TR201809577T4 - Yapısal bileşenleri birleştirmeye yönelik ekleme takımı. - Google Patents
Yapısal bileşenleri birleştirmeye yönelik ekleme takımı. Download PDFInfo
- 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
Links
- 230000037431 insertion Effects 0.000 title 1
- 238000003780 insertion Methods 0.000 title 1
- 230000013011 mating Effects 0.000 abstract 9
- 230000000295 complement effect Effects 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
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)
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.
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) | EP3659905A1 (tr) |
JP (1) | JP6692628B2 (tr) |
CN (2) | CN110844041B (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 (10)
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)
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 |
-
2014
- 2014-12-02 US US14/557,812 patent/US9586667B2/en active Active
-
2015
- 2015-09-16 CA CA2904562A patent/CA2904562C/en active Active
- 2015-10-07 BR BR102015025612-4A patent/BR102015025612B1/pt active IP Right Grant
- 2015-11-19 JP JP2015226613A patent/JP6692628B2/ja active Active
- 2015-11-25 ES ES15196204.0T patent/ES2685805T3/es active Active
- 2015-11-25 TR TR2018/09577T patent/TR201809577T4/tr unknown
- 2015-11-25 EP EP19217714.5A patent/EP3659905A1/en not_active Withdrawn
- 2015-11-25 EP EP15196204.0A patent/EP3028940B1/en active Active
- 2015-11-25 PT PT151962040T patent/PT3028940T/pt unknown
- 2015-11-25 EP EP18172583.9A patent/EP3388330B1/en active Active
- 2015-11-30 CN CN201911094151.7A patent/CN110844041B/zh active Active
- 2015-11-30 CN CN201510854534.5A patent/CN105644766B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
BR102015025612A2 (pt) | 2016-08-02 |
EP3028940B1 (en) | 2018-06-06 |
EP3388330B1 (en) | 2021-10-13 |
ES2685805T3 (es) | 2018-10-11 |
PT3028940T (pt) | 2018-07-11 |
CN105644766A (zh) | 2016-06-08 |
CN110844041B (zh) | 2023-06-09 |
CN110844041A (zh) | 2020-02-28 |
CN105644766B (zh) | 2019-12-20 |
CA2904562C (en) | 2021-06-29 |
CA2904562A1 (en) | 2016-06-02 |
US20160152317A1 (en) | 2016-06-02 |
EP3659905A1 (en) | 2020-06-03 |
US9586667B2 (en) | 2017-03-07 |
EP3028940A1 (en) | 2016-06-08 |
BR102015025612B1 (pt) | 2022-08-02 |
EP3388330A1 (en) | 2018-10-17 |
JP6692628B2 (ja) | 2020-05-13 |
JP2016128314A (ja) | 2016-07-14 |
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