DE602006010322D1 - Tragflächenklappungsvorrichtungen für ein luftfahrzeug und entsprechende verfahren - Google Patents

Tragflächenklappungsvorrichtungen für ein luftfahrzeug und entsprechende verfahren

Info

Publication number
DE602006010322D1
DE602006010322D1 DE602006010322T DE602006010322T DE602006010322D1 DE 602006010322 D1 DE602006010322 D1 DE 602006010322D1 DE 602006010322 T DE602006010322 T DE 602006010322T DE 602006010322 T DE602006010322 T DE 602006010322T DE 602006010322 D1 DE602006010322 D1 DE 602006010322D1
Authority
DE
Germany
Prior art keywords
flow body
airfoil
gap
leading edge
aircraft
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.)
Active
Application number
DE602006010322T
Other languages
English (en)
Inventor
Christopher A Konings
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.)
Boeing Co
Original Assignee
Boeing Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=36525236&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE602006010322(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Publication of DE602006010322D1 publication Critical patent/DE602006010322D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/146—Aerofoil profile comprising leading edges of particular shape
    • 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
    • B64C2009/143—Adjustable 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Radar Systems Or Details Thereof (AREA)
DE602006010322T 2005-01-31 2006-01-17 Tragflächenklappungsvorrichtungen für ein luftfahrzeug und entsprechende verfahren Active DE602006010322D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/048,320 US7322547B2 (en) 2005-01-31 2005-01-31 Aerospace vehicle leading edge slat devices and corresponding methods
PCT/US2006/001602 WO2006083547A1 (en) 2005-01-31 2006-01-17 Aerospace vehicle leading edge slat devices and corresponding methods

Publications (1)

Publication Number Publication Date
DE602006010322D1 true DE602006010322D1 (de) 2009-12-24

Family

ID=36525236

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006010322T Active DE602006010322D1 (de) 2005-01-31 2006-01-17 Tragflächenklappungsvorrichtungen für ein luftfahrzeug und entsprechende verfahren

Country Status (5)

Country Link
US (1) US7322547B2 (de)
EP (1) EP1843942B2 (de)
AT (1) ATE448140T1 (de)
DE (1) DE602006010322D1 (de)
WO (1) WO2006083547A1 (de)

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US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
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US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
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US8534610B1 (en) * 2009-07-17 2013-09-17 The Boeing Company Method and apparatus for a leading edge slat on a wing of an aircraft
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US9688384B1 (en) * 2012-09-20 2017-06-27 The Boeing Company Methods and apparatus to control a gap between movable aircraft wing components
US9254909B2 (en) * 2013-09-24 2016-02-09 The Boeing Company Optimized flap positioning for go-around operations
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US11242130B2 (en) * 2019-03-26 2022-02-08 Yaborä Indústria Aeronáutica S.A. Shuttering mechanism for wing slat telescopic tube duct
US11235854B2 (en) * 2019-04-01 2022-02-01 Yaborä Indústria Aeronáutica S.A. Shutter door mechanism for wing leading edge slat cut-outs
US10751583B1 (en) 2019-04-16 2020-08-25 ESS 2 Tech, LLC Golf club head with airfoil
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EP1843942B2 (de) 2016-02-10
EP1843942A1 (de) 2007-10-17
US7322547B2 (en) 2008-01-29
ATE448140T1 (de) 2009-11-15
US20060169847A1 (en) 2006-08-03
EP1843942B1 (de) 2009-11-11
WO2006083547A1 (en) 2006-08-10

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