FIELD: aviation.
SUBSTANCE: method of cylinder rotation serving as aircraft wings is based on the Magnus effect generated in conjunction with screws of the aircraft main engines and counter oncoming flow of the rotating cylinders. The oncoming gas flow affects the aerodynamically profiled blades of balanced blade rotors. Torques which through further axial spigot joints and gear reducers-multipliers increasing the rotational speed 3.5-4 times are passed to the balanced rotating cylinders coaxial axles with endplates are created on coaxial balanced bladed rotors with the help of aerodynamic forces arising on these blades. Coaxial axles of the balanced rotating cylinders are mounted cantilevered in conical power casings, and conical circular frames, large bases of which are rigidly fastened to the rotating cylinders are fixed at the ends of the coaxial axles using flanged heads.
EFFECT: possibility of the auxiliary power unit refusal.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF ROTATING CYLINDERS ACTING AS WINGS ON AIRCRAFT, AND UNMANNED AERIAL VEHICLE FOR ITS IMPLEMENTATION | 2024 |
|
RU2826746C1 |
METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
DEVICE AND METHOD FOR FLIGHT THROUGH AIR WITH POSSIBILITY OF VERTICAL TAKEOFF AND LANDING | 2013 |
|
RU2566177C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2698497C1 |
HELICOPTER | 2018 |
|
RU2701076C1 |
HELICOPTER | 2018 |
|
RU2701083C1 |
HELICOPTER | 2018 |
|
RU2710839C1 |
ROTOR "AIR WHEEL", GYROSTABILISED AIRCRAFT AND WIND-DRIVEN ELECTRIC PLANT USING ROTOR "AIR WHEEL", SURFACE/DECK DEVICES FOR THEIR START-UP | 2013 |
|
RU2538737C9 |
SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711760C2 |
UNMANNED TRANSONIC AIRCRAFT-HELICOPTER | 2018 |
|
RU2711451C1 |
Authors
Dates
2017-03-07—Published
2016-03-02—Filed