The invention provides a six-axis turbojet power type air runway additionally provided with lifting force wings. The six-axis turbojet power type air runway comprises wing body fusion lifting force wings, a back air inlet channel, vector turbojet power units, belly nozzles, a front embedded flow guide pipe, a middle embedded flow guide pipe, a back tail nozzle, a rear tail nozzle, a flight control computer and an undercarriage. The wing body fusion lift wing is a lift wing of a six-axis turbojet power type air runway; the vector turbojet power unit comprises a turbojet engine and a thrust vector nozzle; the belly nozzle is a fuselage opening and is used for outward exhaust of the six vector nozzles when the helicopter is in a maneuvering mode; the front and middle embedded flow guide pipes are arranged in the fuselage, the back tail nozzle is arranged at the rear part above the fuselage, and the flight control and navigation computer is arranged in the middle of the fuselage. According to the technical scheme, the aircraft can be quickly disassembled and assembled in a short time according to different needs, different tasks can be conveniently executed on an air runway, and the endurance time and endurance mileage of the aircraft are prolonged.

    本发明提供一种加装升力翼的六轴涡喷动力式空中跑道,包括:翼身融合升力翼、背部进气道、矢量涡喷动力单元、机腹喷口、前部内埋式导流管、中部内埋式导流管、背部尾喷口、后部尾喷口、飞行控制计算机及起落架。翼身融合升力翼为六轴涡喷动力式空中跑道的升力翼,矢量涡喷动力单元包括涡喷发动机和推力矢量喷嘴;机腹喷口为机身开口,用于直升机机动模态时六个矢量喷嘴的对外排气;前部、中部内埋式导流管设置于机身内部,背部尾喷口设置于机身上方后部,飞行控制与导航计算机设置于机身中部。本发明技术方案,能够根据不同需要在短时间内快速拆卸、装配,便于空中跑道执行不同任务,提升该飞行器的续航时间和续航里程。


    Access

    Download


    Export, share and cite



    Title :

    Six-axis turbojet power type air runway additionally provided with lifting wings


    Additional title:

    一种加装升力翼的六轴涡喷动力式空中跑道


    Contributors:
    PIAN XUECHAO (author) / LEE DONG-SHIN (author) / JIANG KUN (author) / DONG FANGCHEN (author) / LIU JIA (author) / HUANG ZHI (author) / TIAN JIAWANG (author) / LIU KAI (author) / LIU ENHAO (author) / ZHU SHUHAO (author)

    Publication date :

    2024-11-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Tractor additionally provided with protector

    ZHANG TAO / TIAN YANLI / CHEN XIANGSHUAI et al. | European Patent Office | 2023

    Free access

    Additionally-mounted type lifting hub reduction gear

    JIANG XINQUAN | European Patent Office | 2021

    Free access

    Automobile additionally provided with solar panel

    YU YITONG | European Patent Office | 2015

    Free access


    Multifunctional cabin cover additionally provided with mooring track

    GUO HANHUI / WANG ZHIBIN / HAN CAN et al. | European Patent Office | 2025

    Free access