GB530718A - Improvements in and relating to aircraft wings - Google Patents

Improvements in and relating to aircraft wings

Info

Publication number
GB530718A
GB530718A GB18957/39A GB1895739A GB530718A GB 530718 A GB530718 A GB 530718A GB 18957/39 A GB18957/39 A GB 18957/39A GB 1895739 A GB1895739 A GB 1895739A GB 530718 A GB530718 A GB 530718A
Authority
GB
United Kingdom
Prior art keywords
air
wing
discharge
apertures
intake
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
GB18957/39A
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.)
Airbus Defence and Space GmbH
Junkers Flugzeug und Motorenwerke AG
Original Assignee
Messerschmitt Bolkow Blohm AG
Junkers Flugzeug und Motorenwerke AG
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 Messerschmitt Bolkow Blohm AG, Junkers Flugzeug und Motorenwerke AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB530718A publication Critical patent/GB530718A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

530,718. Reducing surface friction between a body and a fluid. JUNKERS FLUGZEUG - UND - MOTORENWERKE, AKT.- GES. June 29, 1939, No. 18957. Convention date, July 11, 1938. [Class 4] Means for the intake or discharge of air at the boundary layer of an aircraft wing includes means so arranged that a different intake or discharge of air takes place over adjacent areas of a wing. As shown, air is taken in through a conduit having apertures 4 which are disposed adjacent the hinge axis of a movable surface on the wing. The apertures nearer the fuselage are smaller than those more remote or alternatively, are formed of wire netting of smaller mesh.
GB18957/39A 1938-07-11 1939-06-29 Improvements in and relating to aircraft wings Expired GB530718A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE530718X 1938-07-11

Publications (1)

Publication Number Publication Date
GB530718A true GB530718A (en) 1940-12-18

Family

ID=6554625

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18957/39A Expired GB530718A (en) 1938-07-11 1939-06-29 Improvements in and relating to aircraft wings

Country Status (1)

Country Link
GB (1) GB530718A (en)

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