TR201809577T4 - Yapısal bileşenleri birleştirmeye yönelik ekleme takımı. - Google Patents

Yapısal bileşenleri birleştirmeye yönelik ekleme takımı. Download PDF

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Publication number
TR201809577T4
TR201809577T4 TR2018/09577T TR201809577T TR201809577T4 TR 201809577 T4 TR201809577 T4 TR 201809577T4 TR 2018/09577 T TR2018/09577 T TR 2018/09577T TR 201809577 T TR201809577 T TR 201809577T TR 201809577 T4 TR201809577 T4 TR 201809577T4
Authority
TR
Turkey
Prior art keywords
longitudinal axis
mating surface
mating
splicing
structural components
Prior art date
Application number
TR2018/09577T
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 TR201809577T4 publication Critical patent/TR201809577T4/tr

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)
  • Automatic Assembly (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

Mevcut buluş, birinci boylamasına eksen (Xa) dahil olmak üzere bir birinci ekleme braketini (102a), bir birinci bağlama elemanını (104a) ve birinci boylamasına eksen (Xa) boyunca birinci bağlanma elemanından (104a) uzanan bir birinci eşleşme elemanını (106a) içeren bir ekleme takımı (100) ile ilgili olup, birinci eşleşme elemanı (106a) birinci boylamasına eksene (Xa) göre sıfırdan farklı bir açıda yerleştirilen bir birinci eşleşme yüzeyini (108a) içerir. Açıklanan ekleme takımı (100) ayrıca, ikinci boylamasına eksen (Xb) dahil olmak üzere bir ikinci ekleme braketini (102b), bir ikinci bağlama elemanını (104b) ve ikinci boylamasına eksen (Xb) boyunca ikinci bağlanma elemanından (104b) uzanan bir ikinci eşleşme elemanını (106b) içermekte olup, ikinci eşleşme elemanı (106b) ikinci boylamasına eksene (Xb) göre sıfırdan farklı bir açıda yerleştirilen bir ikinci eşleşme yüzeyini (108b) içerir. Birinci eşleşme yüzeyi (108a) ve ikinci eşleşme yüzeyi (108b) bütünleyicidir. Birinci eşleşme yüzeyi (108a) ve ikinci eşleşme yüzeyi (108b) arasındaki yüzey teması, birinci ekleme braketini (102a) ve ikinci ekleme braketini (102b) bağlamak için bir bağlama yerini tanımlar.
TR2018/09577T 2014-12-02 2015-11-25 Yapısal bileşenleri birleştirmeye yönelik ekleme takımı. TR201809577T4 (tr)

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
TR201809577T4 true TR201809577T4 (tr) 2018-07-23

Family

ID=54705061

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2018/09577T TR201809577T4 (tr) 2014-12-02 2015-11-25 Yapısal bileşenleri birleştirmeye yönelik ekleme takımı.

Country Status (9)

Country Link
US (1) US9586667B2 (tr)
EP (3) EP3028940B1 (tr)
JP (1) JP6692628B2 (tr)
CN (2) CN105644766B (tr)
BR (1) BR102015025612B1 (tr)
CA (1) CA2904562C (tr)
ES (1) ES2685805T3 (tr)
PT (1) PT3028940T (tr)
TR (1) TR201809577T4 (tr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
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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
US20240425201A1 (en) * 2023-06-21 2024-12-26 The Boeing Company Systems and methods for shimless assembly and joint splices
CN121201398A (zh) * 2025-11-20 2025-12-26 中航成飞民用飞机有限责任公司 水上飞机抑波板的装配方法

Family Cites Families (20)

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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
US4256790A (en) * 1978-01-19 1981-03-17 Rockwell International Corporation Reinforced composite structure and method of fabrication thereof
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
US6855099B2 (en) * 2001-10-31 2005-02-15 The Boeing Company Manufacturing system for aircraft structures and other large structures
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
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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
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Also Published As

Publication number Publication date
CN110844041B (zh) 2023-06-09
BR102015025612A2 (pt) 2016-08-02
US20160152317A1 (en) 2016-06-02
CA2904562C (en) 2021-06-29
EP3028940A1 (en) 2016-06-08
EP3659905A1 (en) 2020-06-03
CN105644766A (zh) 2016-06-08
PT3028940T (pt) 2018-07-11
CN105644766B (zh) 2019-12-20
EP3388330A1 (en) 2018-10-17
CN110844041A (zh) 2020-02-28
JP2016128314A (ja) 2016-07-14
EP3028940B1 (en) 2018-06-06
US9586667B2 (en) 2017-03-07
CA2904562A1 (en) 2016-06-02
JP6692628B2 (ja) 2020-05-13
BR102015025612B1 (pt) 2022-08-02
EP3388330B1 (en) 2021-10-13
ES2685805T3 (es) 2018-10-11

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