FIELD: aviation.SUBSTANCE: hypersonic aircraft (LA) contains a housing with a thermal protection system, a fuel tank with a supply and control system. Body represents a symmetrically increasing and decreasing on the axis body, which has the form of a spindle, an acute-angled triangle or a disk, and has a regenerative cooling system for the fuel of an aircraft body. There is a system for the controlled supply of fuel to the outer shell of the housing in the zone of compression of the air flow with the possibility of its ignition in the zone of maximum compression and temperature. Ensured forced combustion in the zone of expansion of the flow creating the thrust of the aircraft at low flight speeds is provided, as well as changing the fuel supply to the corresponding area of the outer surface of the hull to control the flight of the aircraft. It is possible to use an additional rocket engine for solid fuel.EFFECT: invention is aimed at simplifying thermal protection.1 cl, 2 dwg


    Access

    Download


    Export, share and cite



    Title :

    ГИПЕРЗВУКОВОЙ ЛЕТАТЕЛЬНЫЙ АППАРАТ


    Publication date :

    2017-08-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Летательный аппарат

    European Patent Office | 2021

    Free access



    ВИНТОКРЫЛЫЙ ЛЕТАТЕЛЬНЫЙ АППАРАТ

    European Patent Office | 2016

    Free access