CN101242992B - 用于机翼的支撑结构 - Google Patents

用于机翼的支撑结构 Download PDF

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Publication number
CN101242992B
CN101242992B CN200680029781.0A CN200680029781A CN101242992B CN 101242992 B CN101242992 B CN 101242992B CN 200680029781 A CN200680029781 A CN 200680029781A CN 101242992 B CN101242992 B CN 101242992B
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CN
China
Prior art keywords
transom
shape
cross
transition region
bar member
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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 - Fee Related
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CN200680029781.0A
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English (en)
Chinese (zh)
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CN101242992A (zh
Inventor
克里斯蒂安·门茨
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 Operations GmbH
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Airbus Operations GmbH
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Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of CN101242992A publication Critical patent/CN101242992A/zh
Application granted granted Critical
Publication of CN101242992B publication Critical patent/CN101242992B/zh
Expired - Fee Related legal-status Critical Current
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/06—Fins
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18—Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19—Three-dimensional [3D] framework structures
    • E04B2001/1924—Struts specially adapted therefor
    • E04B2001/1927—Struts specially adapted therefor of essentially circular cross section
    • E04B2001/193—Struts specially adapted therefor of essentially circular cross section with flattened connecting parts, e.g. ends

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Connection Of Plates (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Toys (AREA)
CN200680029781.0A 2005-08-17 2006-08-16 用于机翼的支撑结构 Expired - Fee Related CN101242992B (zh)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US70914605P 2005-08-17 2005-08-17
DE102005038849A DE102005038849A1 (de) 2005-08-17 2005-08-17 Stützstruktur für einen Flügel
DE102005038849.3 2005-08-17
US60/709,146 2005-08-17
PCT/EP2006/008077 WO2007020069A1 (en) 2005-08-17 2006-08-16 Support structure for a wing

Publications (2)

Publication Number Publication Date
CN101242992A CN101242992A (zh) 2008-08-13
CN101242992B true CN101242992B (zh) 2012-10-10

Family

ID=37697271

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200680029781.0A Expired - Fee Related CN101242992B (zh) 2005-08-17 2006-08-16 用于机翼的支撑结构

Country Status (9)

Country Link
US (1) US8205834B2 (https=)
EP (1) EP1915291B1 (https=)
JP (1) JP5055280B2 (https=)
CN (1) CN101242992B (https=)
BR (1) BRPI0614427A2 (https=)
CA (1) CA2616929A1 (https=)
DE (1) DE102005038849A1 (https=)
RU (1) RU2408497C2 (https=)
WO (1) WO2007020069A1 (https=)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2416009A (en) * 2004-05-12 2006-01-11 Dunlop Aerospace Ltd Hydraulic fluid control apparatus
DE102005038851A1 (de) * 2005-08-17 2007-03-01 Airbus Deutschland Gmbh Fachwerk-Mittelkasten für einen Flügel
GB0712553D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Composite panel stiffener
DE102010051216A1 (de) * 2010-11-12 2012-05-16 Airbus Operations Gmbh Seitenrudersystem an einem Flugzeug
FR2968271B1 (fr) 2010-12-01 2013-01-18 Airbus Operations Sas Panneau triangulaire dispose a l'arriere d'un caisson central du fuselage d'un aeronef
FR2973086B1 (fr) * 2011-03-24 2014-01-10 Airbus Operations Sas Bielle structurale, de preference pour aeronef
US9156559B2 (en) * 2011-10-19 2015-10-13 The Boeing Company Segmented aircraft wing having solar arrays
GB201204231D0 (en) * 2012-03-09 2012-04-25 Airbus Uk Ltd Space frame structure
EP3301015B1 (en) * 2012-06-21 2019-05-22 Bombardier Inc. Morphing wing for an aircraft
US9587414B2 (en) * 2012-09-25 2017-03-07 James A Lachenberg Fully welded fence panel and method of making same
GB2524828A (en) * 2014-04-04 2015-10-07 Airbus Operations Ltd An aircraft comprising a foldable aerodynamic structure and a method of manufacturing a foldable aerodynamic structure for an aircraft
ES2729104T3 (es) 2014-09-29 2019-10-30 Boeing Co Largueros de relanzamiento para aplicaciones de timón y elevador
US10850826B2 (en) * 2017-03-24 2020-12-01 The Boeing Company Aircraft wing space frame
GB2568738A (en) * 2017-11-27 2019-05-29 Airbus Operations Ltd An improved interface between an outer end of a wing and a moveable wing tip device
GB2572150A (en) * 2018-03-19 2019-09-25 Airbus Operations Ltd A moveable wing tip device an outer end of a wing, and interface therebetween
GB2574391A (en) * 2018-05-31 2019-12-11 Airbus Operations Ltd An aircraft wing and wing tip device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB151085A (en) * 1919-06-14 1920-09-14 Frederick Michael Green Improvements in fittings for the metal framework of aeroplanes and the like
FR673934A (fr) * 1928-04-25 1930-01-21 Emboutissage Et De Const Mecan Perfectionnements apportés aux armatures pour surfaces portantes d'aéronefs, notamment à celles pour ailes d'aéroplanes
CN2284731Y (zh) * 1996-05-08 1998-06-24 马金山 一种飞机机翼的翼梢结构

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE612794C (de) * 1936-03-23 Hans Weirich Knotenpunktsverbindung fuer Flugzeugtragflaechen
US155409A (en) * 1874-09-29 Improvement in boat-detaching apparatus
AT78501B (de) * 1917-09-17 1919-09-25 Luftschiffbau Schuette Lanz Aus Einzelprofilen zusammengesetzter Träger für Starrluftschiffe.
US1555409A (en) 1920-12-27 1925-09-29 Curtiss Aeroplane & Motor Co Airplane wing
US1545129A (en) * 1923-09-27 1925-07-07 Jr John F Cook Aircraft structure
DE473098C (de) * 1927-03-18 1929-03-18 Franz Kruckenberg Dipl Ing Die Nutzlast aufnehmender Fahrzeugkoerper
US1773357A (en) * 1929-02-19 1930-08-19 Roger W Griswold Fabricated tubular structure and method of forming the same
US1914344A (en) * 1930-02-14 1933-06-13 Budd Edward G Mfg Co Sheet metal joint construction
DE586542C (de) * 1930-04-05 1933-10-23 Rudolf Ulbricht Geschweisste Knotenblechverbindung fuer Stahlrohrkonstruktionen
US2001215A (en) * 1932-12-10 1935-05-14 Frederick H Ruppel Structure
DE630297C (de) * 1934-06-16 1936-05-25 Arthur Levell Einholmige Flugzeugtragflaeche
US2098752A (en) * 1935-02-06 1937-11-09 Fleetwings Inc Structural section for aircraft
GB462390A (en) 1935-08-29 1937-03-01 James Jacob Mayrow Improved construction of wings, aerofoils and the like for aeronautical machines
CH195404A (de) 1937-04-14 1938-01-31 Aluminium Ind Ag Verfahren zur Herstellung eines gerippeartigen Baukörpers, insbesondere für Fahrzeuge.
US4334816A (en) * 1978-08-03 1982-06-15 General Dynamics Corporation Device and method for assembling large space structures
US4332501A (en) * 1978-08-03 1982-06-01 General Dynamics Corporation Structural node for large space structures
GB2128706B (en) 1982-04-27 1986-01-29 Jr Comm Enterprises Ltd Tubular structures
SU1186845A1 (ru) 1982-12-21 1985-10-23 Центральное конструкторское бюро нефтеаппаратуры Устройство дл соединени схватывающей и охватываемой деталей
DE3721092C2 (de) * 1986-08-20 1998-02-19 Ulrich Kreusel Rohrverbindungssystem
DE19613090B4 (de) * 1995-04-05 2005-09-29 Luftschiffbau Zeppelin Gmbh Träger für ein Luftschiff
DE19920427B4 (de) * 1999-05-04 2006-10-12 Düser, Ulrich Vorrichtung zum Verbinden von Rohren in unterschiedlichen Winkelstellungen
DE19921690B4 (de) * 1999-05-12 2005-02-17 Alfred Bullermann Hohlprofilverbindung
DE202004015047U1 (de) * 2004-09-27 2005-01-13 Reithmeier, Josef Rundrohrbefestiger
DE202004015883U1 (de) * 2004-10-14 2005-01-20 Seele Gmbh & Co. Kg Knotenverbindung mit Gußteilen

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB151085A (en) * 1919-06-14 1920-09-14 Frederick Michael Green Improvements in fittings for the metal framework of aeroplanes and the like
FR673934A (fr) * 1928-04-25 1930-01-21 Emboutissage Et De Const Mecan Perfectionnements apportés aux armatures pour surfaces portantes d'aéronefs, notamment à celles pour ailes d'aéroplanes
CN2284731Y (zh) * 1996-05-08 1998-06-24 马金山 一种飞机机翼的翼梢结构

Also Published As

Publication number Publication date
US20100170995A1 (en) 2010-07-08
WO2007020069A1 (en) 2007-02-22
EP1915291A1 (en) 2008-04-30
US8205834B2 (en) 2012-06-26
JP5055280B2 (ja) 2012-10-24
EP1915291B1 (en) 2011-11-16
CA2616929A1 (en) 2007-02-22
CN101242992A (zh) 2008-08-13
BRPI0614427A2 (pt) 2011-03-29
RU2008109925A (ru) 2009-09-27
JP2009504494A (ja) 2009-02-05
DE102005038849A1 (de) 2007-02-22
RU2408497C2 (ru) 2011-01-10

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C53 Correction of patent of invention or patent application
CB02 Change of applicant information

Address after: hamburg

Applicant after: Airbus Operations GmbH

Address before: hamburg

Applicant before: Airbus GmbH

COR Change of bibliographic data

Free format text: CORRECT: APPLICANT; FROM: AIRBUS GMBH TO: AIRBUS DEUTSCHLAND GMBH

C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20121010

Termination date: 20170816