FIELD: transport.
SUBSTANCE: proposed method consists in creating asymmetric lengthwise aerodynamic drag on aircraft left and right by aerodynamic brake arranged on one of aircraft wings. Aircraft has left and right outer wings with aerodynamic brakes that can be controlled separately.
EFFECT: higher safety.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT FOR LANDING AT CROSS WIND (VERSIONS) | 2008 |
|
RU2400398C2 |
| STAROVEROV'S SPACECRAFT (VERSIONS) AND/OR ALGORITHMS OF ITS OPERATION | 2012 |
|
RU2503592C1 |
| ATTACK AIRCRAFT - 2 (OPTIONS) | 2017 |
|
RU2655588C1 |
| RESCUE SYSTEM OF AIRPLANE (VERSIONS) | 2006 |
|
RU2336203C2 |
| COUNTERAIR MISSILE | 2009 |
|
RU2439476C2 |
| HYDROPLANE (VERSIONS) | 2013 |
|
RU2513345C1 |
| METHOD OF AIRCRAFT CONTROL AND DEVICE TO THIS END | 2011 |
|
RU2504815C2 |
| SIDE-THRUST ENGINE FOR LANDING AIRCRAFT IN CROSSWIND | 2021 |
|
RU2766913C1 |
| ATTACK AIRCRAFT (VERSIONS) | 2016 |
|
RU2623638C1 |
| STAROVEROV' WING (VERSIONS) | 2011 |
|
RU2480375C1 |
