GB580715A - Improvements relating to aircraft controls - Google Patents

Improvements relating to aircraft controls

Info

Publication number
GB580715A
GB580715A GB2030144A GB2030144A GB580715A GB 580715 A GB580715 A GB 580715A GB 2030144 A GB2030144 A GB 2030144A GB 2030144 A GB2030144 A GB 2030144A GB 580715 A GB580715 A GB 580715A
Authority
GB
United Kingdom
Prior art keywords
nut
engaging
rotation
unlike
control
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB2030144A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JERZY STANISLAW RUDLICKI
Original Assignee
JERZY STANISLAW RUDLICKI
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 JERZY STANISLAW RUDLICKI filed Critical JERZY STANISLAW RUDLICKI
Priority to GB2030144A priority Critical patent/GB580715A/en
Publication of GB580715A publication Critical patent/GB580715A/en
Expired legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Transmission Devices (AREA)

Abstract

580,715. Screw mechanism. RUDLICKI, J. S. Oct. 19, 1944, No. 20301. [Class 80 (iii)] [Also in Group XXXIII] An aircraft control mechanism for simultaneous operation of two surfaces in unison or in opposition comprises two members 3, 4 connected with the respective control surfaces and provided with oppositely threaded parts 23, 24 engaged by a single nut 14. Rotation of the nut 14 causes equal and like rotation of the control members 3 and 4 which axial movement of the nut causes equal and opposite rotations of the control members. The nut 14 is rotated by an arm 13 connected by cables or rods to the elevation control lever, and is moved axially by a nut 11 engaging a thread 10 on the fixed casing 78 engaging the nut 14 through the shoulders 16, the nut 11 being turned by an arm 12 secured thereto and connected by a linkage to the rudder bar. The arms 3, 4 are connected by cables or rods to surfaces as described in Specification 379,554, [Group XXXIII], so that their rotation in like or unlike senses causes like or unlike operation of the surfaces. The like and unlike operations may occur simultaneously. The above mechanism may alternatively be turned inside-out, the axles 1, 2 being replaced by hubs in screwed engagement with a hollow sleeve 14 secured against axial movement relative to an internal nut 11 engaging a thread 10 on a fixed central axle 7.
GB2030144A 1944-10-19 1944-10-19 Improvements relating to aircraft controls Expired GB580715A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2030144A GB580715A (en) 1944-10-19 1944-10-19 Improvements relating to aircraft controls

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2030144A GB580715A (en) 1944-10-19 1944-10-19 Improvements relating to aircraft controls

Publications (1)

Publication Number Publication Date
GB580715A true GB580715A (en) 1946-09-17

Family

ID=10143713

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2030144A Expired GB580715A (en) 1944-10-19 1944-10-19 Improvements relating to aircraft controls

Country Status (1)

Country Link
GB (1) GB580715A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3266754A (en) * 1961-03-06 1966-08-16 Boeing Co Control system
GB2359286A (en) * 2000-02-10 2001-08-22 Franklin Zee A vehicle,e.g.a remote controlled toy or model aircraft, a piloted aircraft or glider, or a land- or water-borne vehicle,having a V-shaped tail
CN105151281A (en) * 2015-09-28 2015-12-16 哈尔滨工业大学深圳研究生院 Pitching and yawing conditional decoupling empennage regulating mechanism for aircraft
CN105151280A (en) * 2015-09-28 2015-12-16 哈尔滨工业大学深圳研究生院 Aircraft empennage regulation mechanism with pitching and yawing completely decoupled

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3266754A (en) * 1961-03-06 1966-08-16 Boeing Co Control system
GB2359286A (en) * 2000-02-10 2001-08-22 Franklin Zee A vehicle,e.g.a remote controlled toy or model aircraft, a piloted aircraft or glider, or a land- or water-borne vehicle,having a V-shaped tail
GB2359286B (en) * 2000-02-10 2004-03-03 Franklin Zee A remote controlled vehicle with linked primary and secondary control flaps
CN105151281A (en) * 2015-09-28 2015-12-16 哈尔滨工业大学深圳研究生院 Pitching and yawing conditional decoupling empennage regulating mechanism for aircraft
CN105151280A (en) * 2015-09-28 2015-12-16 哈尔滨工业大学深圳研究生院 Aircraft empennage regulation mechanism with pitching and yawing completely decoupled
CN105151280B (en) * 2015-09-28 2017-04-26 哈尔滨工业大学深圳研究生院 Aircraft empennage regulation mechanism with pitching and yawing completely decoupled
CN105151281B (en) * 2015-09-28 2017-04-26 哈尔滨工业大学深圳研究生院 Pitching and yawing conditional decoupling empennage regulating mechanism for aircraft

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