FIELD: aviation.
SUBSTANCE: first version of a pilotless combat aircraft contains a fuselage and a wing. The barrel of the gun is the front part of the fuselage. It has a forward close-coupled canard configuration, movably mounted on a section of the barrel, which has splines on the outside and spring-loaded in the "front" direction. The second pilotless combat aircraft contains a fuselage and a wing. The barrel of the gun is a longitudinal element of the wing's strength - a spar. The barrel has several cylindrical sections on which the sliding bushings are located, which in turn are attached to the transverse set of the wing.
EFFECT: weight reduction.
4 cl, 3 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| ATTACK AIRCRAFT - 2 (OPTIONS) | 2017 | 
 | RU2655588C1 | 
| ATTACK AIRCRAFT (VERSIONS) | 2016 | 
 | RU2623638C1 | 
| SYSTEM OF PRECISION WEAPON /VERSIONS/ | 2014 | 
 | RU2557873C1 | 
| ANTI-AMBUSH WEAPON | 2015 | 
 | RU2623617C2 | 
| ANTI-AIRCRAFT GUN | 2016 | 
 | RU2639378C1 | 
| LONG-RANGE RADAR DETECTION AIRCRAFT | 2016 | 
 | RU2639374C1 | 
| ANTI-AIRCRAFT MISSILE - 2 | 2017 | 
 | RU2659436C1 | 
| INDEPENDENTLY TARGETABLE MULTIPLE LAUNCHER SYSTEM | 2017 | 
 | RU2653426C1 | 
| LONG-RANGE GUN OF STAROVEROV | 2008 | 
 | RU2391617C2 | 
| AIR-FIRED MISSILE | 2017 | 
 | RU2661490C1 | 
Authors
Dates
2017-06-14—Published
2016-05-04—Filed