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
| Title | Year | Author | Number |
|---|---|---|---|
| LARGE FIRE AEROSOL EXTINGUISHING | 2018 |
|
RU2717783C2 |
| ICE FUEL MIX IGNITION BY LASER OPTICAL DISCHARGE | 2014 |
|
RU2575228C2 |
| METHOD AND AIR VEHICLE FOR MOVING IN PLANETARY ATMOSPHERE WITH SPEEDS ABOVE THE FIRST SPACE AND HIGHLY INTEGRATED HYPERSONIC VEHICLE APPARATUS (VERSIONS) FOR IMPLEMENTATION OF THE METHOD | 2012 |
|
RU2618831C2 |
| DETONATION COMBUSTION PULSE-JET ENGINE | 1997 |
|
RU2142058C1 |
| HYDROCARBON FUEL SUPPLY SYSTEM FOR HYPERSONIC AIRCRAFT AND METHOD OF FUEL SUPPLY TO SYSTEM | 2017 |
|
RU2663252C1 |
| UNIVERSAL JET ENGINE (URE) | 2019 |
|
RU2754976C2 |
| CARBURETOR OF INTERNAL COMBUSTION ENGINE | 2000 |
|
RU2184867C2 |
| RAMJET ENGINE RUNNING ON SOLID PROPELLANT AND METHOD OF ITS OPERATION | 2014 |
|
RU2565131C1 |
| METHOD FOR ORGANISATION OF WORKING PROCESS IN LASER ROCKET ENGINE, AND LASER ROCKET ENGINE | 2012 |
|
RU2484280C1 |
| HYPERSONIC AIRCRAFT EQUIPPED WITH COMBINED POWER UNIT AND METHOD OF ITS OPERATION IN FLIGHT | 2023 |
|
RU2805427C1 |
