FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Aircraft comprises engine built in airframe tail, triangular wings attached to airframe from below and having deflectors of airflows flowing over top and bottom airfoils, tail empennage and undercarriage. Fuselage has air intakes to suck air into engine to allow increased rarefaction of airflow of wing top airfoils.
EFFECT: higher lift.
3 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2012 |
|
RU2494919C1 |
| AIRCRAFT | 2013 |
|
RU2530354C1 |
| AIRBORNE VEHICLE | 2013 |
|
RU2544036C1 |
| AIRBORNE VEHICLE | 2013 |
|
RU2533933C1 |
| AIRBORNE VEHICLE | 2013 |
|
RU2536154C1 |
| AIRCRAFT | 2009 |
|
RU2407672C1 |
| WIDE-BODY AIRCRAFT WING (VERSIONS) | 2014 |
|
RU2568627C1 |
| AIRCRAFT | 2015 |
|
RU2581970C1 |
| AIRCRAFT WING | 2014 |
|
RU2576845C1 |
| AIRCRAFT | 2015 |
|
RU2580391C1 |
