FIELD: transport.
SUBSTANCE: aircraft aerodynamic control element comprises fixed aerodynamic surface field in cantilever on airframe, control surface with its axle and drive arranged inside aircraft airframe. Aforesaid control surface is located within the area of fixed aerodynamic surface, nearby its side chord, spaced from edges and end chord.
EFFECT: simplified attachment of control elements.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AFTERBODY SECTION OF AIR-DYNAMIC STEERING GEARS FOR CONTROLLED AIRCRAFTS (PREFERABLY FOR CONTROLLED AERIAL BOMBS) AND AIR ACTUATOR OF STEERING GEAR | 2009 |
|
RU2418261C2 |
| GUIDED PROJECTILE | 2016 |
|
RU2645322C1 |
| CONTROLLED PROJECTILE | 2007 |
|
RU2354922C1 |
| AERODYNAMIC CONTROL SURFACE OF GUIDED MISSILE | 2005 |
|
RU2289779C1 |
| GUIDED MISSILE | 1998 |
|
RU2135946C1 |
| METHOD FOR CONTROL OF MOVING VEHICLE AND CONTROLLED VEHICLE (MODIFICATIONS) | 2002 |
|
RU2222772C2 |
| METHOD TO CONTROL MOVEMENT OF VEHICLE CONVERTIBLE INTO AIRCRAFT AND DESIGN OF SUCH VEHICLE | 1999 |
|
RU2169085C1 |
| UNMANNED AERIAL VEHICLE | 2023 |
|
RU2812164C1 |
| UNMANNED FLYING VEHICLE | 2005 |
|
RU2288140C1 |
| MULTI-SCREW UNMANNED ROTORCRAFT | 2016 |
|
RU2611480C1 |
