RU2564561C2 - Стыковая накладка и связанный с ней способ соединения отсеков фюзеляжа - Google Patents

Стыковая накладка и связанный с ней способ соединения отсеков фюзеляжа Download PDF

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Publication number
RU2564561C2
RU2564561C2 RU2013132316/11A RU2013132316A RU2564561C2 RU 2564561 C2 RU2564561 C2 RU 2564561C2 RU 2013132316/11 A RU2013132316/11 A RU 2013132316/11A RU 2013132316 A RU2013132316 A RU 2013132316A RU 2564561 C2 RU2564561 C2 RU 2564561C2
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RU
Russia
Prior art keywords
strip
fuselage
shear element
shear
compartments
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RU2013132316/11A
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English (en)
Russian (ru)
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RU2013132316A (ru
Inventor
Ричард Р. РОСМЭН
Ларри ТОЛЕР
Дэвид ЛЕЙБОВ
Original Assignee
Дзе Боинг Компани
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Application filed by Дзе Боинг Компани filed Critical Дзе Боинг Компани
Publication of RU2013132316A publication Critical patent/RU2013132316A/ru
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Publication of RU2564561C2 publication Critical patent/RU2564561C2/ru

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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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Clamps And Clips (AREA)
  • Bridges Or Land Bridges (AREA)
  • Connection Of Plates (AREA)
  • Vehicle Step Arrangements And Article Storage (AREA)
  • Moulding By Coating Moulds (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
RU2013132316/11A 2010-12-15 2011-11-04 Стыковая накладка и связанный с ней способ соединения отсеков фюзеляжа RU2564561C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/968,732 2010-12-15
US12/968,732 US8567722B2 (en) 2010-12-15 2010-12-15 Splice and associated method for joining fuselage sections
PCT/US2011/059422 WO2012082254A1 (en) 2010-12-15 2011-11-04 Splice and associated method for joining fuselage sections

Publications (2)

Publication Number Publication Date
RU2013132316A RU2013132316A (ru) 2015-01-20
RU2564561C2 true RU2564561C2 (ru) 2015-10-10

Family

ID=45044711

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013132316/11A RU2564561C2 (ru) 2010-12-15 2011-11-04 Стыковая накладка и связанный с ней способ соединения отсеков фюзеляжа

Country Status (10)

Country Link
US (1) US8567722B2 (enExample)
EP (1) EP2651757B1 (enExample)
JP (1) JP6000276B2 (enExample)
KR (1) KR101872043B1 (enExample)
CN (2) CN105644767B (enExample)
AU (1) AU2011341598B2 (enExample)
CA (1) CA2817735C (enExample)
ES (1) ES2544051T3 (enExample)
RU (1) RU2564561C2 (enExample)
WO (1) WO2012082254A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2655585C2 (ru) * 2016-11-22 2018-05-28 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Узел стыка отсеков фюзеляжа с сетчатой и традиционной конструктивно-силовыми схемами

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
FR2976916B1 (fr) * 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
US8740151B1 (en) * 2012-01-03 2014-06-03 The Boeing Company Adjustable splice fitting for shimless connection of structual members
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US8960606B2 (en) * 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
EP2781450B1 (en) * 2013-03-19 2018-05-02 Airbus Operations GmbH System and method for interconnecting composite structures
EP3083395B1 (en) * 2013-12-20 2021-09-08 Saab Ab Stiffening element and reinforced structure
US9527572B2 (en) 2014-06-26 2016-12-27 The Boeing Company Elongated structures and related assemblies
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
US9682429B2 (en) 2015-04-22 2017-06-20 The Boeing Company Reaction tool and method for forming openings in an aircraft fuselage joint
US10392132B2 (en) * 2016-07-29 2019-08-27 The Boeing Company Curved aircraft substructure repair systems and methods
US10308342B2 (en) * 2016-09-07 2019-06-04 The Boeing Company Method of repairing damage to fuselage barrel and associated apparatus and system
US11524761B2 (en) * 2016-12-09 2022-12-13 The Boeing Company Stringer-frame intersection of aircraft body
US20200122816A1 (en) * 2018-10-22 2020-04-23 The Boeing Company Bulkhead joint assembly
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
GB2615755A (en) * 2022-02-15 2023-08-23 Airbus Operations Ltd Fuel tank stringer with flow passage
EP4420974A1 (de) * 2023-02-27 2024-08-28 Airbus Operations GmbH Verfahren zur herstellung eines rumpfstrukturbauteils für einen dreiecksbereich und einstückiges rumpfstrukturbauteil

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1376424A1 (ru) * 1985-11-19 1995-10-27 Г.Г. Демьяненко Стык фюзеляжа с центропланом летательного аппарата
FR2922516A1 (fr) * 2007-10-18 2009-04-24 Airbus France Sas Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
US5893534A (en) * 1995-12-22 1999-04-13 The Boeing Company Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
FR2906008B1 (fr) * 2006-09-15 2008-11-07 Airbus France Sa Eclisse de lisses et dispositif de jonction orbitale
US7787979B2 (en) * 2007-03-14 2010-08-31 The Boeing Company Splicing fuselage sections without shims
DE102007018753B4 (de) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten
JP2008285115A (ja) * 2007-05-21 2008-11-27 Mitsubishi Heavy Ind Ltd 航空機組立品およびその製造方法
FR2922518B1 (fr) * 2007-10-18 2010-04-23 Airbus France Structure d'avion comportant des jonctions d'arrets de raidisseurs
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund
FR2931720B1 (fr) 2008-06-02 2010-12-17 Airbus France Procede d'assemblage orbital de troncons d'aeronef en materiau composite

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1376424A1 (ru) * 1985-11-19 1995-10-27 Г.Г. Демьяненко Стык фюзеляжа с центропланом летательного аппарата
FR2922516A1 (fr) * 2007-10-18 2009-04-24 Airbus France Sas Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2655585C2 (ru) * 2016-11-22 2018-05-28 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Узел стыка отсеков фюзеляжа с сетчатой и традиционной конструктивно-силовыми схемами

Also Published As

Publication number Publication date
EP2651757A1 (en) 2013-10-23
WO2012082254A1 (en) 2012-06-21
AU2011341598A1 (en) 2013-05-23
ES2544051T3 (es) 2015-08-27
EP2651757B1 (en) 2015-07-22
US20120153082A1 (en) 2012-06-21
AU2011341598B2 (en) 2016-03-10
CA2817735A1 (en) 2012-06-21
US8567722B2 (en) 2013-10-29
CA2817735C (en) 2016-12-06
KR101872043B1 (ko) 2018-06-27
JP2014500185A (ja) 2014-01-09
KR20130138359A (ko) 2013-12-18
RU2013132316A (ru) 2015-01-20
CN103261020A (zh) 2013-08-21
JP6000276B2 (ja) 2016-09-28
CN103261020B (zh) 2016-01-20
CN105644767B (zh) 2018-06-12
CN105644767A (zh) 2016-06-08

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