FIELD: transportation.
SUBSTANCE: strategic helicopter contains vertical cylindrical fuselage (1) and bearing coaxial propellers (2). Fuselage is implemented according to scheme "tube inside tube", and all helicopter units are located in space formed between external tube walls and internal through tube for installation inside of through fuselage chamber the missile with ability of its launching.
EFFECT: invention improves helicopter maneuverability.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ABOVE-WATER TRANSPORT-LAUNCHING DEVICE "KASATKA" | 2005 |
|
RU2303762C1 |
| HELICOPTER BEARING SYSTEM | 2008 |
|
RU2389651C2 |
| HELICOPTER WITH CONTRAROTATION FUSELAGE | 2008 |
|
RU2363618C1 |
| ROCKET LAUNCHER | 2006 |
|
RU2330233C1 |
| BEARING UNIT OF AIRCRAFT | 2007 |
|
RU2354581C1 |
| HELICOPTER CONTRAROTATION DEVICE | 2009 |
|
RU2390467C1 |
| HELICOPTER WITH PITCH ROTOR | 2010 |
|
RU2423290C1 |
| HELICOPTER WITH WEDGE-SHAPED AIRFRAME | 2009 |
|
RU2392187C1 |
| SMALL TWO-DECK AIRCRAFT CARRIER | 2009 |
|
RU2390462C1 |
| HYDRID ROCKET | 2008 |
|
RU2383851C1 |
