WO2011039399A3 - Cuaderna de aeronave y método de obtención de la misma. - Google Patents

Cuaderna de aeronave y método de obtención de la misma. Download PDF

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Publication number
WO2011039399A3
WO2011039399A3 PCT/ES2010/070628 ES2010070628W WO2011039399A3 WO 2011039399 A3 WO2011039399 A3 WO 2011039399A3 ES 2010070628 W ES2010070628 W ES 2010070628W WO 2011039399 A3 WO2011039399 A3 WO 2011039399A3
Authority
WO
WIPO (PCT)
Prior art keywords
obtaining
sections
skin
aircraft
ring frame
Prior art date
Application number
PCT/ES2010/070628
Other languages
English (en)
French (fr)
Other versions
WO2011039399A2 (es
Inventor
Enrique Vera Villares
José María PINA LÓPEZ
Original Assignee
Airbus Operations, S.L.
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
Priority to ESP200930757 priority Critical
Priority to ES200930757A priority patent/ES2383424B1/es
Application filed by Airbus Operations, S.L. filed Critical Airbus Operations, S.L.
Publication of WO2011039399A2 publication Critical patent/WO2011039399A2/es
Publication of WO2011039399A3 publication Critical patent/WO2011039399A3/es

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10Bulkheads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49764Method of mechanical manufacture with testing or indicating
    • Y10T29/49778Method of mechanical manufacture with testing or indicating with aligning, guiding, or instruction
    • Y10T29/4978Assisting assembly or disassembly

Abstract

Cuaderna de aeronave y método de obtención de la misma, estando realizada dicha cuaderna en material compuesto, comprendiendo dicha cuaderna varias particiones (20) que conforman, al unirse, la citada cuaderna en su totalidad, comprendiendo dichas particiones (20) secciones (1) de longitud (2), estando dispuestas dichas secciones (1) sobre la parte interior del revestimiento (3) que conforma el fuselaje de la aeronave, estando dicho fuselaje realizado de forma integral en una sola pieza, siendo la longitud (2) de las secciones (1) es la máxima posible, de tal modo que la separación (5) máxima entre la sección (1) de cuaderna y el revestimiento (3), estando medida esta separación (5) por la parte interior del citado revestimiento (3), sea inferior al valor límite permitido para el uso de un sellante en estado líquido.
PCT/ES2010/070628 2009-09-29 2010-09-28 Cuaderna de aeronave y método de obtención de la misma. WO2011039399A2 (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ESP200930757 2009-09-29
ES200930757A ES2383424B1 (es) 2009-09-29 2009-09-29 Cuaderna de aeronave y metodo de obtencion de la misma

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CA2776034A CA2776034A1 (en) 2009-09-29 2010-09-28 Aircraft ring frame and method for obtaining it
RU2012117773/11A RU2545218C2 (ru) 2009-09-29 2010-09-28 Шпангоут летательного аппарата и способ его изготовления
EP10770536A EP2484584A2 (en) 2009-09-29 2010-09-28 Aircraft frame and method for obtaining it
CN201080053958.7A CN102666273B (zh) 2009-09-29 2010-09-28 飞机机架和用于获得飞机机架的方法

Publications (2)

Publication Number Publication Date
WO2011039399A2 WO2011039399A2 (es) 2011-04-07
WO2011039399A3 true WO2011039399A3 (es) 2011-10-27

Family

ID=43826711

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2010/070628 WO2011039399A2 (es) 2009-09-29 2010-09-28 Cuaderna de aeronave y método de obtención de la misma.

Country Status (7)

Country Link
US (2) US20110168840A1 (es)
EP (1) EP2484584A2 (es)
CN (1) CN102666273B (es)
CA (1) CA2776034A1 (es)
ES (1) ES2383424B1 (es)
RU (1) RU2545218C2 (es)
WO (1) WO2011039399A2 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012202504A1 (de) * 2012-02-17 2013-08-22 Airbus Operations Gmbh Strukturbauteil für ein Luft- oder Raumfahrzeug
EP2759467B1 (en) * 2013-01-24 2016-10-19 Airbus Operations GmbH Aircraft frame and method of mounting two fuselage segments
US10626992B2 (en) * 2015-11-30 2020-04-21 The Boeing Company Sealant containment assembly, system, and method
RU181682U1 (ru) * 2017-12-11 2018-07-26 Владимир Васильевич Галайко FUSELAGE OF AIRCRAFT
RU2694486C1 (ru) * 2018-10-05 2019-07-15 Акционерное общество "Научно-производственное объединение им. С.А. Лавочкина" Шпангоут
CN109849351A (zh) * 2018-11-29 2019-06-07 中国商用飞机有限责任公司北京民用飞机技术研究中心 基于共胶接工艺的复合材料机翼壁板与金属翼肋密封方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060048890A1 (en) * 2004-09-06 2006-03-09 Honda Motor Co., Ltd. Production method of annular, fiber-reinforced composite structure, and annular frame constituted by such structure for aircraft fuselages
GB2428417A (en) * 2005-10-27 2007-01-31 Hal Errikos Calamvokis Aircraft fuselage structure

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1761898A2 (ru) * 1991-03-04 1992-09-15 Центральный научно-исследовательский институт специального машиностроения Опорный шпангоут из композиционного материала
CA2515149C (en) * 2003-02-24 2011-01-11 Bell Helicopter Textron Inc. Contact stiffeners for structural skins
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7621482B2 (en) * 2005-11-15 2009-11-24 The Boeing Company Weight optimized pressurizable aircraft fuselage structures having near elliptical cross sections
US8038099B2 (en) * 2008-04-30 2011-10-18 The Boeing Company Bonded metal fuselage and method for making the same

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060048890A1 (en) * 2004-09-06 2006-03-09 Honda Motor Co., Ltd. Production method of annular, fiber-reinforced composite structure, and annular frame constituted by such structure for aircraft fuselages
GB2428417A (en) * 2005-10-27 2007-01-31 Hal Errikos Calamvokis Aircraft fuselage structure

Also Published As

Publication number Publication date
RU2545218C2 (ru) 2015-03-27
CA2776034A1 (en) 2011-04-07
ES2383424B1 (es) 2013-05-03
RU2012117773A (ru) 2013-11-10
EP2484584A2 (en) 2012-08-08
WO2011039399A2 (es) 2011-04-07
ES2383424A1 (es) 2012-06-21
CN102666273B (zh) 2015-08-05
CN102666273A (zh) 2012-09-12
US20110168840A1 (en) 2011-07-14
US20130264422A1 (en) 2013-10-10

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