UA79830U - Control drive of moving aircraft airfoil wing - Google Patents
Control drive of moving aircraft airfoil wingInfo
- Publication number
- UA79830U UA79830U UAU201303055U UAU201303055U UA79830U UA 79830 U UA79830 U UA 79830U UA U201303055 U UAU201303055 U UA U201303055U UA U201303055 U UAU201303055 U UA U201303055U UA 79830 U UA79830 U UA 79830U
- Authority
- UA
- Ukraine
- Prior art keywords
- wing
- airfoil
- aircraft
- control drive
- fuselage
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A control drive of a moving aircraft airfoil wing attached to the fixed airfoil relative to the fuselage with possibility of its turning comprises a propeller mounted in the aircraft aerodynamic surface fixed relative to the fuselage with an output rotating unit connected to the movable wing airfoil. As a propeller a servo drive is used, an output rotating unit is made in the form of at least one torsion bar, whose one end is connected to the servo drive shaft and passes through a thrust bearing and a roller mounted in a slider bearing, which has a rectangular opening, a torsion bar has at least one bend, whose axis of rotation coincides with the axis of rotation of the movable aerodynamic surface of the aircraft wing and is mounted in a bearing roller with possibility of describe a conical surface and by interaction with a mobile airfoil wing to change its angular position.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAU201303055U UA79830U (en) | 2013-03-12 | 2013-03-12 | Control drive of moving aircraft airfoil wing |
PCT/UA2013/000058 WO2014142773A1 (en) | 2013-03-12 | 2013-06-10 | Drive for controlling a moveable aerodynamic surface of an aircraft wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAU201303055U UA79830U (en) | 2013-03-12 | 2013-03-12 | Control drive of moving aircraft airfoil wing |
Publications (1)
Publication Number | Publication Date |
---|---|
UA79830U true UA79830U (en) | 2013-04-25 |
Family
ID=51537221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAU201303055U UA79830U (en) | 2013-03-12 | 2013-03-12 | Control drive of moving aircraft airfoil wing |
Country Status (2)
Country | Link |
---|---|
UA (1) | UA79830U (en) |
WO (1) | WO2014142773A1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3958779A (en) * | 1975-05-27 | 1976-05-25 | Fairchild Industries Inc. | Aircraft control system with a jam isolating coupling |
US6244542B1 (en) * | 1999-07-20 | 2001-06-12 | Northrop Grumman Corporation | Rotor driven edge |
US6467733B1 (en) * | 2001-11-28 | 2002-10-22 | Northrop Grumman Corporation | Aerodynamic control surface system |
ES2345584B1 (en) * | 2007-12-21 | 2011-07-18 | Airbus Operations, S.L. | AIRCRAFT CONTROL SURFACE. |
-
2013
- 2013-03-12 UA UAU201303055U patent/UA79830U/en unknown
- 2013-06-10 WO PCT/UA2013/000058 patent/WO2014142773A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2014142773A1 (en) | 2014-09-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CY1122262T1 (en) | VERTICAL AXIS TURBINE | |
MX362864B (en) | Landing gear drive system. | |
MX2015005606A (en) | An airplane wing, an airplane and a flap system. | |
GB201117340D0 (en) | Flat support | |
BR112016006370A2 (en) | Method for controlling the operation of an aircraft turboprop engine engine and turboprop engine control system | |
JP2016502017A5 (en) | ||
RU2017110703A (en) | MULTICOPTER WITH A SWIVEL WING | |
WO2009025231A1 (en) | Helicopter | |
NZ706696A (en) | Vertical take-off and landing aircraft | |
UA100763C2 (en) | Aircraft with coaxial counter-rotating sustaining rotors without cyclic change of pitch equipped with means of aerodynamic control of position and trajectory of flight | |
GB201209686D0 (en) | A slat support assembly | |
CN203767067U (en) | Centre-of-gravity shift yawing device for helicopters | |
WO2017123347A3 (en) | Feathering propeller clutch mechanisms | |
NZ761896A (en) | Bistable pitch propeller system with bidirectional propeller rotation | |
WO2012076705A3 (en) | Aircraft rotor comprising rotary wings | |
EP4324636A3 (en) | Actuator with variable speed servo motor for redraw assembly | |
UA79830U (en) | Control drive of moving aircraft airfoil wing | |
CN203996872U (en) | A kind of unmanned airplane empennage balance adjusting structure | |
HRP20120045A2 (en) | Wind turbine with horizontal parallelogram of lever for transitional motion of blades | |
WO2016200458A3 (en) | Mono-cyclic swashplate | |
RU2009117369A (en) | MOTORCRAFT SCREWS OF Aircraft Wing | |
UA117784C2 (en) | Aerodynamic device | |
CN104002969B (en) | A kind of rotary flapping wing thrust generating apparatus with spring | |
CN203845007U (en) | Rotatable flapping wing thrust generation device with spring | |
CN203127146U (en) | Ring-shaped aircraft with power |