The invention discloses a three-body fusion aircraft which comprises an aircraft body, two wings and an aircraft empennage. The two wings are arranged on the two sides of the fuselage respectively, the first end of the fuselage is connected with the first ends of the wings, the empennage is arranged at the second end of the fuselage, and during flight, the first end of the fuselage is located at the front end of the second end of the fuselage; the wings comprise first wing sections, the sides, close to the fuselage, of the first wing sections are integrally connected with the fuselage, the first wing sections are provided with business cabins, and the fuselage is provided with a hydrogen tank cabin. The business cabins are arranged on the wings, the hydrogen tank cabins are arranged on the fuselage, the volume of the hydrogen tank cabins can be increased, the requirement for the hydrogen fuel amount of the aircraft voyage is met, and the aircraft is small in infiltration area and small in flight resistance.

    本发明公开了一种三机体融合飞机,包括机身、两个机翼以及机尾翼;两个所述机翼分别设置在所述机身两侧,所述机身第一端和所述机翼第一端相连,所述机尾翼设置在所述机身第二端,飞行时,所述机身第一端位于所述机身第二端的前端;所述机翼包括第一翼段,所述第一翼段靠近所述机身一侧与所述机身一体连接,所述第一翼段设有商务舱,所述机身设有氢罐舱。在商务舱设置在所述机翼,机身上设置氢罐舱,可增大氢罐舱的容积,满足飞机航程的氢燃料量需求,且本申请飞机的浸润面积较小,飞行阻力小。


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    Title :

    Three-airframe integrated aircraft


    Additional title:

    一种三机体融合的飞机


    Contributors:
    CUI ZHENG (author) / PENG LEI (author)

    Publication date :

    2022-09-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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