FIELD: aeronautical engineering. SUBSTANCE: aircraft comprises lift-thrust or cruise engine provided with two nozzles and lift-jet engine. Nozzles of both jet engines are located in center portion of fuselage, i.e. engines are located by their nozzles towards each other. EFFECT: enhanced reliability. 2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
VTOL AIRCRAFT | 2013 |
|
RU2531792C1 |
VERTICAL TAKE-OFF AND LANDING AEROPLANE | 1992 |
|
RU2028964C1 |
AIRCRAFT | 2014 |
|
RU2577824C1 |
AIRCRAFT (VERSIONS) | 2012 |
|
RU2486105C1 |
AIRCRAFT | 2015 |
|
RU2607037C1 |
AIRBORNE VEHICLE | 2014 |
|
RU2562259C1 |
AIRCRAFT | 2012 |
|
RU2495796C1 |
AIRCRAFT | 2016 |
|
RU2639352C1 |
SUPERSONIC LOW-VISIBILITY AIRCRAFT-HELICOPTER | 2018 |
|
RU2692742C1 |
AIRCRAFT VERTICAL TAKE-OFF SYSTEM | 2014 |
|
RU2582743C1 |
Authors
Dates
1997-08-10—Published
1994-12-21—Filed