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公开(公告)号:US20240336356A1
公开(公告)日:2024-10-10
申请号:US18539741
申请日:2023-12-14
Applicant: Textron Innovations Inc.
Inventor: Charles Eric COVINGTON , Chia-Wei SU , Darren Gregory LANG , Thomas PARSONS , Cody Earl FEGELY
Abstract: A rotorcraft has a drive system including a main rotor coupled to a main rotor gearbox to rotate the main rotor at a rotor speed, a main engine coupled to the drive system to provide a first power, a supplemental engine coupled, when a first clutch is engaged, to the drive system to provide a second power additive to the first power, and a control system operable to control the main engine and the supplemental engine to provide a total power demand, where the main engine is controlled based on variations in rotor speed and a power compensation command to produce the first power, and the supplemental engine is controlled to produce the second power in response to a supplemental power demand.