JP5055280B2 - 翼用の支持構造 - Google Patents

翼用の支持構造 Download PDF

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Publication number
JP5055280B2
JP5055280B2 JP2008526438A JP2008526438A JP5055280B2 JP 5055280 B2 JP5055280 B2 JP 5055280B2 JP 2008526438 A JP2008526438 A JP 2008526438A JP 2008526438 A JP2008526438 A JP 2008526438A JP 5055280 B2 JP5055280 B2 JP 5055280B2
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JP
Japan
Prior art keywords
support structure
transition region
bar
joining
cross
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.)
Expired - Fee Related
Application number
JP2008526438A
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English (en)
Japanese (ja)
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JP2009504494A5 (enExample
JP2009504494A (ja
Inventor
クリスティアン メンツ
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
Original Assignee
Airbus Operations GmbH
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Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of JP2009504494A publication Critical patent/JP2009504494A/ja
Publication of JP2009504494A5 publication Critical patent/JP2009504494A5/ja
Application granted granted Critical
Publication of JP5055280B2 publication Critical patent/JP5055280B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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 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)
JP2008526438A 2005-08-17 2006-08-16 翼用の支持構造 Expired - Fee Related JP5055280B2 (ja)

Applications Claiming Priority (5)

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

Publications (3)

Publication Number Publication Date
JP2009504494A JP2009504494A (ja) 2009-02-05
JP2009504494A5 JP2009504494A5 (enExample) 2009-09-17
JP5055280B2 true JP5055280B2 (ja) 2012-10-24

Family

ID=37697271

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008526438A Expired - Fee Related JP5055280B2 (ja) 2005-08-17 2006-08-16 翼用の支持構造

Country Status (9)

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

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
CA2876985A1 (en) * 2012-06-21 2013-12-27 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
CN107074342B (zh) 2014-09-29 2020-12-04 波音公司 用于方向舵和升降舵应用的转折的翼梁
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

Family Cites Families (27)

* 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.
GB151085A (en) * 1919-06-14 1920-09-14 Frederick Michael Green Improvements in fittings for the metal framework of aeroplanes and the like
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
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
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
CN2284731Y (zh) * 1996-05-08 1998-06-24 马金山 一种飞机机翼的翼梢结构
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

Also Published As

Publication number Publication date
EP1915291B1 (en) 2011-11-16
CN101242992A (zh) 2008-08-13
DE102005038849A1 (de) 2007-02-22
CA2616929A1 (en) 2007-02-22
RU2008109925A (ru) 2009-09-27
EP1915291A1 (en) 2008-04-30
BRPI0614427A2 (pt) 2011-03-29
RU2408497C2 (ru) 2011-01-10
JP2009504494A (ja) 2009-02-05
US8205834B2 (en) 2012-06-26
WO2007020069A1 (en) 2007-02-22
CN101242992B (zh) 2012-10-10
US20100170995A1 (en) 2010-07-08

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