DE602005008138D1 - Vorflügel für ein Flugzeug und entsprechende Verfahren - Google Patents

Vorflügel für ein Flugzeug und entsprechende Verfahren

Info

Publication number
DE602005008138D1
DE602005008138D1 DE602005008138T DE602005008138T DE602005008138D1 DE 602005008138 D1 DE602005008138 D1 DE 602005008138D1 DE 602005008138 T DE602005008138 T DE 602005008138T DE 602005008138 T DE602005008138 T DE 602005008138T DE 602005008138 D1 DE602005008138 D1 DE 602005008138D1
Authority
DE
Germany
Prior art keywords
extended position
aircraft
leading edge
slat
edge device
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
DE602005008138T
Other languages
English (en)
Inventor
Scott N Rampton
Stephen R Amorosi
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
Application filed by Boeing Co filed Critical Boeing Co
Publication of DE602005008138D1 publication Critical patent/DE602005008138D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C9/22Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • 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
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
  • Discharge By Other Means (AREA)
  • Transmission Devices (AREA)
  • Moulding By Coating Moulds (AREA)
  • Circuits Of Receivers In General (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Paper (AREA)
  • Measuring Pulse, Heart Rate, Blood Pressure Or Blood Flow (AREA)
DE602005008138T 2004-06-15 2005-04-15 Vorflügel für ein Flugzeug und entsprechende Verfahren Active DE602005008138D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/868,234 US7270305B2 (en) 2004-06-15 2004-06-15 Aircraft leading edge apparatuses and corresponding methods

Publications (1)

Publication Number Publication Date
DE602005008138D1 true DE602005008138D1 (de) 2008-08-28

Family

ID=34938173

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005008138T Active DE602005008138D1 (de) 2004-06-15 2005-04-15 Vorflügel für ein Flugzeug und entsprechende Verfahren

Country Status (5)

Country Link
US (1) US7270305B2 (de)
EP (1) EP1607324B8 (de)
AT (1) ATE401239T1 (de)
DE (1) DE602005008138D1 (de)
ES (1) ES2308372T3 (de)

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US8424810B1 (en) 2010-03-31 2013-04-23 The Boeing Company Low noise wing slat system with rigid cove-filled slat
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CN102642615A (zh) * 2012-05-11 2012-08-22 中国航空工业集团公司西安飞机设计研究所 一种带单缝襟翼的飞机增升装置
ES2728917T3 (es) * 2014-06-12 2019-10-29 Airbus Operations Gmbh Dispositivo de borde de salida de variación progresiva de un perfil aerodinámico
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EP3241740B1 (de) * 2016-05-03 2020-08-19 Airbus Operations GmbH System zur ansteuerung einer vorflügelvorrichtung eines flugzeugflügels
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EP3575206A1 (de) * 2018-06-01 2019-12-04 Airbus Operations GmbH System zum antrieb einer klappenanordnung zwischen einer eingezogenen position und einer erweiterten position
EP3594108B1 (de) * 2018-07-12 2021-12-08 Airbus Operations GmbH System zum antrieb einer klappenanordnung zwischen einer eingezogenen position und einer ausgefahrenen position
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ATE401239T1 (de) 2008-08-15
US7270305B2 (en) 2007-09-18
ES2308372T3 (es) 2008-12-01
EP1607324B1 (de) 2008-07-16
EP1607324B8 (de) 2008-08-20
EP1607324A1 (de) 2005-12-21

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