FIELD: vertical takeoff and landing flying vehicles. SUBSTANCE: proposed device includes centrifugal blower and aerodynamic surfaces of wing profile which are made in form of taper spirals ensuring simultaneously positive angle of attack in direction of lift. Resultant angle of attack on aerodynamic surface is defined by amount of angle of spiral and iconicity in plane of vector of absolute velocity of air flow. EFFECT: simplified construction; enhanced economical efficiency. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE | 1997 |
|
RU2172705C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2011 |
|
RU2459746C1 |
| DEVICE FOR CREATING LIFT FORCE IN VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 1992 |
|
RU2005660C1 |
| LEBACH ("BIRD") | 2010 |
|
RU2592122C2 |
| METHOD OF CREATING AIRCRAFT LIFT OR THRUST | 2010 |
|
RU2406650C1 |
| DEVICE AND METHOD FOR FLIGHT THROUGH AIR WITH POSSIBILITY OF VERTICAL TAKEOFF AND LANDING | 2013 |
|
RU2566177C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2013 |
|
RU2534112C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2023 |
|
RU2810988C1 |
| AXISYMMETRIC AIRCRAFT | 2022 |
|
RU2789464C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2012 |
|
RU2518143C2 |
