GB478190A - Improvements in and relating to aircraft wings - Google Patents

Improvements in and relating to aircraft wings

Info

Publication number
GB478190A
GB478190A GB16087/36A GB1608736A GB478190A GB 478190 A GB478190 A GB 478190A GB 16087/36 A GB16087/36 A GB 16087/36A GB 1608736 A GB1608736 A GB 1608736A GB 478190 A GB478190 A GB 478190A
Authority
GB
United Kingdom
Prior art keywords
flap
wing
passage
relating
aircraft wings
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
GB16087/36A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB16087/36A priority Critical patent/GB478190A/en
Publication of GB478190A publication Critical patent/GB478190A/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 areas or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/146Adjustable control surfaces or members, e.g. rudders forming slots at an other wing location than the rear or the front
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C2009/143Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/06Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/20Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • 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
    • 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
    • Y02T50/30Wing lift efficiency

Abstract

478,190. Controlling aircraft CARDEN, A. D. June 9, 1936, No. 16087. [Class 4] A fixed wing 1 provided with a split flap 5 is formed with an air passage 3 leading from the upper surface of the wing to the space between the divided parts of the trailing edge, the upper end of passage 3 being closed by a flap 4 interconnected with the operating mechanism of flap 5 so that the passage is closed when flap 5 is raised and opened when it is lowered. The air passage may be arranged also to communicate with an aperture in the underside of the wing as at 10.
GB16087/36A 1936-06-09 1936-06-09 Improvements in and relating to aircraft wings Expired GB478190A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB16087/36A GB478190A (en) 1936-06-09 1936-06-09 Improvements in and relating to aircraft wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16087/36A GB478190A (en) 1936-06-09 1936-06-09 Improvements in and relating to aircraft wings

Publications (1)

Publication Number Publication Date
GB478190A true GB478190A (en) 1938-01-10

Family

ID=10070941

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16087/36A Expired GB478190A (en) 1936-06-09 1936-06-09 Improvements in and relating to aircraft wings

Country Status (1)

Country Link
GB (1) GB478190A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2772058A (en) * 1951-05-10 1956-11-27 Charles H Grant Aircraft wing with means to increase lift through control of air flow
CN114750930A (en) * 2022-05-07 2022-07-15 中国航空工业集团公司沈阳飞机设计研究所 Wing surface slotted spoiler type course control surface

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2772058A (en) * 1951-05-10 1956-11-27 Charles H Grant Aircraft wing with means to increase lift through control of air flow
CN114750930A (en) * 2022-05-07 2022-07-15 中国航空工业集团公司沈阳飞机设计研究所 Wing surface slotted spoiler type course control surface

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