The present invention relates to a hybrid aircraft using hydrogen fuel, comprising: a fuselage housing a hydrogen storage device; a wing attached to the fuselage; the hydrogen combustion engine is mounted on the wing, and hydrogen is supplied to the hydrogen combustion engine by the hydrogen storage device; the electric propulsion device is mounted at the tail part of the fuselage; and a hydrogen fuel cell supplied with hydrogen by the hydrogen storage device to generate electrical energy, and the electric propulsion device supplied with power by the hydrogen fuel cell. According to the hybrid power aircraft, the hybrid power mode that the hydrogen-fired engine and the hydrogen fuel cell drive the tail electric propulsion device is adopted, and the aircraft can be improved in the aspects of environmental protection, economy and efficiency in a leap-over mode.

    本发明涉及一种使用氢燃料的混合动力飞机,包括:机身,机身容纳氢储存装置;机翼,机翼附连到机身;燃氢发动机,燃氢发动机安装在机翼上,并且燃氢发动机由氢储存装置供应氢;电推进装置,电推进装置安装到机身的尾部;以及氢燃料电池,氢燃料电池由氢储存装置供应氢以产生电能,并且电推进装置由氢燃料电池提供电力。这种混合动力飞机采用燃氢发动机和氢燃料电池驱动尾部电推进装置的混合动力形式,可以使得飞机在环保、经济和效率上得到跨越式的提升。


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    Title :

    Hybrid aircraft using hydrogen fuel


    Additional title:

    使用氢燃料的混合动力飞机


    Contributors:
    WANG LI (author) / LI JINYE (author) / GUO SHIXIAN (author) / WANG YUHAN (author) / WU DAWEI (author) / TAN ZHAOGUANG (author)

    Publication date :

    2024-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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