess electrical power regenerated by the plurality of flight control actuators and to provide supplemental power to the plurality of flight control actuators to thereby satisfy transient power requirements.
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