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).


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    Title :

    THRUST FORCE GENERATION DEVICE AND AIRCRAFT


    Additional title:

    SCHUBKRAFTERZEUGUNGSVORRICHTUNG UND FLUGZEUG
    DISPOSITIF DE GÉNÉRATION DE FORCE DE POUSSÉE, ET AÉRONEF


    Contributors:
    TAKAMI HIKARU (author) / YOKOI YUTO (author)

    Publication date :

    2020-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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