ATE496826T1 - Schlitzflügel für flugzeug - Google Patents

Schlitzflügel für flugzeug

Info

Publication number
ATE496826T1
ATE496826T1 AT03799834T AT03799834T ATE496826T1 AT E496826 T1 ATE496826 T1 AT E496826T1 AT 03799834 T AT03799834 T AT 03799834T AT 03799834 T AT03799834 T AT 03799834T AT E496826 T1 ATE496826 T1 AT E496826T1
Authority
AT
Austria
Prior art keywords
airfoil element
slot
airplane
wing
wingspan
Prior art date
Application number
AT03799834T
Other languages
English (en)
Inventor
Lie-Mine Gea
James Mclean
David Witkowski
Steven Krist
Richard Campbell
John Vassberg
Original Assignee
Boeing Co
Us Of America Represented By The Administrator Of The Nat Aeronautics And Space Administration Nasa
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=32717271&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ATE496826(T1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co, Us Of America Represented By The Administrator Of The Nat Aeronautics And Space Administration Nasa filed Critical Boeing Co
Application granted granted Critical
Publication of ATE496826T1 publication Critical patent/ATE496826T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/149—Aerofoil profile for supercritical or transonic flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • 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)
  • Toys (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Laminated Bodies (AREA)
AT03799834T 2002-10-09 2003-10-09 Schlitzflügel für flugzeug ATE496826T1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US41735502P 2002-10-09 2002-10-09
US10/678,474 US7048228B2 (en) 2002-10-09 2003-10-03 Slotted aircraft wing
PCT/US2003/032169 WO2004041640A2 (en) 2002-10-09 2003-10-09 Slotted aircraft wing

Publications (1)

Publication Number Publication Date
ATE496826T1 true ATE496826T1 (de) 2011-02-15

Family

ID=32717271

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03799834T ATE496826T1 (de) 2002-10-09 2003-10-09 Schlitzflügel für flugzeug

Country Status (7)

Country Link
US (1) US7048228B2 (de)
EP (1) EP1558493B1 (de)
JP (1) JP2006502914A (de)
AT (1) ATE496826T1 (de)
AU (1) AU2003299548A1 (de)
DE (1) DE60335895D1 (de)
WO (1) WO2004041640A2 (de)

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US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
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US7357358B2 (en) 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US6978971B1 (en) 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7270305B2 (en) 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US8544800B2 (en) * 2005-07-21 2013-10-01 The Boeing Company Integrated wingtip extensions for jet transport aircraft and other types of aircraft
US7500641B2 (en) 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
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
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US8109473B2 (en) * 2006-05-30 2012-02-07 Israel Aerospace Industries Ltd. Slotted high lift aerofoils
IL176022A (en) * 2006-05-30 2011-11-30 Israel Aerospace Ind Ltd Wings for aircraft
US7578484B2 (en) 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US20100006695A1 (en) * 2006-09-25 2010-01-14 Michel Aguilar Vertical take-off and landing vehicle which does not have a rotary wing
US7900876B2 (en) * 2007-08-09 2011-03-08 The Boeing Company Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods
US20090084904A1 (en) * 2007-10-02 2009-04-02 The Boeing Company Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8789798B2 (en) * 2008-02-12 2014-07-29 Bombardier Inc. Slat configuration for fixed-wing aircraft
US8128035B2 (en) * 2008-04-15 2012-03-06 The Boeing Company Winglets with recessed surfaces, and associated systems and methods
US8944386B2 (en) 2011-06-09 2015-02-03 Aviation Partners, Inc. Split blended winglet
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
CN102149599B (zh) 2008-06-20 2014-11-19 航空伙伴股份有限公司 弯曲的机翼末梢
WO2010032241A1 (en) * 2008-09-17 2010-03-25 Israel Aerospace Industries Ltd. Aerofoil accessories and method for modyfying the geometry of a wing element
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
US8936219B2 (en) 2012-03-30 2015-01-20 The Boeing Company Performance-enhancing winglet system and method
US10118686B2 (en) * 2012-09-27 2018-11-06 The Boeing Company Wing root insert system for an aircraft family
IL226859A (en) * 2013-06-10 2017-09-28 Abramov Danny Slot wing with groove and wings for aircraft
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
US9511850B2 (en) 2014-04-12 2016-12-06 The Boeing Company Wing tip device for an aircraft wing
CA3028165A1 (en) 2016-06-29 2018-01-04 Bombardier Inc. Methods and systems for deploying adjacent trailing edge flaps
EP3269635A1 (de) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Flugzeugflügel
US20190057180A1 (en) * 2017-08-18 2019-02-21 International Business Machines Corporation System and method for design optimization using augmented reality
EP3511243B1 (de) * 2018-01-15 2021-12-29 The Aircraft Performance Company GmbH Flugzeugflügel
CA3037923C (en) * 2018-03-29 2025-12-09 Bombardier Inc. System and method for improving the operation of an aircraft
DE102019130597B4 (de) 2019-11-13 2024-07-18 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zum Erweitern der Flugenveloppe eines Verkehrsflugzeugs
CN112052525B (zh) * 2020-09-25 2023-03-17 中国直升机设计研究所 一种气动载荷分配方法
GB2616252A (en) * 2022-01-31 2023-09-06 Airbus Operations Ltd Aircraft with movable wing tip device
GB2615311A (en) * 2022-01-31 2023-08-09 Airbus Operations Ltd Aircraft wing with movable wing tip device
CN114906316A (zh) * 2022-04-15 2022-08-16 西华大学 超声速吹气环量后缘装置和飞行器
GB2628523B (en) * 2022-11-16 2025-07-09 Airbus Operations Ltd Aircraft wing
CN116238682A (zh) * 2023-03-31 2023-06-09 中国商用飞机有限责任公司 飞行器用翼梢小翼和配备有该翼梢小翼的飞行器
CN117446152A (zh) * 2023-12-22 2024-01-26 中国航空工业集团公司西安飞机设计研究所 一种开裂式舵面结构及飞行器

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Also Published As

Publication number Publication date
EP1558493A2 (de) 2005-08-03
WO2004041640A8 (en) 2004-07-22
AU2003299548A1 (en) 2004-06-07
WO2004041640A2 (en) 2004-05-21
US7048228B2 (en) 2006-05-23
EP1558493B1 (de) 2011-01-26
WO2004041640A3 (en) 2004-06-10
US20040195464A1 (en) 2004-10-07
DE60335895D1 (de) 2011-03-10
AU2003299548A8 (en) 2004-06-07
JP2006502914A (ja) 2006-01-26

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Legal Events

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