GB748094A - Improvements in or relating to aircraft controls - Google Patents

Improvements in or relating to aircraft controls

Info

Publication number
GB748094A
GB748094A GB24323/53A GB2432353A GB748094A GB 748094 A GB748094 A GB 748094A GB 24323/53 A GB24323/53 A GB 24323/53A GB 2432353 A GB2432353 A GB 2432353A GB 748094 A GB748094 A GB 748094A
Authority
GB
United Kingdom
Prior art keywords
aileron
wing
aircraft
torsion bar
pivoted
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
GB24323/53A
Inventor
William John Strang
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB24323/53A priority Critical patent/GB748094A/en
Publication of GB748094A publication Critical patent/GB748094A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

748,094. Aircraft ailerons. BRISTOL AEROPLANE CO., Ltd. Aug. 27, 1954 [Sept. 2, 1953], No. 24323/53. Class 4. A fixed wing aircraft has ailerons 11, each operated by at least one servo tab 12, and resilient means urging each aileron downwardly so as to reduce or eliminate the tendency of the aileron to be deflected upwardly from the position in which it forms a smooth continuation of the wing, when the aileron is left free to set itself in normal flight. As shown, the aileron is formed with a portion 13 penetrating into a compartment in the wing 10 and, with a flexible sealing strip 15, divides the said compartment into two parts communicating with the upper and lower surfaces of the wing. The flap 12 is similarly arranged on the aileron. A torsion bar 18 extending parallel to the pivot axis 14 has one end fast with the aileron, and the other journalled in a bearing 22 in the portion 13 and fast to a link 19 pivoted to a further link 20 pivoted to the wing at 21, so that deflection of the aileron twists the torsion bar 18. When the aircraft is stationary or at landing or take-off speed, the bar 18 deflects the aileron to its downmost position, giving high lift. In normal flight, the aileron if left free, assumes a position which renders it a smooth continuation of the wing. The torsion bar assists in mass balancing the aileron.
GB24323/53A 1953-09-02 1953-09-02 Improvements in or relating to aircraft controls Expired GB748094A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB24323/53A GB748094A (en) 1953-09-02 1953-09-02 Improvements in or relating to aircraft controls

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24323/53A GB748094A (en) 1953-09-02 1953-09-02 Improvements in or relating to aircraft controls

Publications (1)

Publication Number Publication Date
GB748094A true GB748094A (en) 1956-04-18

Family

ID=10209898

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24323/53A Expired GB748094A (en) 1953-09-02 1953-09-02 Improvements in or relating to aircraft controls

Country Status (1)

Country Link
GB (1) GB748094A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8292236B2 (en) 2008-04-23 2012-10-23 Airbus Operations Limited Flight surface seal
CN113830286A (en) * 2021-09-18 2021-12-24 中国商用飞机有限责任公司 Aileron actuation structure and wing comprising an aileron actuation structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8292236B2 (en) 2008-04-23 2012-10-23 Airbus Operations Limited Flight surface seal
CN113830286A (en) * 2021-09-18 2021-12-24 中国商用飞机有限责任公司 Aileron actuation structure and wing comprising an aileron actuation structure

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