DE217315T1 - Beplankungsfeld fuer einen fluegelkasten und fertigungsverfahren. - Google Patents

Beplankungsfeld fuer einen fluegelkasten und fertigungsverfahren.

Info

Publication number
DE217315T1
DE217315T1 DE198686113295T DE86113295T DE217315T1 DE 217315 T1 DE217315 T1 DE 217315T1 DE 198686113295 T DE198686113295 T DE 198686113295T DE 86113295 T DE86113295 T DE 86113295T DE 217315 T1 DE217315 T1 DE 217315T1
Authority
DE
Germany
Prior art keywords
manufacturing process
wing box
planking field
planking
field
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.)
Pending
Application number
DE198686113295T
Other languages
English (en)
Inventor
Robert R. Kirkland Washington Us Hammer
Raymond E. Redmond Washington De Pearson
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
Application filed by Boeing Co filed Critical Boeing Co
Publication of DE217315T1 publication Critical patent/DE217315T1/de
Pending legal-status Critical Current

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Vehicle Step Arrangements And Article Storage (AREA)
DE198686113295T 1985-09-30 1986-09-26 Beplankungsfeld fuer einen fluegelkasten und fertigungsverfahren. Pending DE217315T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/781,776 US4749155A (en) 1985-09-30 1985-09-30 Method of making wing box cover panel

Publications (1)

Publication Number Publication Date
DE217315T1 true DE217315T1 (de) 1988-01-14

Family

ID=25123893

Family Applications (1)

Application Number Title Priority Date Filing Date
DE198686113295T Pending DE217315T1 (de) 1985-09-30 1986-09-26 Beplankungsfeld fuer einen fluegelkasten und fertigungsverfahren.

Country Status (4)

Country Link
US (1) US4749155A (de)
EP (1) EP0217315A3 (de)
JP (1) JPS62168789A (de)
DE (1) DE217315T1 (de)

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CA2253037C (en) * 1997-11-12 2004-11-02 Sakura Rubber Co., Ltd. Method of manufacturing structure by using biodegradable mold
US6513757B1 (en) 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
GB0021955D0 (en) * 2000-09-07 2000-10-25 Bae Systems Plc Stiffening means for structural components
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
JP4574086B2 (ja) * 2001-09-03 2010-11-04 富士重工業株式会社 複合材翼の製造方法および複合材翼
GB0207239D0 (en) * 2002-03-27 2002-05-08 Airbus Uk Ltd Wing skin and method of manufacture thereof
US20040035979A1 (en) * 2002-08-23 2004-02-26 Mccoskey William Robert Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same
US7093470B2 (en) * 2002-09-24 2006-08-22 The Boeing Company Methods of making integrally stiffened axial load carrying skin panels for primary aircraft structure and fuel tank structures
US7182293B2 (en) * 2004-04-27 2007-02-27 The Boeing Company Airfoil box and associated method
CA2529108C (en) * 2004-12-07 2012-10-30 Airbus Deutschland Gmbh Airplane wing, method for manufacturing an airplane wing and use of a welding process for welding a wing spar
US7387277B2 (en) * 2004-12-29 2008-06-17 The Boeing Company Aircraft wing composed of composite and metal panels
FR2888816B1 (fr) * 2005-07-20 2007-08-31 Airbus France Sas Panneau auto-raidi monolithique
WO2007091990A2 (en) † 2006-01-11 2007-08-16 The Boeing Company Aircraft wing composed of composite and metal panels
DE102006026167B3 (de) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Leichtbau-Strukturpanel
WO2008132251A1 (es) * 2007-04-30 2008-11-06 Airbus España, S.L. Cajón de torsión multilarguero integrado de material compuesto
GB0803689D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Trailing edge aircraft structure with overhaning cover
WO2011043346A1 (ja) 2009-10-08 2011-04-14 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
GB201008186D0 (en) * 2010-05-17 2010-06-30 Airbus Operations Ltd A structural assembly for an aircraft
GB201020189D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd An aircraft structure
JP5808111B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体
JP5808112B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 複合材構造体およびこれを備えた航空機主翼
ES2401830B1 (es) * 2011-06-29 2014-04-10 Airbus Operations S.L. Paneles de relleno para los revestimientos de los tanques de combustible de las aeronaves.
CN102514709B (zh) * 2011-12-06 2014-04-09 南京航空航天大学 一种采用格栅结构的飞行器机翼盒段及设计方法
ES2606245T3 (es) * 2012-07-17 2017-03-23 Airbus Operations, S.L. Borde de ataque altamente integrado de una superficie sustentadora de una aeronave
US9481444B2 (en) * 2012-09-12 2016-11-01 The Boeing Company Passive load alleviation for aerodynamic lift structures
FR3000470B1 (fr) * 2012-12-28 2015-12-25 Airbus Operations Sas Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe
JP6093192B2 (ja) * 2013-01-25 2017-03-08 三菱航空機株式会社 航空機の機体用パネル、航空機の翼
GB201301766D0 (en) * 2013-01-31 2013-03-20 Airbus Operations Ltd Structural assembly joint
RU2532254C2 (ru) * 2013-02-07 2014-11-10 Общество с ограниченной ответственностью "Научно-технологический испытательный центр АпАТэК-Дубна" Кессон крыла из композиционного материала
RU2532255C1 (ru) * 2013-06-05 2014-11-10 Общество с ограниченной ответственностью "Научно-технологический испытательный центр АпАТэК-Дубна" Кессон крыла из композиционного материала
ES2674659T3 (es) 2013-09-23 2018-07-03 Airbus Operations S.L. Método para fabricar una caja de torsión aeronáutica, caja de torsión y herramienta para fabricar una caja de torsión aeronáutica
FR3015426B1 (fr) * 2013-12-20 2017-10-27 Airbus Operations Sas Procede de realisation d'un caisson central de voilure
US9657489B2 (en) * 2015-06-15 2017-05-23 The Boeing Company Fractal stiffening
RU2613661C1 (ru) * 2016-01-11 2017-03-21 Федеральное государственное бюджетное образовательное учреждение высшего образования Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" (КНИТУ-КАИ) Способ сборки крыла из полимерного композиционного материала
US10479474B2 (en) * 2016-07-14 2019-11-19 The Boeing Company Friction stir welded wingtip torque box
US10421528B2 (en) * 2016-08-16 2019-09-24 The Boeing Company Planked stringers that provide structural support for an aircraft wing
CN110582444B (zh) * 2017-05-01 2023-03-07 庞巴迪公司 具有限定压力地板的上机翼蒙皮的飞机机翼单元
IT201700122745A1 (it) * 2017-10-27 2019-04-27 Salver S P A Procedimento di assemblaggio di parti di un’ala aeronautica
RU2690300C1 (ru) * 2017-11-09 2019-05-31 Акционерное общество Научно-производственное объединение "Опытно-конструкторское бюро имени М.П. Симонова" Кессон отъемной части крыла
US11161592B2 (en) * 2019-09-11 2021-11-02 Textron Innovations Inc. Torque box sleeves for aircraft wing assemblies
CN111452953B (zh) * 2020-04-01 2023-04-07 中国商用飞机有限责任公司 一种适用于构造飞机翼面的盒式结构
GB2623830A (en) * 2022-10-31 2024-05-01 Airbus Operations Ltd Aircraft wing structure

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US3519228A (en) * 1967-09-29 1970-07-07 Dow Chemical Co Airfoil structure
GB1250885A (de) * 1967-12-05 1971-10-20
GB1317779A (en) * 1970-08-04 1973-05-23 Gill M C Laminated fibre glass flooring and method of making the same
US3768760A (en) * 1970-10-30 1973-10-30 Hercules Inc Graphite fiber composite covering employing multi-directional
DE2109692C3 (de) * 1971-03-02 1981-06-04 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Flügelkasten für Luftfahrzeuge in Verbundbauweise
US3861674A (en) * 1973-07-09 1975-01-21 Norman Buck Manufacturing Co I Composite diving board
US3902944A (en) * 1974-02-14 1975-09-02 Fiber Science Inc Noncircular filament wound article of manufacture and method of making same
US3962506A (en) * 1974-04-29 1976-06-08 Fiber Science, Inc. Multi-chambered cellular structure and method for manufacture
US3995081A (en) * 1974-10-07 1976-11-30 General Dynamics Corporation Composite structural beams and method
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GB2072579B (en) * 1980-04-01 1984-06-06 British Aerospace Stiffened panel of fibre reinforced plastics materials
US4461669A (en) * 1983-09-30 1984-07-24 The Boeing Company Pivotal mount for laminating head
US4475976A (en) * 1983-12-23 1984-10-09 The Boeing Company Method and apparatus for forming composite material articles

Also Published As

Publication number Publication date
JPS62168789A (ja) 1987-07-25
EP0217315A2 (de) 1987-04-08
US4749155A (en) 1988-06-07
EP0217315A3 (de) 1988-01-07

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