FIELD: aircraft engineering.
SUBSTANCE: aircraft has a fuselage, a chassis, a wing made with the possibility to change the angle of its installation in the lengthwise plane relative to the fuselage, a means for reducing the run length at landing, for which purpose the said wing is used, which is made with the possibility of its installation on a larger angle by the absolute value than the landing angle of its installation.
EFFECT: invention is aimed at reducing the run length at landing.
4 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2014 |
|
RU2577824C1 |
| AIRBORNE VEHICLE | 2014 |
|
RU2562259C1 |
| AIRCRAFT | 2016 |
|
RU2639352C1 |
| AIRCRAFT (VERSIONS) | 2012 |
|
RU2486105C1 |
| VTOL AIRCRAFT | 2013 |
|
RU2531792C1 |
| AIRCRAFT | 2012 |
|
RU2495796C1 |
| AIRCRAFT | 2012 |
|
RU2509033C1 |
| VERTICAL TAKE-OFF AND LANDING AEROPLANE | 1992 |
|
RU2028964C1 |
| AIRCRAFT | 2017 |
|
RU2672308C1 |
| VERTICAL OR SHORT TAKEOFF AND LANDING AIRCRAFT | 1994 |
|
RU2086477C1 |
