GB2100684B - Flap arrangement for the leading edge of an aircraft wing - Google Patents

Flap arrangement for the leading edge of an aircraft wing

Info

Publication number
GB2100684B
GB2100684B GB08215918A GB8215918A GB2100684B GB 2100684 B GB2100684 B GB 2100684B GB 08215918 A GB08215918 A GB 08215918A GB 8215918 A GB8215918 A GB 8215918A GB 2100684 B GB2100684 B GB 2100684B
Authority
GB
United Kingdom
Prior art keywords
leading edge
aircraft wing
flap arrangement
flap
arrangement
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
GB08215918A
Other versions
GB2100684A (en
Inventor
Werner Staudacher
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
Original Assignee
Messerschmitt Bolkow Blohm 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 filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB2100684A publication Critical patent/GB2100684A/en
Application granted granted Critical
Publication of GB2100684B publication Critical patent/GB2100684B/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
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/26—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by multiple flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Prostheses (AREA)
  • Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
  • Air-Flow Control Members (AREA)
GB08215918A 1981-06-04 1982-06-01 Flap arrangement for the leading edge of an aircraft wing Expired GB2100684B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19813122137 DE3122137A1 (en) 1981-06-04 1981-06-04 FRONT EDGE FLAP SYSTEM FOR PLANE WINGS

Publications (2)

Publication Number Publication Date
GB2100684A GB2100684A (en) 1983-01-06
GB2100684B true GB2100684B (en) 1984-12-05

Family

ID=6133868

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08215918A Expired GB2100684B (en) 1981-06-04 1982-06-01 Flap arrangement for the leading edge of an aircraft wing

Country Status (3)

Country Link
DE (1) DE3122137A1 (en)
FR (1) FR2507148A1 (en)
GB (1) GB2100684B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3177060D1 (en) * 1981-06-10 1989-10-05 Boeing Co Leading edge vortex flap for wings
US7204454B2 (en) 2005-02-25 2007-04-17 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
US7216835B2 (en) * 2005-02-25 2007-05-15 Northrop Grumman Corporation Aircraft with extendable leading edge of fuselage and wings
US7246770B2 (en) * 2005-02-25 2007-07-24 Northrop Grumman Corporation Aircraft with rotatable leading edge of fuselage and wings
GB2527001A (en) * 2013-04-15 2015-12-09 Christian Emmanuel Norden A transition arrangement for an aircraft
GB2579221A (en) * 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft control mechanism

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047257A (en) * 1958-04-24 1962-07-31 Martin Marietta Corp Device for changing airfoil profile
DE2751361C2 (en) * 1977-11-17 1984-09-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München A method for controlling aircraft by controlling detached wing leading edge eddy currents
US4293110A (en) * 1979-03-08 1981-10-06 The Boeing Company Leading edge vortex flap for wings

Also Published As

Publication number Publication date
FR2507148A1 (en) 1982-12-10
FR2507148B1 (en) 1985-03-08
GB2100684A (en) 1983-01-06
DE3122137C2 (en) 1987-06-25
DE3122137A1 (en) 1982-12-23

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee