DE602006009252D1 - Systeme zur nutzlastverkleidung bei luftfahrzeugen und entsprechende verfahren - Google Patents

Systeme zur nutzlastverkleidung bei luftfahrzeugen und entsprechende verfahren

Info

Publication number
DE602006009252D1
DE602006009252D1 DE602006009252T DE602006009252T DE602006009252D1 DE 602006009252 D1 DE602006009252 D1 DE 602006009252D1 DE 602006009252 T DE602006009252 T DE 602006009252T DE 602006009252 T DE602006009252 T DE 602006009252T DE 602006009252 D1 DE602006009252 D1 DE 602006009252D1
Authority
DE
Germany
Prior art keywords
fairing
section
airfoil
application systems
corresponding methods
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
DE602006009252T
Other languages
English (en)
Inventor
Nicolaas Voogt
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=36816648&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE602006009252(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 DE602006009252D1 publication Critical patent/DE602006009252D1/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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • 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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE602006009252T 2005-05-20 2006-04-26 Systeme zur nutzlastverkleidung bei luftfahrzeugen und entsprechende verfahren Active DE602006009252D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/134,019 US7300021B2 (en) 2005-05-20 2005-05-20 Aerospace vehicle fairing systems and associated methods
PCT/US2006/016002 WO2006127204A1 (en) 2005-05-20 2006-04-26 Aerospace vehicle fairing systems and associated methods

Publications (1)

Publication Number Publication Date
DE602006009252D1 true DE602006009252D1 (de) 2009-10-29

Family

ID=36816648

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006009252T Active DE602006009252D1 (de) 2005-05-20 2006-04-26 Systeme zur nutzlastverkleidung bei luftfahrzeugen und entsprechende verfahren

Country Status (8)

Country Link
US (1) US7300021B2 (de)
EP (1) EP1883576B2 (de)
JP (1) JP5414269B2 (de)
CN (1) CN101180209B (de)
AT (1) ATE442986T1 (de)
CA (1) CA2602901C (de)
DE (1) DE602006009252D1 (de)
WO (1) WO2006127204A1 (de)

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US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems 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
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
DE102006015727A1 (de) * 2006-02-25 2007-09-06 Airbus Deutschland Gmbh Verkleidungskörper der Klappenkinematik am Flügel eines Flugzeuges
US7874524B2 (en) * 2007-11-16 2011-01-25 The Boeing Company Methods and apparatus for a multi-segment flap fence
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
GB0803722D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Shock bump
GB0803719D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Aerodynamic structure with asymmetrical shock bump
GB0803730D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Shock bump array
GB0803724D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Aerodynamic structure with non-uniformly spaced shock bumps
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
DE102009060325A1 (de) * 2009-12-23 2011-06-30 Airbus Operations GmbH, 21129 Hochauftriebssystem für ein Flugzeug
DE102010010577A1 (de) 2010-03-08 2011-09-08 Airbus Operations Gmbh Hochauftriebssystem für ein Flugzeug
ES2399262B1 (es) * 2010-12-31 2014-04-29 Airbus Operations, S.L. Herraje regulable para la instalación y ajuste de carenas en aeronaves.
US9623957B2 (en) * 2014-08-26 2017-04-18 The Boeing Company Torque tube door
US11305869B1 (en) 2020-12-23 2022-04-19 Wayfarer Aircraft Research And Development Inc. Systems and methods for aircraft lift enhancement

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US20060261217A1 (en) 2006-11-23
JP2008540255A (ja) 2008-11-20
EP1883576B2 (de) 2018-10-17
CN101180209A (zh) 2008-05-14
CN101180209B (zh) 2012-12-12
EP1883576A1 (de) 2008-02-06
EP1883576B1 (de) 2009-09-16
WO2006127204A1 (en) 2006-11-30
JP5414269B2 (ja) 2014-02-12
ATE442986T1 (de) 2009-10-15
CA2602901A1 (en) 2006-11-30
US7300021B2 (en) 2007-11-27

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