PT3028940T - Conjunto de emenda para união de componentes estruturais - Google Patents

Conjunto de emenda para união de componentes estruturais

Info

Publication number
PT3028940T
PT3028940T PT151962040T PT15196204T PT3028940T PT 3028940 T PT3028940 T PT 3028940T PT 151962040 T PT151962040 T PT 151962040T PT 15196204 T PT15196204 T PT 15196204T PT 3028940 T PT3028940 T PT 3028940T
Authority
PT
Portugal
Prior art keywords
structural components
splice assembly
joining structural
joining
splice
Prior art date
Application number
PT151962040T
Other languages
English (en)
Inventor
C Reeves Andrew
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 PT3028940T publication Critical patent/PT3028940T/pt

Links

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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • 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
    • B64C1/064—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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/069—Joining arrangements therefor
    • 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
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Automatic Assembly (AREA)
PT151962040T 2014-12-02 2015-11-25 Conjunto de emenda para união de componentes estruturais PT3028940T (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/557,812 US9586667B2 (en) 2014-12-02 2014-12-02 Splice assembly for joining structural components

Publications (1)

Publication Number Publication Date
PT3028940T true PT3028940T (pt) 2018-07-11

Family

ID=54705061

Family Applications (1)

Application Number Title Priority Date Filing Date
PT151962040T PT3028940T (pt) 2014-12-02 2015-11-25 Conjunto de emenda para união de componentes estruturais

Country Status (9)

Country Link
US (1) US9586667B2 (pt)
EP (3) EP3659905A1 (pt)
JP (1) JP6692628B2 (pt)
CN (2) CN110844041B (pt)
BR (1) BR102015025612B1 (pt)
CA (1) CA2904562C (pt)
ES (1) ES2685805T3 (pt)
PT (1) PT3028940T (pt)
TR (1) TR201809577T4 (pt)

Families Citing this family (10)

* 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
EP3173330B1 (en) * 2015-11-30 2018-06-06 Airbus Operations GmbH Rod connection system, structural aircraft component and connector stud
US10934020B2 (en) 2017-01-25 2021-03-02 The Boeing Company Method and system for joining structures
DE102018222431B4 (de) * 2018-12-20 2023-12-07 Premium Aerotec Gmbh Rumpfbauteil für ein Luftfahrzeug, Verfahren zur Herstellung eines Rumpfbauteils sowie Luftfahrzeug
FR3094255B1 (fr) * 2019-03-27 2022-07-01 Airbus Operations Sas procede d’assemblage de pieces structurelles
US11198497B2 (en) 2019-06-19 2021-12-14 The Boeing Company Splice fittings that are affixed to stringers via web-installed fasteners
US11873072B2 (en) 2021-01-20 2024-01-16 The Boeing Company Pressure bulkhead assembly methods and systems
US11845528B2 (en) 2021-01-20 2023-12-19 The Boeing Company Pressure bulkhead assembly and method and system for making the same
US12017748B2 (en) * 2021-03-17 2024-06-25 The Boeing Company Fuselage barrel assemblies and methods of assembling fuselage barrel assemblies
GB2612958B (en) * 2021-11-08 2023-12-20 Airbus Operations Ltd Panel assembly

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB641432A (en) 1947-01-17 1950-08-09 Sncan Improved assembling device and applications thereof, in particular to the structuresof aircraft
GB821147A (en) * 1956-08-31 1959-09-30 Arthur Frederick Johnson Improvements in and relating to cloches or frames and greenhouses for horticulture and the like
FR2566812B2 (fr) 1984-07-02 1986-12-26 Lattre Jean De Mur de palplanches a elements plies a froid
US4809480A (en) * 1986-04-18 1989-03-07 Hale Cecil E Building metal support apparatus and method
AT400390B (de) 1992-02-05 1995-12-27 Seebach Metallwaren Profilleistensystem
US6105902A (en) 1997-07-15 2000-08-22 Mcdonnell Douglas Corporation Aircraft fuselage and method of forming same
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
FR2910874B1 (fr) 2007-01-02 2009-02-13 Airbus France Sas Lisses assemblees au niveau d'une jonction circonferentielle d'un fuselage d'avion.
US20100116938A1 (en) * 2008-11-13 2010-05-13 Kline William T Method and apparatus for joining composite structural members and structural members made thereby
GB0901640D0 (en) * 2009-02-03 2009-03-11 Airbus Uk Ltd Joint
ES2385906B1 (es) * 2009-09-30 2013-06-17 Airbus Operations, S.L. Disposición de unión circunferencial de elementos estructurales con un elemento de acoplamiento realizado en material compuesto.
US8408493B2 (en) * 2010-05-19 2013-04-02 The Boeing Company Composite stringer end trim
US20120043449A1 (en) 2010-08-19 2012-02-23 Jacob Sajan Joseph Clamp assembly
FR2970463B1 (fr) * 2011-01-17 2013-02-15 Airbus Operations Sas Dispositif d'eclissage a tenue mecanique amelioree.
FR2976916B1 (fr) 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
US8993097B2 (en) * 2011-10-10 2015-03-31 The Boeing Company Tapered height curved composite stringers and corresponding panels
US8960606B2 (en) 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
FR3006297B1 (fr) * 2013-05-29 2016-07-15 Airbus Operations Sas Procede d'assemblage de deux panneaux comportant des raidisseurs a l'aide d'eclisses et aeronef comprenant une zone de jonction amelioree entre une poutre ventrale et une barque avant

Also Published As

Publication number Publication date
BR102015025612B1 (pt) 2022-08-02
EP3388330A1 (en) 2018-10-17
CN110844041B (zh) 2023-06-09
CN105644766A (zh) 2016-06-08
JP2016128314A (ja) 2016-07-14
EP3388330B1 (en) 2021-10-13
EP3659905A1 (en) 2020-06-03
CA2904562A1 (en) 2016-06-02
US20160152317A1 (en) 2016-06-02
CN110844041A (zh) 2020-02-28
US9586667B2 (en) 2017-03-07
JP6692628B2 (ja) 2020-05-13
BR102015025612A2 (pt) 2016-08-02
CN105644766B (zh) 2019-12-20
ES2685805T3 (es) 2018-10-11
TR201809577T4 (tr) 2018-07-23
CA2904562C (en) 2021-06-29
EP3028940A1 (en) 2016-06-08
EP3028940B1 (en) 2018-06-06

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