FIELD: aircraft engineering.
SUBSTANCE: aircraft wing features the profile of thin rhomb composed by top and bottom airfoils. Wing tail section can displace relative to fixed head section and turn about its axis. Angle of tail section turn relative to the line parallel about top airfoil and crossing the tail section centre make 90 degrees upward and 30 degrees downward.
EFFECT: shorter landing run.
6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WING | 2012 |
|
RU2503582C1 |
| AIRBORNE VEHICLE | 2013 |
|
RU2533933C1 |
| WIDE-BODY AIRCRAFT WING (VERSIONS) | 2014 |
|
RU2568627C1 |
| AIRCRAFT | 2013 |
|
RU2530354C1 |
| AIRCRAFT WING | 2013 |
|
RU2537348C1 |
| AIRCRAFT | 2015 |
|
RU2581970C1 |
| AIRCRAFT | 2009 |
|
RU2407672C1 |
| AIRBORNE VEHICLE | 2013 |
|
RU2544036C1 |
| AIRCRAFT | 2015 |
|
RU2580391C1 |
| AIRCRAFT WING | 2012 |
|
RU2494920C1 |
