FIELD: AVIATION. SUBSTANCE: helicopter has fuselage 1, rotor 2, airfoils 19 and swivel module 4 fixed on post 6 by means of swivel bracket 5, which all may turn about vertical axes O2 end O1. EFFECT: extended functional capabilities. 1 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
HELICOPTER | 1992 |
|
RU2009078C1 |
FLYING VEHICLE | 0 |
|
SU1827363A1 |
AIRCRAFT | 1996 |
|
RU2120394C1 |
HELICOPTER, METHODS OF USE THEREOF, AND PARKING PLACE THEREFOR | 0 |
|
SU1810231A1 |
METHOD TO DECREASE ROTOR ANGLE OF ATTACK AT PRE-LANDING MANOEUVRES OF SINGLE ROTOR HELICOPTER (VERSIONS) | 2014 |
|
RU2539621C1 |
AEROMOBILE OF HOVER TAKE-OFF | 2017 |
|
RU2648937C1 |
AIRCRAFT | 1992 |
|
RU2028966C1 |
MULTI-PURPOSE TWO-FUSELAGE HELICOPTER AIRCRAFT | 2017 |
|
RU2650258C1 |
METHOD OF TRANSPORTATION OF MI-8 HELICOPTERS BY IL-76 AIRCRAFT AND RIGGING FOR PLACING AND MOORING THE HELICOPTERS ON IL-76 AIRCRAFT | 2005 |
|
RU2310584C2 |
TANK | 1992 |
|
RU2027974C1 |
Authors
Dates
1994-01-15—Published
1992-08-19—Filed