RU2408497C2 - Опорная конструкция для крыла - Google Patents

Опорная конструкция для крыла Download PDF

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Publication number
RU2408497C2
RU2408497C2 RU2008109925/11A RU2008109925A RU2408497C2 RU 2408497 C2 RU2408497 C2 RU 2408497C2 RU 2008109925/11 A RU2008109925/11 A RU 2008109925/11A RU 2008109925 A RU2008109925 A RU 2008109925A RU 2408497 C2 RU2408497 C2 RU 2408497C2
Authority
RU
Russia
Prior art keywords
transition region
cross
rod
articulation
connecting element
Prior art date
Application number
RU2008109925/11A
Other languages
English (en)
Russian (ru)
Other versions
RU2008109925A (ru
Inventor
Кристиан МАНЦ (DE)
Кристиан МАНЦ
Original Assignee
Эйрбас Дойчланд Гмбх
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 Эйрбас Дойчланд Гмбх filed Critical Эйрбас Дойчланд Гмбх
Publication of RU2008109925A publication Critical patent/RU2008109925A/ru
Application granted granted Critical
Publication of RU2408497C2 publication Critical patent/RU2408497C2/ru

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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)
RU2008109925/11A 2005-08-17 2006-08-16 Опорная конструкция для крыла RU2408497C2 (ru)

Applications Claiming Priority (4)

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

Publications (2)

Publication Number Publication Date
RU2008109925A RU2008109925A (ru) 2009-09-27
RU2408497C2 true RU2408497C2 (ru) 2011-01-10

Family

ID=37697271

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2008109925/11A RU2408497C2 (ru) 2005-08-17 2006-08-16 Опорная конструкция для крыла

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)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2822808C1 (ru) * 2023-12-22 2024-07-15 Публичное акционерное общество "Объединенная авиастроительная корпорация" (ПАО "ОАК") Система раскладки крыла летательного аппарата

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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

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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
GB2128706A (en) * 1982-04-27 1984-05-02 Jr Comm Enterprises Ltd Tubular structures

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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
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

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
GB2128706A (en) * 1982-04-27 1984-05-02 Jr Comm Enterprises Ltd Tubular structures

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2822808C1 (ru) * 2023-12-22 2024-07-15 Публичное акционерное общество "Объединенная авиастроительная корпорация" (ПАО "ОАК") Система раскладки крыла летательного аппарата

Also Published As

Publication number Publication date
JP5055280B2 (ja) 2012-10-24
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
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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PD4A Correction of name of patent owner
MM4A The patent is invalid due to non-payment of fees

Effective date: 20170817