GB584700A - Improvements in or relating to control flaps or tabs for aircraft - Google Patents

Improvements in or relating to control flaps or tabs for aircraft

Info

Publication number
GB584700A
GB584700A GB2136044A GB2136044A GB584700A GB 584700 A GB584700 A GB 584700A GB 2136044 A GB2136044 A GB 2136044A GB 2136044 A GB2136044 A GB 2136044A GB 584700 A GB584700 A GB 584700A
Authority
GB
United Kingdom
Prior art keywords
control member
eccentrics
movement
link
tab
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
GB2136044A
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.)
LAWRENCE BOYDEN
REUBEN WATKIN SHORT
Original Assignee
LAWRENCE BOYDEN
REUBEN WATKIN SHORT
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 LAWRENCE BOYDEN, REUBEN WATKIN SHORT filed Critical LAWRENCE BOYDEN
Priority to GB2136044A priority Critical patent/GB584700A/en
Publication of GB584700A publication Critical patent/GB584700A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements

Landscapes

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

Abstract

584,700. Controlling aircraft. SPURR, E., SHORT, R. W., TAYLOR, B., and BOYDEN, L. Nov. 1, 1944, No. 21360. [Class 4] Control means for a balance or trimming tab 5 is provided within the structure of the control surface 4, and comprises eccentrics 2, 2a, mounted at the pivotal axes of the main control member 4 and tab respectively, a link 10 connecting the eccentrics such that movement of the control member eccentric, or movement of the link with the control member; causes an angular setting of the tab in relation to the main control member. -Movement of the control member eccentric 2 may be effected by a lever 12 operated by a control lever in the pilot's cockpit. The eccentrics 2, 2a may be set parallel to one another and in the same direction, to give a parallelogram motion, as shown, or may be set in opposite directions. In order to prevent the transmission of load to the fixed portion of the wing structure 8, the connecting link 10 may be enclosed in a sleeve 11, the. ends of which are anchored to the pivotal axes of the eccentrics.
GB2136044A 1944-11-01 1944-11-01 Improvements in or relating to control flaps or tabs for aircraft Expired GB584700A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2136044A GB584700A (en) 1944-11-01 1944-11-01 Improvements in or relating to control flaps or tabs for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2136044A GB584700A (en) 1944-11-01 1944-11-01 Improvements in or relating to control flaps or tabs for aircraft

Publications (1)

Publication Number Publication Date
GB584700A true GB584700A (en) 1947-01-21

Family

ID=10161590

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2136044A Expired GB584700A (en) 1944-11-01 1944-11-01 Improvements in or relating to control flaps or tabs for aircraft

Country Status (1)

Country Link
GB (1) GB584700A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106986004A (en) * 2017-03-02 2017-07-28 中国航空研究院 A kind of servo-actuated synergistic device of rudder of aircraft
US20240076030A1 (en) * 2022-09-01 2024-03-07 Airbus Operations Gmbh Trailing edge system for a wing of an aircraft, method of operating control surfaces of an aircraft, aircraft wing and aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106986004A (en) * 2017-03-02 2017-07-28 中国航空研究院 A kind of servo-actuated synergistic device of rudder of aircraft
US20240076030A1 (en) * 2022-09-01 2024-03-07 Airbus Operations Gmbh Trailing edge system for a wing of an aircraft, method of operating control surfaces of an aircraft, aircraft wing and aircraft

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