ATE473917T1 - Flügelelement-verbundgelenk - Google Patents

Flügelelement-verbundgelenk

Info

Publication number
ATE473917T1
ATE473917T1 AT07867062T AT07867062T ATE473917T1 AT E473917 T1 ATE473917 T1 AT E473917T1 AT 07867062 T AT07867062 T AT 07867062T AT 07867062 T AT07867062 T AT 07867062T AT E473917 T1 ATE473917 T1 AT E473917T1
Authority
AT
Austria
Prior art keywords
portions
joints
element compound
wing element
skin
Prior art date
Application number
AT07867062T
Other languages
English (en)
Inventor
Max Kismarton
Willard Westre
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 ATE473917T1 publication Critical patent/ATE473917T1/de

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
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • 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
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. 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
    • 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
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/19—Sheets or webs edge spliced or joined

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Prostheses (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Revetment (AREA)
  • Road Paving Structures (AREA)
AT07867062T 2006-06-13 2007-04-06 Flügelelement-verbundgelenk ATE473917T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/423,885 US7837148B2 (en) 2006-06-13 2006-06-13 Composite wing-body joint
PCT/US2007/008695 WO2008054499A2 (en) 2006-06-13 2007-04-06 Composite wing-body joint

Publications (1)

Publication Number Publication Date
ATE473917T1 true ATE473917T1 (de) 2010-07-15

Family

ID=39304599

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07867062T ATE473917T1 (de) 2006-06-13 2007-04-06 Flügelelement-verbundgelenk

Country Status (8)

Country Link
US (1) US7837148B2 (de)
EP (1) EP2032432B1 (de)
JP (1) JP5184523B2 (de)
CN (1) CN101466595B (de)
AT (1) ATE473917T1 (de)
CA (1) CA2649125C (de)
DE (1) DE602007007771D1 (de)
WO (1) WO2008054499A2 (de)

Families Citing this family (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
EP1918193A1 (de) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Integrierte Verbundhaut für Flugzeug-Midbox-Hebeoberflächen
US7849729B2 (en) 2006-12-22 2010-12-14 The Boeing Company Leak detection in vacuum bags
US8568551B2 (en) 2007-05-22 2013-10-29 The Boeing Company Pre-patterned layup kit and method of manufacture
US9770871B2 (en) 2007-05-22 2017-09-26 The Boeing Company Method and apparatus for layup placement
US8333864B2 (en) 2008-09-30 2012-12-18 The Boeing Company Compaction of prepreg plies on composite laminate structures
US8707766B2 (en) 2010-04-21 2014-04-29 The Boeing Company Leak detection in vacuum bags
US8936695B2 (en) 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US8752293B2 (en) 2007-12-07 2014-06-17 The Boeing Company Method of fabricating structures using composite modules and structures made thereby
US8916010B2 (en) 2007-12-07 2014-12-23 The Boeing Company Composite manufacturing method
GB0803689D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Trailing edge aircraft structure with overhaning cover
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.
GB201000878D0 (en) * 2010-01-20 2010-03-10 Airbus Operations Ltd Sandwich panel
GB201005308D0 (en) 2010-03-30 2010-05-12 Airbus Operations Ltd Composite structural member
FR2962409B1 (fr) * 2010-07-09 2012-09-21 Airbus Operations Sas Procede de realisation d'un caisson central de voilure
US8333345B2 (en) * 2010-08-26 2012-12-18 The Boeing Company Composite aircraft joint
ES2396838B1 (es) * 2010-09-13 2014-02-06 Airbus Operations S.L. Disposición de unión de piezas de material compuesto reforzada direccionalmente.
GB201016279D0 (en) * 2010-09-28 2010-11-10 Airbus Operations Ltd Stiffener run-out
US8578609B2 (en) * 2010-10-27 2013-11-12 Airbus Operations S.L. Manufacturing procedure of a part made out of a composite material introducing a geometric change in one of its faces
JP5693195B2 (ja) * 2010-12-14 2015-04-01 三菱重工業株式会社 ボルト継手構造
US8997496B2 (en) * 2011-06-29 2015-04-07 United Technologies Corporation Hybrid exhaust component
EP2554471B1 (de) * 2011-08-01 2013-10-23 Eurocopter Deutschland GmbH Lastenschnittstelle, insbesondere Lastenschnittstelle einer Flugzeugstruktur
EP2554472B1 (de) * 2011-08-01 2013-12-11 Eurocopter Deutschland GmbH Lastenschnittstelle, insbesondere Lastenschnittstelle für eine Flugzeugdrucktür
US9010688B2 (en) * 2012-02-07 2015-04-21 The Boeing Company Structural joint having continuous skin with inside and outside stringers
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US10118686B2 (en) * 2012-09-27 2018-11-06 The Boeing Company Wing root insert system for an aircraft family
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
US8973871B2 (en) * 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
US9227718B2 (en) 2013-06-07 2016-01-05 The Boeing Company Lower joints between outboard wing boxes and center wing sections of aircraft wing assemblies
US9475570B2 (en) 2013-08-23 2016-10-25 The Boeing Company Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies
US9315254B2 (en) * 2013-10-11 2016-04-19 The Boeing Company Joint assembly and method of assembling same
RU2556268C1 (ru) * 2014-02-20 2015-07-10 Открытое Акционерное Общество "Научно-Производственная Корпорация "Иркут" Стык консоли крыла с центропланом самолета
US9896183B2 (en) 2014-08-25 2018-02-20 Sikorsky Aircraft Corporation Airframe component with electrically bonded connections
FR3031082B1 (fr) * 2014-12-30 2017-02-10 Airbus Operations Sas Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere
US10099445B2 (en) 2015-05-14 2018-10-16 The Boeing Company Systems and methods for forming composite materials
CN105523052B (zh) * 2015-12-20 2018-02-16 沈阳市沈飞专用设备厂 一种碳纤维蒙皮结构
US9897130B2 (en) 2016-04-15 2018-02-20 The Boeing Company Telescoping cap assembly for encapsulating a fastener disposed within a confined space
US10087970B2 (en) 2016-04-29 2018-10-02 The Boeing Company Sealant Containment Assembly
US10556665B2 (en) 2016-06-20 2020-02-11 The Boeing Company Apparatuses and methods for improved sealing
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
US10696373B2 (en) 2016-09-13 2020-06-30 The Boeing Company Aircraft wings and aircraft including such aircraft wings
US9964131B1 (en) 2017-04-28 2018-05-08 The Boeing Company Methods and apparatuses for providing corrosion protection to joined surfaces
US10773787B2 (en) 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10766598B2 (en) 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10875625B2 (en) * 2017-08-23 2020-12-29 The Boeing Company Co-cured spar and stringer center wing box
JP7090409B2 (ja) 2017-08-30 2022-06-24 三菱重工業株式会社 複合材の構造体
US10745104B2 (en) * 2018-03-02 2020-08-18 The Boeing Company Stringer transition through a common base charge
IL259149B (en) 2018-05-03 2022-09-01 Israel Aerospace Ind Ltd Structural elements made of composite materials
US10738628B2 (en) 2018-05-25 2020-08-11 General Electric Company Joint for band features on turbine nozzle and fabrication
US11231060B2 (en) 2019-01-16 2022-01-25 Bruce Daniel McFall Hybrid tension/transverse compression structural joint
FR3101611B1 (fr) * 2019-10-02 2022-02-25 Airbus Operations Sas Panneau renforcé à structure alvéolaire comprenant au moins une zone de liaison présentant une surépaisseur et aéronef comprenant au moins un tel panneau renforcé
CN111044358B (zh) * 2019-11-26 2022-08-12 中国商用飞机有限责任公司北京民用飞机技术研究中心 侧边自由的长桁截止端试验测试装置及测试方法
CN110920860A (zh) * 2019-12-16 2020-03-27 中国商用飞机有限责任公司 复材机翼
US11319051B2 (en) * 2020-01-03 2022-05-03 The Boeing Company Stiffened composite ribs
US11858623B2 (en) 2021-09-13 2024-01-02 The Boeing Company Aircraft fuel tank joints and methods of assembling the same

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4015035A (en) * 1972-08-10 1977-03-29 Lockheed Aircraft Corporation Method of forming fiber-reinforced epoxy composite joints, and product thereof
US3885071A (en) * 1972-08-10 1975-05-20 Lockheed Aircraft Corp Fiber-reinforced epoxy composite joints
US4565595A (en) 1981-09-30 1986-01-21 The Boeing Company Method of making composite aircraft wing
US4741943A (en) 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
DE3614618A1 (de) 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm Schalenstruktur aus faserverstaerktem kunststoff
DE3826378A1 (de) 1988-08-03 1990-02-08 Mtu Muenchen Gmbh Fasertechnische propellerschaufeln
US5567535A (en) * 1992-11-18 1996-10-22 Mcdonnell Douglas Corporation Fiber/metal laminate splice
US5951800A (en) * 1992-11-18 1999-09-14 Mcdonnell Douglas Corp. Fiber/metal laminate splice
US6190484B1 (en) 1999-02-19 2001-02-20 Kari Appa Monolithic composite wing manufacturing process
FR2832668B1 (fr) 2001-11-26 2004-02-13 Airbus France Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede
US7204951B2 (en) 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
DE10301445B4 (de) * 2003-01-16 2005-11-17 Airbus Deutschland Gmbh Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung
US8156711B2 (en) * 2003-02-24 2012-04-17 Bell Helicopter Textron Inc. Contact stiffeners for structural skins
US7115323B2 (en) * 2003-08-28 2006-10-03 The Boeing Company Titanium foil ply replacement in layup of composite skin
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint

Also Published As

Publication number Publication date
WO2008054499A3 (en) 2008-11-27
CN101466595A (zh) 2009-06-24
JP5184523B2 (ja) 2013-04-17
DE602007007771D1 (de) 2010-08-26
EP2032432B1 (de) 2010-07-14
WO2008054499A2 (en) 2008-05-08
CA2649125C (en) 2012-01-03
JP2009539702A (ja) 2009-11-19
EP2032432A2 (de) 2009-03-11
US7837148B2 (en) 2010-11-23
US20090084899A1 (en) 2009-04-02
CA2649125A1 (en) 2008-05-08
CN101466595B (zh) 2012-06-13

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