The invention discloses a manned air cushion type aircraft and a steering control method thereof, and relates to the technical field of novel aircraft take-off and landing. The air cushion type takeoff and landing system can be suitable for various takeoff and landing environments, the problem that an existing fixed wing aircraft is single in takeoff and landing environment is solved, the steering mode of the air cushion type takeoff and landing system is improved, the air cushion type takeoff and landing system has the steering capacity in various environments, meanwhile, flow loss for steering is reduced, and the rolling problem caused by steering is avoided. The bottom of the fuselage is fixedly connected with an annular airbag; an air inlet is formed in the top surface of the tail part of the machine body, and a fan is arranged in the air inlet; a gas pipeline and a pressurizing chamber are arranged in the machine body; a pair of steering spray pipes symmetrically distributed along the center of the fuselage is further arranged at the tail of the fuselage. When an air cushion type takeoff and landing system of a fixed-wing aircraft is modified, the total weight of an aircraft body is reduced, the total mass of the aircraft is reduced, the aircraft has a multi-habitat takeoff and landing function and an air bag withdrawing function, the carrying space and the aerodynamic shape of the aircraft are reserved, and personnel transportation and rescue in areas such as open sea and desert are achieved.

    本发明公开了一种载人气垫式飞机及其转向操纵方法,涉及新型飞行器起降技术领域。能够适用于各种起飞降落环境,解决了现有固定翼飞机起飞降落环境单一的问题,并改进了气垫式起落系统的转向方式,使其具备了多种环境下的转向能力,同时减小了用于转向的流量损耗,避免了由转向引起的滚转问题。机身的底部固定连接有环形的气囊;机身尾部的顶面上开设有进气口,所述进气口内设有风机;机身内部设有输气管道以及增压室;在机身尾部还设有一对沿机身中心对称分布的转向喷管。在固定翼飞机改装气垫式起落系统时减小机体总重量,减小了飞机总体质量,使飞机具备多栖起降功能、气囊收回功能并保留了飞机的运载空间与气动外形,实现远海、沙漠等地区的人员运输与救援。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Manned air cushion type aircraft and steering control method thereof


    Weitere Titelangaben:

    一种载人气垫式飞机及其转向操纵方法


    Beteiligte:
    YIN QIAOZHI (Autor:in) / YANG LINCHENG (Autor:in) / ZHANG PENG (Autor:in) / ZHANG SONGYANG (Autor:in) / WEI XIAOHUI (Autor:in) / NIE HONG (Autor:in) / WANG JIANKANG (Autor:in)

    Erscheinungsdatum :

    2023-12-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B60V Luftkissenfahrzeuge , AIR-CUSHION VEHICLES / B64C AEROPLANES , Flugzeuge



    Manned aircraft parachute control method, controller system and manned aircraft

    ZHAO DELI / XIE PENG / ZHOU SHUANGJIU | Europäisches Patentamt | 2021

    Freier Zugriff

    Manned aircraft and control device thereof

    FAN CHANGLIANG | Europäisches Patentamt | 2022

    Freier Zugriff

    Manned aircraft control method

    ZHANG SHENGWEI / WANG TAORAN / ZHAO QINGLONG et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    MANNED AIRCRAFT

    SUZUKI YOICHI | Europäisches Patentamt | 2023

    Freier Zugriff

    Manned aircraft

    YIN ZUOZONG / YAN LINTONG / LI WEI et al. | Europäisches Patentamt | 2023

    Freier Zugriff