ES2605567T3 - Junta de empalme unida - Google Patents

Junta de empalme unida Download PDF

Info

Publication number
ES2605567T3
ES2605567T3 ES12816554.5T ES12816554T ES2605567T3 ES 2605567 T3 ES2605567 T3 ES 2605567T3 ES 12816554 T ES12816554 T ES 12816554T ES 2605567 T3 ES2605567 T3 ES 2605567T3
Authority
ES
Spain
Prior art keywords
attachment
shaped
body side
extensions
joint assembly
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.)
Active
Application number
ES12816554.5T
Other languages
English (en)
Inventor
Paul NORDMAN
Paul Nelson
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
Application granted granted Critical
Publication of ES2605567T3 publication Critical patent/ES2605567T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/47—Molded joint
    • Y10T403/472—Molded joint including mechanical interlock
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/50—Bridged by diverse connector

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

Un conjunto de junta lateral de cuerpo de un avión, que comprende: un primer y segundo largueros (208) en forma de t, teniendo cada uno una porción vertical (209), caracterizado por que dicha porción vertical define un hueco longitudinal (408); y por que el conjunto de junta lateral de cuerpo comprende además un accesorio cruciforme (206) que tiene un elemento de fijación de nervio central (304) y una primera y segunda extensiones de accesorio (302) en forma de t que se extienden en direcciones opuestas desde dicho elemento de fijación de nervio central (304), teniendo cada extensión de accesorio una porción de accesorio horizontal (306) y una porción de fijación del larguero (308) que se extiende hacia arriba desde dicha porción de accesorio horizontal; en el que dichas porciones de fijación del larguero (308) de dichas primera y segunda extensiones de accesorio (302) en forma de t se insertan en dicho hueco longitudinal (408) de dichos primer y segundo largueros (208) en forma de t, respectivamente.

Description

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Claims (1)

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    imagen2
ES12816554.5T 2012-03-07 2012-12-13 Junta de empalme unida Active ES2605567T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201213414066 2012-03-07
US13/414,066 US8684311B2 (en) 2012-03-07 2012-03-07 Bonded splice joint
PCT/US2012/069591 WO2013133880A1 (en) 2012-03-07 2012-12-13 Bonded splice joint

Publications (1)

Publication Number Publication Date
ES2605567T3 true ES2605567T3 (es) 2017-03-15

Family

ID=47594986

Family Applications (1)

Application Number Title Priority Date Filing Date
ES12816554.5T Active ES2605567T3 (es) 2012-03-07 2012-12-13 Junta de empalme unida

Country Status (6)

Country Link
US (2) US8684311B2 (es)
EP (1) EP2822852B1 (es)
JP (2) JP6138837B2 (es)
CN (1) CN104144852B (es)
ES (1) ES2605567T3 (es)
WO (1) WO2013133880A1 (es)

Families Citing this family (25)

* 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
CA2768957C (en) * 2009-10-08 2014-07-29 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
ES2397727B1 (es) * 2010-10-28 2014-01-17 Airbus Operations, S.L. Retenedores reutilizables para coencolado de larguerillos no curados.
US9926067B1 (en) * 2013-06-10 2018-03-27 The Boeing Company Stringer flange extending to composite skin edge
US9580164B2 (en) * 2013-07-10 2017-02-28 The Boeing Company Apparatus and methods for joining aircraft composite structures
US9315254B2 (en) * 2013-10-11 2016-04-19 The Boeing Company Joint assembly and method of assembling same
US10538322B2 (en) * 2014-12-19 2020-01-21 Sikorsky Aircraft Corporation Delta fuselage for vertical take-off and landing (VTOL) aircraft
CN105366025A (zh) * 2015-11-17 2016-03-02 江西洪都航空工业集团有限责任公司 三梁式单翼飞机机翼与机身连接接头
US9808988B2 (en) * 2015-11-30 2017-11-07 The Boeing Company Carbon fiber reinforced plastic (CFRP) stringer termination softening with stacked CFRP noodle
US10450870B2 (en) 2016-02-09 2019-10-22 General Electric Company Frangible gas turbine engine airfoil
US10421528B2 (en) * 2016-08-16 2019-09-24 The Boeing Company Planked stringers that provide structural support for an aircraft wing
US10207789B2 (en) * 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
US10308342B2 (en) * 2016-09-07 2019-06-04 The Boeing Company Method of repairing damage to fuselage barrel and associated apparatus and system
US10696373B2 (en) * 2016-09-13 2020-06-30 The Boeing Company Aircraft wings and aircraft including such aircraft wings
CN106697327B (zh) * 2016-12-19 2019-10-18 中航成飞民用飞机有限责任公司 飞机壁板对接结构
CN110603192B (zh) * 2017-05-01 2023-06-16 庞巴迪公司 允许位置调节的飞机机翼与机身接口
US10773789B2 (en) * 2017-07-07 2020-09-15 The Boeing Company Skin-panel interface of an aircraft
JP6978957B2 (ja) * 2018-02-13 2021-12-08 三菱重工業株式会社 組立体の製造方法、補強部材、及び組立体
US10780611B2 (en) * 2018-06-18 2020-09-22 The Boeing Company Method for co-curing perpendicular stiffeners
US11161593B2 (en) * 2019-08-05 2021-11-02 The Boeing Company T-tail joint assemblies for aircraft
US11401024B2 (en) * 2019-10-09 2022-08-02 The Boeing Company Fuselage sections having tapered wing rib interfaces
US11548607B2 (en) * 2019-12-16 2023-01-10 The Boeing Company Longitudinal beam joint for a pressure deck assembly
US11524762B2 (en) * 2020-02-21 2022-12-13 The Boeing Company Fuselage structure splice
JP7830079B2 (ja) * 2020-11-18 2026-03-16 ザ・ボーイング・カンパニー マルチセグメント式スパーの製造
CN112591073B (zh) * 2020-12-23 2021-09-24 北京北航天宇长鹰无人机科技有限公司 一种翼身结合接头及无人机

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5951800A (en) 1992-11-18 1999-09-14 Mcdonnell Douglas Corp. Fiber/metal laminate splice
GB2409443A (en) 2003-12-23 2005-06-29 Airbus Uk Ltd Rib for an aircraft and the manufacture thereof
FR2873347B1 (fr) * 2004-07-22 2006-11-17 Airbus France Sas Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
US7574835B2 (en) 2005-04-07 2009-08-18 The Boeing Company Composite-to-metal joint
US20070051851A1 (en) 2005-09-02 2007-03-08 The Boeing Company Multi-piece fastener for limited clearance applications
US7837148B2 (en) 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
GB0619512D0 (en) 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
US7686251B2 (en) 2006-12-13 2010-03-30 The Boeing Company Rib support for wing panels
DE102007029500B4 (de) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil
DE102007033868B4 (de) * 2007-07-20 2013-01-31 Airbus Operations Gmbh Profil mit wenigstens einem Hohlprofilquerschnitt
FR2922517B1 (fr) * 2007-10-18 2010-04-23 Airbus France Avion comportant des jonctions d'arrets de raidisseurs et procede de fabrication d'un tel avion
FR2922516B1 (fr) * 2007-10-18 2010-04-16 Airbus France Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
DE102007055233A1 (de) * 2007-11-20 2009-05-28 Airbus Deutschland Gmbh Kupplungsvorrichtung zum Zusammenfügen von Rumpfsektionen, Kombination aus einer Kupplungsvorrichtung und zumindest einer Rumpfsektion sowie Verfahren zur Herstellung der Kupplungsvorrichtung
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund
DE102008002117B4 (de) * 2008-05-30 2013-10-31 Airbus Operations Gmbh Verbund und Struktur
WO2011071939A2 (en) * 2009-12-07 2011-06-16 Global Aerosystems, Llc Wing spar splice joint
US8408493B2 (en) 2010-05-19 2013-04-02 The Boeing Company Composite stringer end trim
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
US8993097B2 (en) * 2011-10-10 2015-03-31 The Boeing Company Tapered height curved composite stringers and corresponding panels

Also Published As

Publication number Publication date
US20130233973A1 (en) 2013-09-12
JP6340451B2 (ja) 2018-06-06
CN104144852A (zh) 2014-11-12
JP6138837B2 (ja) 2017-05-31
WO2013133880A1 (en) 2013-09-12
JP2015509465A (ja) 2015-03-30
CN104144852B (zh) 2016-07-06
EP2822852B1 (en) 2016-08-31
US8684311B2 (en) 2014-04-01
EP2822852A1 (en) 2015-01-14
JP2017137052A (ja) 2017-08-10
US20140161512A1 (en) 2014-06-12
US8915471B2 (en) 2014-12-23

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