FIELD: transport.
SUBSTANCE: invention relates to aerodynamic elements for stabilisation of airborne vehicles. Airborne vehicle aerodynamic focus control element includes airfoil fixed on shaft, steering machine and linkage for transmission of hinge moment from shaft to steering machine rod. The linkage transmits hinge moment generated by air foil to steering machine rod via one or more its members which are mechanical or pneumatic springs.
EFFECT: invention is focused on providing relation between mass centre position and aerodynamic focus position.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WITH FEATHERED HORIZONTAL TAIL | 2015 |
|
RU2609620C1 |
| AIRCRAFT OF FEATHERED CANARD ARRANGEMENT (KRASNOV-CANARD) | 2015 |
|
RU2609644C1 |
| CONTROL ACTUATOR OF ALL-MOVING AERODYNAMIC SURFACE | 1994 |
|
RU2090446C1 |
| AIRFOIL CONTROL ACTUATOR OF AIRBORNE VEHICLE | 0 |
|
SU1794804A1 |
| FRAMEWORK | 2016 |
|
RU2646691C2 |
| METHOD TO CONTROL MOVEMENT OF VEHICLE CONVERTIBLE INTO AIRCRAFT AND DESIGN OF SUCH VEHICLE | 1999 |
|
RU2169085C1 |
| FLYING VEHICLE AERODYNAMIC CONFIGURATION | 1993 |
|
RU2093417C1 |
| METHOD OF TURNING FLYING VEHICLE CONTROL AERODYNAMIC SURFACE | 2001 |
|
RU2193992C2 |
| ORNITHOPTER | 2010 |
|
RU2452660C2 |
| HELICOPTER | 1993 |
|
RU2089455C1 |
