FIELD: transportation.
SUBSTANCE: in the super-cargo aircraft, structural robustness of the fuselage is partially provided for by the transported element. The super-cargo aircraft can have a fastening device for fastening the transported element to the fuselage. The fastening device is designed for holding part of the load carried by the super-cargo aircraft.
EFFECT: design of a super-cargo aircraft with low unladen weight.
9 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SYSTEM AND METHOD FOR SECURING CARGO | 2018 |
|
RU2760941C2 |
| SYSTEM OF INJECTION OF PAYLOAD INTO LOW-ALTITUDE NEAR-EARTH ORBIT | 1997 |
|
RU2191145C2 |
| VERTICALLY BUILT-IN STIFFENERS | 2013 |
|
RU2649839C2 |
| DEVICE FOR MOORING AIRCRAFT FUSELAGE IN TRANSPORT FLYING VEHICLE | 1996 |
|
RU2105700C1 |
| FLYING VEHICLE CASE | 1999 |
|
RU2193506C2 |
| TRANSPORT AIRCRAFT | 0 |
|
SU835023A1 |
| TRANSPORT AIRCRAFT | 1989 |
|
RU1775970C |
| COMPARTMENT OF FLYING VEHICLE WITH EXTERNAL STORE PYLONS | 1999 |
|
RU2176970C2 |
| AMPHIBIA | 1999 |
|
RU2174080C2 |
| CONTROLLABLE AEROSTATIC FLYING CRANE | 1995 |
|
RU2098318C1 |
