FIELD: aircraft engineering.
SUBSTANCE: proposed craft comprises the frame coupled without transmission with bearing thin disc equipped with folding radial blades of centrifugal fan articulated with the disc top surface. Axial fan adjustable blades are arranged the disc edges converting into rotor in vertical flight and into circular wing in horizontal flight. Disc drive blades folding flush with the disc bottom surface are arranged under the disc, disc being spinned by engine jet gas. Engines are secured to aforesaid frame by flight control fins.
EFFECT: combined design.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DISC CRAFT | 2013 |
|
RU2520177C1 |
| ROTOR "AIR WHEEL", GYROSTABILISED AIRCRAFT AND WIND-DRIVEN ELECTRIC PLANT USING ROTOR "AIR WHEEL", SURFACE/DECK DEVICES FOR THEIR START-UP | 2013 |
|
RU2538737C9 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| HYBRID JET PLANE-HELICOPTER | 2019 |
|
RU2706430C1 |
| AIRCRAFT WING | 1996 |
|
RU2101215C1 |
| AIRCRAFT | 2000 |
|
RU2192986C2 |
| HIGH-SPEED TURBOFAN COMBINED HELICOPTER | 2016 |
|
RU2629475C1 |
| UNMANNED TRANSONIC AIRCRAFT-HELICOPTER | 2018 |
|
RU2711451C1 |
| AERONAUTICAL RECONNAISSANCE-STRIKE SYSTEM | 2019 |
|
RU2717280C1 |
| UNMANNED JET-HELICOPTER | 2018 |
|
RU2699513C1 |
