The invention discloses a household small aircraft which comprises a flight system and a riding system and further comprises a lift system. The lift system comprises a front lift fan assembly, a rear lift fan assembly, a left wingtip spray pipe and a right wingtip spray pipe; wherein the front lift fan assembly and the rear lift fan assembly are arranged on a front fuselage body and a rear fuselage body of the fuselage respectively, are driven by the power system and can generate downward airflow; the left wingtip spray pipe is arranged at the wingtip of the left main wing of the wing, the front lift fan cavity provides entrained air, and the left wingtip spray pipe can spray downward airflow; the right wingtip spray pipe is arranged at the wingtip of the right main wing of the wing, entrained air is provided by the front lift fan cavity, and the right wingtip spray pipe can spray downward airflow. According to the scheme, through coordinated operation of the lift force system, in-situ vertical lifting of the aircraft and state conversion between vertical lifting and level flight cruise can be achieved, the lifting convenience of the aircraft can be greatly improved, and therefore the requirement for in-situ air travel can be met.

    本发明公开了一种家用小型飞机,包括飞行系统和驾乘系统,还包括升力系统;升力系统包括前升力风扇组件、后升力风扇组件、左翼尖喷管和右翼尖喷管;其中,前后升力风扇组件分别设置于机身的前机身和后机身,而且均由动力系统提供驱动力,并且均能够产生向下的气流;左翼尖喷管设置于机翼左主翼的翼尖,且由前升力风扇腔提供引气,并且能够喷出向下的气流;右翼尖喷管设置于机翼右主翼的翼尖,且由前升力风扇腔提供引气,并且能够喷出向下的气流。在本方案中,通过升力系统的协调运作,可实现飞机的就地垂直升降,以及垂直升降与平飞巡航的状态转换,可大大提高了飞机的升降便利性,从而有助于满足就地空中出行的需求。


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    Title :

    Domestic small aircraft


    Additional title:

    一种家用小型飞机


    Contributors:
    LI GANG (author)

    Publication date :

    2023-03-17


    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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