FIELD: aviation; disk-type wings.
SUBSTANCE: proposed disk-type wing for helicopter has through horizontal holes whose walls are airtight and watertight; these holes may be opened or closed. Through vertical holes are located symmetrically around central hole or around center of disk-type wing when there is no central hole. Lower surface of disk-type wing may be flat or ellipsoid in shape. Through vertical holes of helicopter disk-type wing are made in form of Laval nozzles.
EFFECT: enhanced efficiency.
2 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
HIGH-SPEED TURBOFAN COMBINED HELICOPTER | 2016 |
|
RU2629475C1 |
HEAVY-DUTY MULTIROTOR CONVERTIBLE ROTORCRAFT | 2013 |
|
RU2521121C1 |
HIGH-SPEED ROTARY-WING AIRCRAFT | 2013 |
|
RU2539679C1 |
SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711633C2 |
ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
AIRCRAFT | 2022 |
|
RU2808288C1 |
HELICOPTER | 2018 |
|
RU2701083C1 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2698497C1 |
MULTIROTOR CONVERTIBLE HIGH-SPEED HELICOPTER | 2014 |
|
RU2548304C1 |
Authors
Dates
2007-05-27—Published
2005-07-27—Filed