GB520962A - Improvements in or relating to means for balancing the control surfaces of aircraft - Google Patents

Improvements in or relating to means for balancing the control surfaces of aircraft

Info

Publication number
GB520962A
GB520962A GB3203638A GB3203638A GB520962A GB 520962 A GB520962 A GB 520962A GB 3203638 A GB3203638 A GB 3203638A GB 3203638 A GB3203638 A GB 3203638A GB 520962 A GB520962 A GB 520962A
Authority
GB
United Kingdom
Prior art keywords
chamber
leading edge
aircraft
openings
balancing
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
GB3203638A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB3203638A priority Critical patent/GB520962A/en
Publication of GB520962A publication Critical patent/GB520962A/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
    • B64C9/02—Mounting or supporting thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Check Valves (AREA)

Abstract

520,962. Aircraft controls. FAIREY AVIATION CO., Ltd., and YOUNGMAN, R. T. Nov. 4, 1938, No. 32036. [Class 4] An aircraft control surface has its hinge set back from the leading edge which extends into a chamber in a wing &c. the chamber being formed with a central opening communicating with one or more openings at or near the leading edge of the wing. As shown, the tail fin 11 is formed with a chamber 12 in which extends the leading edge of the rudder 13, the chamber being formed with a central opening 15 communicating with one or more openings at or near the leading edge which openings may be valve controlled. In its mid position the rudder closes the opening 15.
GB3203638A 1938-11-04 1938-11-04 Improvements in or relating to means for balancing the control surfaces of aircraft Expired GB520962A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3203638A GB520962A (en) 1938-11-04 1938-11-04 Improvements in or relating to means for balancing the control surfaces of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3203638A GB520962A (en) 1938-11-04 1938-11-04 Improvements in or relating to means for balancing the control surfaces of aircraft

Publications (1)

Publication Number Publication Date
GB520962A true GB520962A (en) 1940-05-08

Family

ID=10332111

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3203638A Expired GB520962A (en) 1938-11-04 1938-11-04 Improvements in or relating to means for balancing the control surfaces of aircraft

Country Status (1)

Country Link
GB (1) GB520962A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2484359A (en) * 1945-05-12 1949-10-11 Tipton Elizabeth Barrett Control booster for aircraft
FR2669995A1 (en) * 1982-05-18 1992-06-05 Onera (Off Nat Aerospatiale) Variable-effectiveness control surface for missiles, especially supersonic missiles
GB2540953A (en) * 2015-07-31 2017-02-08 Airbus Operations Ltd A control surface for an aircraft
CN109305329A (en) * 2018-10-26 2019-02-05 上海歌尔泰克机器人有限公司 The processing method of wing, unmanned vehicle and wing

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2484359A (en) * 1945-05-12 1949-10-11 Tipton Elizabeth Barrett Control booster for aircraft
FR2669995A1 (en) * 1982-05-18 1992-06-05 Onera (Off Nat Aerospatiale) Variable-effectiveness control surface for missiles, especially supersonic missiles
GB2540953A (en) * 2015-07-31 2017-02-08 Airbus Operations Ltd A control surface for an aircraft
US10279888B2 (en) 2015-07-31 2019-05-07 Airbus Operations Limited Control surface for an aircraft
CN109305329A (en) * 2018-10-26 2019-02-05 上海歌尔泰克机器人有限公司 The processing method of wing, unmanned vehicle and wing

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