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UA79830U - Control drive of moving aircraft airfoil wing - Google Patents

Control drive of moving aircraft airfoil wing

Info

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
Application number
UAU201303055U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Юрий Григорьевич Сидоренко
Георгий Владимирович Бейлин
Сергей Юриевич Петренко
Original Assignee
Юрий Григорьевич Сидоренко
Георгий Владимирович Бейлин
Сергей Юриевич Петренко
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Юрий Григорьевич Сидоренко, Георгий Владимирович Бейлин, Сергей Юриевич Петренко filed Critical Юрий Григорьевич Сидоренко
Priority to UAU201303055U priority Critical patent/UA79830U/en
Publication of UA79830U publication Critical patent/UA79830U/en
Priority to PCT/UA2013/000058 priority patent/WO2014142773A1/en

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.
UAU201303055U 2013-03-12 2013-03-12 Control drive of moving aircraft airfoil wing UA79830U (en)

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)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN219056616U (en) * 2022-11-25 2023-05-23 峰飞航空科技(昆山)有限公司 Connecting rod assembly, steering engine buffer structure and aircraft

Family Cites Families (4)

* Cited by examiner, † Cited by third party
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.

Also Published As

Publication number Publication date
WO2014142773A1 (en) 2014-09-18

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