GB272455A - Improvements in apparatus for varying the flow on the wings of aeroplanes - Google Patents

Improvements in apparatus for varying the flow on the wings of aeroplanes

Info

Publication number
GB272455A
GB272455A GB9739/27A GB973927A GB272455A GB 272455 A GB272455 A GB 272455A GB 9739/27 A GB9739/27 A GB 9739/27A GB 973927 A GB973927 A GB 973927A GB 272455 A GB272455 A GB 272455A
Authority
GB
United Kingdom
Prior art keywords
wing
flaps
varying
dornier
steering
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
GB9739/27A
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.)
Dornier Metallbauten GmbH
Original Assignee
Dornier Metallbauten GmbH
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 Dornier Metallbauten GmbH filed Critical Dornier Metallbauten GmbH
Publication of GB272455A publication Critical patent/GB272455A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air-Flow Control Members (AREA)

Abstract

272,455. Dornier, C., and Dornier Metallbauten Ges. June 14, 1926, [Convention date]. Steering and balancing.-To vary the airflow over an aeroplane wing for varying the flight speed or for steering, flaps b normally lying flush with the wing surface are pivoted at their edges about transverse axes away from the leading edge of the wing and are movable separately or simultaneously into the airstream. The flaps may be arranged along the upper surface or along both surfaces of the wing, or two flaps may be arranged at sensitive places, one a short dis. tance behind the leading edge on the lower surface and the other on the upper surface a short distance forward of the trailing edge.
GB9739/27A 1926-06-14 1927-04-08 Improvements in apparatus for varying the flow on the wings of aeroplanes Expired GB272455A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE272455X 1926-06-14

Publications (1)

Publication Number Publication Date
GB272455A true GB272455A (en) 1927-12-01

Family

ID=6010316

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9739/27A Expired GB272455A (en) 1926-06-14 1927-04-08 Improvements in apparatus for varying the flow on the wings of aeroplanes

Country Status (1)

Country Link
GB (1) GB272455A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2428936A (en) * 1943-09-10 1947-10-14 Goodrich Co B F Aerodynamic brake
US2450709A (en) * 1943-02-22 1948-10-05 Lockheed Aircraft Corp Aircraft control
US3166272A (en) * 1963-10-28 1965-01-19 Boeing Co Mixing mechanism
US4046338A (en) * 1975-10-14 1977-09-06 Kline Richard L Airfoil for aircraft having improved lift generating device
FR2590045A1 (en) * 1985-11-13 1987-05-15 Lipp Robert Self steering device of a profiled-winged element, blade, vane, wing for maximum thrust by automatic monitoring of its equilibrium in the flow of a fluid
US4955958A (en) * 1987-09-26 1990-09-11 Mbb Gmbh Aircraft
GB2345894A (en) * 1999-01-20 2000-07-26 Francis Bernard Mclarney A method of roll control for aeroplanes
US10807708B2 (en) 2015-10-30 2020-10-20 Bae Systems Plc Air vehicle and imaging apparatus therefor
US10814972B2 (en) 2015-10-30 2020-10-27 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US10822084B2 (en) 2015-10-30 2020-11-03 Bae Systems Plc Payload launch apparatus and method
US11059562B2 (en) 2015-10-30 2021-07-13 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US11077943B2 (en) 2015-10-30 2021-08-03 Bae Systems Plc Rotary-wing air vehicle and method and apparatus for launch and recovery thereof

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450709A (en) * 1943-02-22 1948-10-05 Lockheed Aircraft Corp Aircraft control
US2428936A (en) * 1943-09-10 1947-10-14 Goodrich Co B F Aerodynamic brake
US3166272A (en) * 1963-10-28 1965-01-19 Boeing Co Mixing mechanism
US4046338A (en) * 1975-10-14 1977-09-06 Kline Richard L Airfoil for aircraft having improved lift generating device
FR2590045A1 (en) * 1985-11-13 1987-05-15 Lipp Robert Self steering device of a profiled-winged element, blade, vane, wing for maximum thrust by automatic monitoring of its equilibrium in the flow of a fluid
US4955958A (en) * 1987-09-26 1990-09-11 Mbb Gmbh Aircraft
GB2345894A (en) * 1999-01-20 2000-07-26 Francis Bernard Mclarney A method of roll control for aeroplanes
US10807708B2 (en) 2015-10-30 2020-10-20 Bae Systems Plc Air vehicle and imaging apparatus therefor
US10814972B2 (en) 2015-10-30 2020-10-27 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US10822084B2 (en) 2015-10-30 2020-11-03 Bae Systems Plc Payload launch apparatus and method
US11059562B2 (en) 2015-10-30 2021-07-13 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US11077943B2 (en) 2015-10-30 2021-08-03 Bae Systems Plc Rotary-wing air vehicle and method and apparatus for launch and recovery thereof

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