An hybrid aircraft power plant, has: a gas turbine engine having a high-pressure spool including a high-pressure compressor, a high-pressure turbine, and a high-pressure shaft drivingly engaging the high-pressure turbine to the high-pressure compressor, a low-pressure spool including a low-pressure compressor, a low-pressure turbine, and a low-pressure shaft drivingly engaging the low-pressure turbine to the low-pressure compressor; an electric motor drivingly engaged to the low-pressure shaft; and a torque-transmitting device operatively connected to the HP-shaft and having an engaged configuration in which the torque-transmitting device drivingly engages the electric motor to the high-pressure shaft and a disengaged configuration in which the torque-transmitting device disconnects the electric motor from the high-pressure shaft.
HYBRID POWER PLANT FOR AIRCRAFT
GROUPE MOTOPROPULSEUR HYBRIDE POUR AERONEF
2022-07-25
Patent
Electronic Resource
English
SUBSONIC AIRCRAFT HYBRID POWER PLANT AND KRISHTOP MULTIPURPOSE AIRCRAFT (VERSIONS)
European Patent Office | 2019
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