This thrust force generation device (1) is provided with: a turbo fan engine unit (2) that is provided with a generator (7) for generating power using a rotation force of a drive shaft, and drives a fan (5) provided on the drive shaft using gas produced by burning fuel; a motor driving fan unit (3) that is provided with a motor (9) driven by power supplied from the generator (7), that is provided in parallel with the turbo fan engine unit (2), and that drives a fan (8) by using the motor (9); and a conducting unit (20) that connects the generator (7) to the motor (9), and supplies the power generated by the generator (7) to the motor (9). The turbo fan engine unit (2) and the motor driving fan unit (3) are integrated with each other, and the conducting unit (20) is disposed between the turbo fan engine unit (2) and the motor driving fan unit (3).
THRUST FORCE GENERATION DEVICE AND AIRCRAFT
SCHUBKRAFTERZEUGUNGSVORRICHTUNG UND FLUGZEUG
DISPOSITIF DE GÉNÉRATION DE FORCE DE POUSSÉE, ET AÉRONEF
2020-07-29
Patent
Electronic Resource
English