GB558044A - Improvements relating to aircraft wing flaps - Google Patents

Improvements relating to aircraft wing flaps

Info

Publication number
GB558044A
GB558044A GB10158/42A GB1015842A GB558044A GB 558044 A GB558044 A GB 558044A GB 10158/42 A GB10158/42 A GB 10158/42A GB 1015842 A GB1015842 A GB 1015842A GB 558044 A GB558044 A GB 558044A
Authority
GB
United Kingdom
Prior art keywords
flap
flaps
wing
aircraft wing
improvements relating
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
GB10158/42A
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.)
Sir WG Armstrong Whitworth and Co Engineers Ltd
Sir WG Armstrong Whitworth Aircraft Ltd
Original Assignee
Sir WG Armstrong Whitworth and Co Engineers Ltd
Sir WG Armstrong Whitworth Aircraft 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 Sir WG Armstrong Whitworth and Co Engineers Ltd, Sir WG Armstrong Whitworth Aircraft Ltd filed Critical Sir WG Armstrong Whitworth and Co Engineers Ltd
Priority to GB10158/42A priority Critical patent/GB558044A/en
Publication of GB558044A publication Critical patent/GB558044A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areasĀ or the like
    • B64C21/08Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areasĀ or the like adjustable
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)

Abstract

558,044. Controlling aircraft. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., Sir W. G., and LLOYD, J. July 21, 1942, No. 10158. Drawings to Specification. [Class 4] An aeroplane has flaps extending substantially the whole length of the trailing edge of the wing the inboard flap being movable rearwardly or rearwardly and downwardly to a greater extent than any of the others. A wing having two flaps is described, the inboard flap being movable rearwardly about 30 per cent of the average wing chord of the section on which the flap is mounted and the outboard flap about 25 per cent of the average chord of the corresponding section. The flaps may be mounted on convergent links as described in Specification 558,043 and the outer flap has an aileron which may be operated as described in that Specification or as described in Specification 558,045.
GB10158/42A 1942-07-21 1942-07-21 Improvements relating to aircraft wing flaps Expired GB558044A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10158/42A GB558044A (en) 1942-07-21 1942-07-21 Improvements relating to aircraft wing flaps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10158/42A GB558044A (en) 1942-07-21 1942-07-21 Improvements relating to aircraft wing flaps

Publications (1)

Publication Number Publication Date
GB558044A true GB558044A (en) 1943-12-16

Family

ID=9962599

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10158/42A Expired GB558044A (en) 1942-07-21 1942-07-21 Improvements relating to aircraft wing flaps

Country Status (1)

Country Link
GB (1) GB558044A (en)

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