FIELD: aircraft engineering.
SUBSTANCE: aircraft comprises fuselage with cockpit, triangular wing secured atop said fuselage, tail unit, engine arranged above said wing, ejector connected with said engine and landing gear. Engines and ejectors are arranged on both sides of the wing axial line. Tail unit keel is arranged between ejectors. Short cantilever wing is secured from below to said fuselage for attachment of tail undercarriage legs.
EFFECT: better lift.
2 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRBORNE VEHICLE | 2013 |
|
RU2533933C1 |
| AIRCRAFT | 2013 |
|
RU2530354C1 |
| AIRBORNE VEHICLE | 2013 |
|
RU2544036C1 |
| AIRCRAFT | 2012 |
|
RU2503590C1 |
| AFT PORTION OF WIDE-BODY AIRCRAFT | 2013 |
|
RU2545394C1 |
| AIRCRAFT | 2017 |
|
RU2641399C1 |
| AIRCRAFT | 2015 |
|
RU2581970C1 |
| AIRCRAFT | 2009 |
|
RU2407671C1 |
| AIRCRAFT FUSELAGE | 2013 |
|
RU2544055C1 |
| AIRCRAFT (VERSIONS) | 2011 |
|
RU2462392C1 |
