FIELD: transport.
SUBSTANCE: proposed helicopter has one-side wedge-like nose cone. Said nose cone is formed by one-side skewed side airframe panel to counteract helicopter turn in forward flight.
EFFECT: reduced power consumption of rotor drive.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER WITH CONTRAROTATION FUSELAGE | 2008 |
|
RU2363618C1 |
| HELICOPTER CONTRAROTATION DEVICE | 2009 |
|
RU2390467C1 |
| HELICOPTER BEARING SYSTEM | 2008 |
|
RU2389651C2 |
| BEARING UNIT OF AIRCRAFT | 2007 |
|
RU2354581C1 |
| HELICOPTER WITH PITCH ROTOR | 2010 |
|
RU2423290C1 |
| STRATEGIC HELICOPTER | 2007 |
|
RU2336199C1 |
| HELICOPTER AND METHOD OF CONTROL OF SINGLE-ROTOR HELICOPTER | 2002 |
|
RU2238221C2 |
| ROTOR | 2008 |
|
RU2385268C1 |
| SUPERSONIC LOW-VISIBILITY AIRCRAFT-HELICOPTER | 2018 |
|
RU2692742C1 |
| HELICOPTER | 2003 |
|
RU2246426C1 |
