WO2007001365A3 - Splice joints for composite aircraft fuselages and other structures - Google Patents

Splice joints for composite aircraft fuselages and other structures Download PDF

Info

Publication number
WO2007001365A3
WO2007001365A3 PCT/US2005/032737 US2005032737W WO2007001365A3 WO 2007001365 A3 WO2007001365 A3 WO 2007001365A3 US 2005032737 W US2005032737 W US 2005032737W WO 2007001365 A3 WO2007001365 A3 WO 2007001365A3
Authority
WO
WIPO (PCT)
Prior art keywords
panel portion
structures
stiffener
attached
composite skin
Prior art date
Application number
PCT/US2005/032737
Other languages
French (fr)
Other versions
WO2007001365A2 (en
Inventor
Jeffrey F Stulc
Wallace C Chan
Brian C Clapp
Neal G Rolfes
Original Assignee
Boeing Co
Jeffrey F Stulc
Wallace C Chan
Brian C Clapp
Neal G Rolfes
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, Jeffrey F Stulc, Wallace C Chan, Brian C Clapp, Neal G Rolfes filed Critical Boeing Co
Priority to ES05858121.6T priority Critical patent/ES2606242T3/en
Priority to CA2583535A priority patent/CA2583535C/en
Priority to EP05858121.6A priority patent/EP1794050B1/en
Priority to JP2007533538A priority patent/JP5130045B2/en
Publication of WO2007001365A2 publication Critical patent/WO2007001365A2/en
Publication of WO2007001365A3 publication Critical patent/WO2007001365A3/en

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
    • B64C1/068—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
    • B64C1/068—Fuselage sections
    • 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
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • 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
    • 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
    • Y10T29/49826—Assembling or joining
    • 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
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24322—Composite web or sheet
    • Y10T428/24331—Composite web or sheet including nonapertured component
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612—Composite web or sheet
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material
    • Y10T428/24661—Forming, or cooperating to form cells

Abstract

Structures and methods for joining composite fuselage sections and other panel assemblies together are disclosed herein. In one embodiment, a shell structure configured in accordance, with the present invention includes a first panel portion (210a) positioned adjacent to a second panel portion (210b). The first panel portion (210a) can include a first stiffener (214a-214e) attached to a first composite skin (112a) , and the second panel portion (210b) can include a second stiffener (214i-214j) attached to a second composite skin (112b). The shell structure can further include a fitting (230) extending across a first edge region of the first panel portion (210a) and a second edge region of the second panel portion (210b). A first end portion (232a) of the fitting (230) can be attached to the first stiffener (214a-214e) and the first composite skin (112a), and a second end portion (232b) of the fitting (230) can be attached to a second stiffener (214i-214j) and a second composite skin (112b), to join the first panel portion (210a) to the second panel portion (210b) .
PCT/US2005/032737 2004-09-23 2005-09-14 Splice joints for composite aircraft fuselages and other structures WO2007001365A2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
ES05858121.6T ES2606242T3 (en) 2004-09-23 2005-09-14 Junction joints for airframes composed of aircraft and other structures
CA2583535A CA2583535C (en) 2004-09-23 2005-09-14 Splice joints for composite aircraft fuselages and other structures
EP05858121.6A EP1794050B1 (en) 2004-09-23 2005-09-14 Splice joints for composite aircraft fuselages and other structures
JP2007533538A JP5130045B2 (en) 2004-09-23 2005-09-14 Joint joints for composite aircraft fuselage and other structures

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/949,848 2004-09-23
US10/949,848 US7325771B2 (en) 2004-09-23 2004-09-23 Splice joints for composite aircraft fuselages and other structures

Publications (2)

Publication Number Publication Date
WO2007001365A2 WO2007001365A2 (en) 2007-01-04
WO2007001365A3 true WO2007001365A3 (en) 2007-02-22

Family

ID=36072898

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/032737 WO2007001365A2 (en) 2004-09-23 2005-09-14 Splice joints for composite aircraft fuselages and other structures

Country Status (6)

Country Link
US (6) US7325771B2 (en)
EP (1) EP1794050B1 (en)
JP (2) JP5130045B2 (en)
CA (1) CA2583535C (en)
ES (1) ES2606242T3 (en)
WO (1) WO2007001365A2 (en)

Families Citing this family (140)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8336596B2 (en) * 2002-11-22 2012-12-25 The Boeing Company Composite lamination using array of parallel material dispensing heads
US8934702B2 (en) 2003-12-02 2015-01-13 The Boeing Company System and method for determining cumulative tow gap width
US7289656B2 (en) * 2003-12-02 2007-10-30 The Boeing Company Systems and methods for determining inconsistency characteristics of a composite structure
RU2270135C2 (en) * 2004-03-04 2006-02-20 Карклин Андрей Михайлович Flying vehicle fuselage
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US20060108048A1 (en) 2004-11-24 2006-05-25 The Boeing Company In-process vision detection of flaws and fod by back field illumination
US7424902B2 (en) 2004-11-24 2008-09-16 The Boeing Company In-process vision detection of flaw and FOD characteristics
US7503368B2 (en) 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7837147B2 (en) 2005-03-18 2010-11-23 The Boeing Company Systems and methods for reducing noise in aircraft fuselages and other structures
FR2883548B1 (en) * 2005-03-23 2007-06-15 Airbus France Sas DEVICE AND METHOD FOR DISSYMMETRIC CARBON-METAL MIXED DISCHARGE
NL1030029C2 (en) * 2005-09-26 2007-03-27 Gtm Consulting B V Method and device for gluing components to a composite molded part.
NL1030066C2 (en) * 2005-09-29 2007-03-30 Gtm Consulting B V Method for manufacturing a molded part from a composite material.
FR2896768B1 (en) * 2006-01-27 2009-10-09 Eurocopter France CONTROLLED FLAMBING ANTI-CRASH COMPOSITE STRUCTURE FOR AIRCRAFT.
DE102006044683A1 (en) * 2006-02-07 2007-08-23 Grob, Margret Aircraft body and method for its production
EP2021238A2 (en) * 2006-05-15 2009-02-11 Alcoa Inc. Reinforced hybrid structures and methods thereof
DE102006025930B4 (en) * 2006-06-02 2008-09-11 Airbus Deutschland Gmbh Hull structure and method of making a hull structure
DE102006026167B3 (en) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Lightweight structural panel
DE102006026168A1 (en) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Aircraft fuselage structure and method for its manufacture
DE102006026169B4 (en) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Aircraft fuselage structure and method for its manufacture
DE102006026170B4 (en) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Aircraft fuselage structure and method for its manufacture
NL2000100C2 (en) * 2006-06-13 2007-12-14 Gtm Consulting B V Laminate from metal sheets and plastic.
US7740306B2 (en) * 2006-07-26 2010-06-22 Utilicorp L.C. Stiffeners for utility trailer structural panels
DE102006039290A1 (en) * 2006-08-22 2008-03-13 Airbus Deutschland Gmbh Frame element for aircraft component assembly system, has connecting struts that are provided with recesses for receiving ribs of aircraft structure when frame element is attached to aircraft structure
NL2000232C2 (en) * 2006-09-12 2008-03-13 Gtm Consulting B V Skin panel for an aircraft fuselage.
FR2906008B1 (en) * 2006-09-15 2008-11-07 Airbus France Sa SMOOTH CHEST AND ORBITAL JUNCTION DEVICE
US7628358B2 (en) * 2006-10-26 2009-12-08 The Boeing Company Wing panel structure
FR2910874B1 (en) * 2007-01-02 2009-02-13 Airbus France Sas SMOOTH ASSEMBLIES AT THE LEVEL OF A CIRCUMFERENTIAL JUNCTION OF AN AIRCRAFT FUSELAGE.
FR2911112B1 (en) * 2007-01-05 2009-02-13 Airbus France Sas FUSELAGE SECTION FOR AIRCRAFT AND AIRCRAFT COMPRISING SUCH A SECTION
US9511571B2 (en) 2007-01-23 2016-12-06 The Boeing Company Composite laminate having a damping interlayer and method of making the same
US7787979B2 (en) * 2007-03-14 2010-08-31 The Boeing Company Splicing fuselage sections without shims
DE102007018753B4 (en) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Fire protection room for aircraft passengers with the help of fuselage made of fiber-metal laminates
DE102007019821B4 (en) * 2007-04-26 2012-11-22 Airbus Operations Gmbh Structural element of an aircraft fuselage
US20090211697A1 (en) * 2007-05-15 2009-08-27 Heinimann Markus B Reinforced hybrid structures and methods thereof
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US20080296432A1 (en) * 2007-06-04 2008-12-04 Kernkamp Industries Corporation Method of extending length of aircraft to increase interior space
US8043458B2 (en) * 2007-06-21 2011-10-25 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom
DE102007028918A1 (en) * 2007-06-22 2009-01-02 Airbus Deutschland Gmbh Method for producing a fuselage cell of an aircraft and device
DE102007029500B4 (en) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Method for coupling stiffening profile elements and structural component
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US7998392B2 (en) * 2007-09-25 2011-08-16 The Boeing Company Method for manufacturing and attachment of wing fairings
FR2922516B1 (en) * 2007-10-18 2010-04-16 Airbus France LIGHTING OF OMEGA STIFFENERS AT THE CIRCUMFERENTIAL JUNCTION OF AN AIRCRAFT FUSELAGE
FR2922518B1 (en) * 2007-10-18 2010-04-23 Airbus France AIRCRAFT STRUCTURE COMPRISING STIFF STOP JUNCTIONS
FR2922517B1 (en) * 2007-10-18 2010-04-23 Airbus France AIRCRAFT COMPRISING SUNNY ARRESTOR JUNCTIONS AND METHOD OF MANUFACTURING SUCH A PLANE
DE102007052098A1 (en) * 2007-10-31 2009-05-14 Airbus Deutschland Gmbh Crossbar for creating a fuselage cell and method for connecting two in particular wound CFRP fuselage sections
DE102008006834A1 (en) * 2008-01-30 2009-10-15 Airbus Deutschland Gmbh Connecting arrangement for connecting two stiffening elements of different cross-sectional profile for an aircraft or spacecraft, and a shell component
DE102008008386A1 (en) * 2008-02-09 2009-08-13 Airbus Deutschland Gmbh Method for producing an FVW component
US8499631B2 (en) * 2008-02-15 2013-08-06 The Boeing Company Nondestructive inspection of aircraft stiffeners
DE102008010197B4 (en) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Method for connecting two fuselage sections with the creation of a transverse joint and transverse joint connection
DE102008012252B4 (en) 2008-03-03 2014-07-31 Airbus Operations Gmbh Composite as well as aircraft or spacecraft with such a composite
DE102008012282A1 (en) * 2008-03-03 2009-09-17 Airbus Deutschland Gmbh Hull structure for airplane
DE102008013365B4 (en) * 2008-03-10 2011-03-17 Airbus Operations Gmbh Transverse joint between two fuselage sections
US8220745B2 (en) * 2008-04-14 2012-07-17 Airbus Deutschland Gmbh Connection arrangement for connecting a first and second reinforcing element for an aircraft or spacecraft, and a shell component
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
ES2352941B1 (en) * 2008-05-16 2012-01-25 Airbus Operations, S.L. INTEGRATED AIRCRAFT STRUCTURE IN COMPOSITE MATERIAL
FR2931720B1 (en) * 2008-06-02 2010-12-17 Airbus France METHOD FOR ORBITAL ASSEMBLY OF AIRCRAFT STRINGS IN COMPOSITE MATERIAL
JP4697279B2 (en) 2008-09-12 2011-06-08 ソニー株式会社 Image display device and detection method
FR2936495B1 (en) * 2008-09-30 2011-06-03 Airbus France ASSEMBLY OF PANELS FOR AIRCRAFT FUSELAGE.
FR2936488B1 (en) * 2008-09-30 2011-04-15 Airbus France AIRCRAFT FUSELAGE TRUNK IN COMPOSITE MATERIAL WITH INTERNAL CONSTANT PROFILE
DE102008044049A1 (en) * 2008-11-25 2010-06-02 Airbus Deutschland Gmbh Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft
US20100132880A1 (en) * 2008-12-01 2010-06-03 Kevin Patrick Kelleher Composite honeycomb sandwich panel splicing
NL2002289C2 (en) * 2008-12-04 2010-06-07 Gtm Holding B V Sandwich panel, support member for use in a sandwich panel and aircraft provided with such a sandwich panel.
FR2940785B1 (en) * 2009-01-08 2012-10-26 Airbus France LONGITUDINAL JUNCTION FOR AIRCRAFT FUSELAGE PANELS IN COMPOSITE MATERIALS
DE102009009491A1 (en) * 2009-02-18 2010-09-09 Airbus Deutschland Gmbh Method for producing a shell body
US8540909B2 (en) 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
US8524356B1 (en) 2009-03-09 2013-09-03 The Boeing Company Bonded patch having multiple zones of fracture toughness
US8409384B2 (en) * 2009-03-09 2013-04-02 The Boeing Company Predictable bonded rework of composite structures
US8449703B2 (en) 2009-03-09 2013-05-28 The Boeing Company Predictable bonded rework of composite structures using tailored patches
US9492975B2 (en) 2009-03-09 2016-11-15 The Boeing Company Structural bonded patch with tapered adhesive design
US8617694B1 (en) 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
ES2390318B1 (en) * 2009-03-10 2013-09-16 Airbus Operations, S.L. CLOSED STRUCTURE IN COMPOSITE MATERIAL.
US20100233424A1 (en) * 2009-03-10 2010-09-16 The Boeing Company Composite structures employing quasi-isotropic laminates
DE102009012429B4 (en) * 2009-03-10 2012-08-30 Telair International Gmbh Floor module of a cargo deck in the fuselage of an aircraft
US8425710B2 (en) 2009-03-13 2013-04-23 The Boeing Company Automated placement of vibration damping materials
DE102009013585B4 (en) * 2009-03-17 2012-01-26 Airbus Operations Gmbh Fuselage cell structure for a hybrid aircraft
ES2371951B1 (en) * 2009-03-25 2012-11-21 Airbus Operations, S.L. PROVISION OF THE BOARD OF STRUCTURAL ELEMENTS OF A COMPOSITE MATERIAL.
DE102009014933A1 (en) 2009-03-25 2010-10-07 Airbus Operations Gmbh Method for tolerance compensation between two components and tool for carrying out the method
DE102009021369A1 (en) 2009-05-12 2010-11-18 Airbus Operations Gmbh Method for producing an aircraft fuselage and fuselage
ES2382765B1 (en) * 2009-06-29 2013-05-03 Airbus Operations, S.L. AIRCRAFT NOTEBOOK DESIGN
FR2947522B1 (en) * 2009-07-03 2011-07-01 Airbus Operations Sas FUSELAGE ELEMENT COMPRISING A FUSELAGE STRING AND JUNCTION MEANS, FUSELAGE PORTION, FUSELAGE AND AIRCRAFT
ES2376098B1 (en) * 2009-07-24 2013-02-04 Airbus Operations S.L. PROCESS OF ASSEMBLY OF FUSELAGE SECTIONS OF AN AIRCRAFT.
US9079674B1 (en) * 2009-09-18 2015-07-14 Blue Origin, Llc Composite structures for aerospace vehicles, and associated systems and methods
DE102009056533B4 (en) * 2009-12-03 2015-02-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Fuselage component
DE102009056994B4 (en) 2009-12-04 2020-03-19 Airbus Defence and Space GmbH Butt joint between fuselage sections and procedures
US20110215202A1 (en) * 2009-12-07 2011-09-08 Global Aerosystems, Llc Wing spar splice joint
CA2788948C (en) 2010-02-05 2019-03-26 Learjet Inc. System and method for fabricating a composite material assembly
DE102010018932B4 (en) 2010-04-30 2013-06-13 Airbus Operations Gmbh Perimeter stiffening for an aircraft fuselage
ES2400768B1 (en) * 2010-06-30 2014-02-12 Airbus Operations, S.L. INTERNAL AIRCRAFT STRUCTURE IN COMPOSITE MATERIAL.
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
FR2970942B1 (en) * 2011-01-28 2013-02-22 Airbus Operations Sas CONNECTING STIFF FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A VESSEL HOUSING
FR2973773B1 (en) * 2011-04-05 2013-11-29 Airbus Operations Sas METHOD FOR SLOWING THE PROPAGATION OF CRACKS IN A SECURE STRUCTURE AND A HIGHLY SECURE FRAME, ESPECIALLY A FUSELAGE
ES2401830B1 (en) * 2011-06-29 2014-04-10 Airbus Operations S.L. FILLING PANELS FOR COATINGS OF AIRCRAFT FUEL TANKS.
FR2984274B1 (en) * 2011-12-15 2014-06-27 Airbus Operations Sas SECURED BEAM, IN PARTICULAR A STRONG FUSELAGE FRAME, AS WELL AS AIRCRAFT FUSELAGE EQUIPPED WITH SUCH FRAMES
JP5924934B2 (en) 2011-12-28 2016-05-25 三菱重工業株式会社 Composite joint structure
US8740151B1 (en) * 2012-01-03 2014-06-03 The Boeing Company Adjustable splice fitting for shimless connection of structual members
CA2864881A1 (en) * 2012-02-17 2013-08-22 Saab Ab Method and mould system for net moulding of a co-cured, integrated structure
US8985514B2 (en) * 2012-06-20 2015-03-24 The Boeing Company Composite structural panels and aircraft fuselages
US8939406B2 (en) 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
US8985517B2 (en) * 2012-10-26 2015-03-24 Textron Innovations Inc. Passive cooling of transmission using mast mounted heat pipes
US8960606B2 (en) 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
EP2730495B1 (en) * 2012-11-13 2016-04-27 Airbus Operations GmbH Shell structure of a fuselage
EP2738085A1 (en) 2012-11-30 2014-06-04 Airbus Operations GmbH Aircraft fuselage structure and method
DE102013202084A1 (en) * 2013-02-08 2014-08-14 Airbus Operations Gmbh Vehicle with a planking
EP2767388A1 (en) * 2013-02-15 2014-08-20 Airbus Operations GmbH Fibre reinforced plastic profiles having sections with different fibre types
DE102013102812B4 (en) * 2013-03-19 2017-01-26 Airbus Operations Gmbh Hull structure for a means of transport, means of transport and method of making a hull structure for a means of transport
EP2808156B1 (en) 2013-05-28 2017-07-12 Airbus Operations GmbH A shell segment of an aircraft and a production method
CN105392620B (en) 2013-08-09 2018-02-13 波音公司 Composite stiffened and its manufacture method
US10479475B2 (en) 2013-08-09 2019-11-19 The Boeing Company Composite stringer beam joint structure of an aircraft
US9315254B2 (en) * 2013-10-11 2016-04-19 The Boeing Company Joint assembly and method of assembling same
US9656319B2 (en) * 2013-11-13 2017-05-23 The Boeing Company Positioning system for electromagnetic riveting
US10265915B2 (en) 2014-01-17 2019-04-23 Sikorsky Aircraft Corporation Composite bonded repair method
US9896185B2 (en) * 2014-06-23 2018-02-20 Greenpoint Technologies, Inc. Aircraft interior flooring systems
USD777014S1 (en) * 2014-08-12 2017-01-24 Servi-Sure, LLC Integrated stiffener
US9555587B2 (en) 2014-08-13 2017-01-31 The Boeing Company Composite layup tools for aircraft fuselage barrels, methods of assembling the layup tools, and aircraft fuselage barrel sections formed utilizing the layup tools
US9399510B2 (en) * 2014-08-20 2016-07-26 The Boeing Company Hat stringer closeout fitting and method of making same
US10183804B2 (en) * 2014-08-25 2019-01-22 Heil Trailer International, Llc Tank trailer having integrated heat panels
US9499275B2 (en) * 2014-10-16 2016-11-22 Rohr, Inc. Stress-relieving joint between materials with differing coefficients of thermal expansion
US9545759B2 (en) 2015-01-30 2017-01-17 CGTech Automated fiber placement with course trajectory compensation
US9919791B2 (en) * 2015-04-15 2018-03-20 Gulfstream Aerospace Corporation Stiffening structures, wing structures, and methods for manufacturing stiffening structures
US9981367B2 (en) 2015-07-07 2018-05-29 The Boeing Company Exterior indexing process and tooling
US10112695B2 (en) * 2015-08-20 2018-10-30 Georgian Aerospace Llc Receptacle, payload assembly and related methods for an aircraft
US10907651B2 (en) * 2016-01-12 2021-02-02 Rolls-Royce Corporation Fan track liner subassembly angled upturn joint
US10450870B2 (en) 2016-02-09 2019-10-22 General Electric Company Frangible gas turbine engine airfoil
ES2900159T3 (en) * 2016-06-30 2022-03-16 Airbus Operations Gmbh Window frame system, window frame fixing system and vehicle hull window frame fixing system
CN106114915B (en) * 2016-08-26 2018-08-31 西安融智航空科技有限公司 A kind of safeguard structure of interconnected carrying heat-insulation integrative
US10308342B2 (en) * 2016-09-07 2019-06-04 The Boeing Company Method of repairing damage to fuselage barrel and associated apparatus and system
JP6838076B2 (en) * 2016-11-11 2021-03-03 三菱重工業株式会社 Parts manufacturing method and parts manufacturing system
US11845236B2 (en) 2018-03-12 2023-12-19 The Boeing Company Composite structure splice and method
FR3087188B1 (en) * 2018-10-12 2021-05-21 Airbus Operations Sas RAIDI STRUCTURAL PANEL FOR AIRCRAFT, FEATURING AN IMPROVED DESIGN
US20200122816A1 (en) * 2018-10-22 2020-04-23 The Boeing Company Bulkhead joint assembly
US11167849B2 (en) * 2018-11-06 2021-11-09 The Boeing Company Modular cargo handling system
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
US11198497B2 (en) * 2019-06-19 2021-12-14 The Boeing Company Splice fittings that are affixed to stringers via web-installed fasteners
US11725386B2 (en) * 2020-01-16 2023-08-15 Simpson Strong-Tie Company Inc. Serrated beam
US11420718B2 (en) * 2020-03-27 2022-08-23 The Boeing Company Aircraft tail assembly
FR3114574A1 (en) * 2020-09-30 2022-04-01 Airbus Operations Interface element for connecting two aircraft fuselage sections with a reduced number of parts.
US11919617B2 (en) 2020-12-17 2024-03-05 The Boeing Company Circumferential lap splices for sections of fuselage
US11845699B2 (en) 2021-09-07 2023-12-19 Blue Origin, Llc Methods for manufacturing coated composite materials
CN114212276B (en) * 2021-11-30 2023-08-11 北京卫星制造厂有限公司 Space station cabin door and assembling and adjusting method of cabin door sealing structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
US6155450A (en) * 1996-10-29 2000-12-05 Mcdonnell Douglas Corporation Composite shell shaped as a body of revolution
US6364250B1 (en) * 1998-09-25 2002-04-02 Daimlerchrysler Aerospace Airbus Gmbh Shell component for an aircraft fuselage and method of manufacturing the same
US20030080251A1 (en) * 2001-10-30 2003-05-01 The Boeing Company Light weight and high strength fuselage
US6613258B1 (en) * 1997-07-22 2003-09-02 Aerospatiale Societe Nationale Industrielle Method for making parts in composite material with thermoplastic matrix

Family Cites Families (249)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2004A (en) * 1841-03-12 Improvement in the manner of constructing and propelling steam-vessels
US1188485A (en) * 1910-09-03 1916-06-27 Underpinning & Foundation Company Tube joint and guide.
GB128643A (en) * 1917-08-22 1919-07-03 British & Colonial Aeroplane C Improvements in or relating to Aircraft Fuselages.
US1300777A (en) * 1918-03-19 1919-04-15 British & Colonial Aeroplane Company Ltd Aircraft-fuselage.
US1370288A (en) * 1918-05-28 1921-03-01 Quasiarc Company Ltd Metal plate structure
US1976257A (en) * 1930-03-12 1934-10-09 Super Marine Systems Inc Laminated body and method of making same
US1922063A (en) * 1931-05-01 1933-08-15 Curtiss Aeroplane & Motor Co Monocoque body
US2029635A (en) * 1933-04-08 1936-02-04 Ralson Alfred Birdy Fishplate for laterally joining two or more metallic strips
GB524721A (en) * 1938-02-05 1940-08-13 Amiot F Improvements in and relating to "stressed skin" fuselages or nacelles for aircraft
US2254152A (en) * 1938-04-29 1941-08-26 William Rhodes Davis Aircraft construction
US2367750A (en) * 1941-01-17 1945-01-23 Central Aircraft Corp Aircraft construction
US2292372A (en) * 1941-07-28 1942-08-11 Vultee Aircraft Inc Structural element
US2387219A (en) * 1941-08-08 1945-10-16 Vickers Armstrongs Ltd Aircraft structure
GB559954A (en) * 1942-09-07 1944-03-13 Vultee Aircraft Inc Airplane structures
US2405643A (en) * 1944-02-07 1946-08-13 Lockheed Aircraft Corp Structural connector
US2742247A (en) * 1950-10-31 1956-04-17 Handley Page Ltd Outer surfaces for craft moving in one fluid
US2639788A (en) * 1951-06-27 1953-05-26 Boeing Co Structural joint
US3271917A (en) 1959-06-12 1966-09-13 Rubenstein David Reinforced plastic constructions
US2992711A (en) * 1959-11-16 1961-07-18 Ryan Aeronautical Co Reinforcing means for attaching structural members to lightweight corrugated panels
US3071217A (en) * 1960-01-15 1963-01-01 Avro Aircraft Ltd Vibration damping in sheet metal structures
US3306797A (en) 1963-08-02 1967-02-28 Universal Moulded Fiber Glass Method and apparatus for making elongated articles of fiber reinforced resin material
US3490983A (en) * 1965-05-17 1970-01-20 Hitco Fiber reinforced structures and methods of making the same
US3507634A (en) * 1965-10-22 1970-04-21 United Aircraft Corp Composite metal structure
US3452501A (en) * 1966-05-02 1969-07-01 Ernest C Zimmer Snap locking structural device
US3603096A (en) 1969-12-10 1971-09-07 Atomic Energy Commission Apparatus for installing a reinforced vessel in an underground cavity
US3879245A (en) * 1972-06-27 1975-04-22 Composite Structures Corp Method of making composite cored structures
US3974313A (en) 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
US3995080A (en) 1974-10-07 1976-11-30 General Dynamics Corporation Filament reinforced structural shapes
US3976269A (en) * 1974-12-19 1976-08-24 The Boeing Company Intrinsically tuned structural panel
US4086378A (en) 1975-02-20 1978-04-25 Mcdonnell Douglas Corporation Stiffened composite structural member and method of fabrication
US4064534A (en) 1976-04-20 1977-12-20 Leone International Sales Corporation System for monitoring the production of items which are initially difficult to physically inspect
US4050208A (en) * 1976-10-04 1977-09-27 The Boeing Company Aircraft interior ceiling panel assembly and attachment apparatus
US4186535A (en) * 1977-06-10 1980-02-05 Verco Manufacturing, Inc. Shear load resistant structure
US4331495A (en) 1978-01-19 1982-05-25 Rockwell International Corporation Method of fabricating a reinforced composite structure
US4256790A (en) * 1978-01-19 1981-03-17 Rockwell International Corporation Reinforced composite structure and method of fabrication thereof
US4310132A (en) * 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US4828202A (en) * 1979-09-27 1989-05-09 The Boeing Company Method and apparatus for wideband vibration damping of reinforced skin structures
US4490958A (en) * 1979-12-12 1985-01-01 Lowe Colin F Sheet metal beam
US4311661A (en) 1980-05-05 1982-01-19 Mcdonnell Douglas Corporation Resin impregnation process
IL63240A (en) * 1980-07-11 1984-12-31 Weecan Marine Method and apparatus for manufacturing an integral shell formed body
DE3040838C2 (en) 1980-10-30 1984-10-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Method and device for the production of flat components from fiber-reinforced materials
US4331723A (en) 1980-11-05 1982-05-25 The Boeing Company Advanced composite
FR2497726A1 (en) 1981-01-12 1982-07-16 Brochier Fils J MULTILAYER TEXTILE ARTICLE FOR REINFORCING LAMINATED MATERIALS AND PROCESS FOR OBTAINING THE SAME
US4448838A (en) * 1981-09-04 1984-05-15 Lear Fan Corp. Graphite fiber reinforced laminate structure capable of withstanding lightning strikes
US4463044A (en) * 1981-09-28 1984-07-31 The Boeing Company Composite panel of varied thickness
JPS58208362A (en) * 1982-05-28 1983-12-05 Mitsubishi Heavy Ind Ltd Bagging adhesion to structure
DE3277865D1 (en) 1982-07-19 1988-02-04 Boeing Co Method and apparatus for fiber lamination
US4492607A (en) 1983-02-22 1985-01-08 Rockwell International Corporation Method for producing integrally stiffened fiber reinforced plastic panels
US4715560A (en) * 1983-03-14 1987-12-29 Lear Fan Limited Composite cruciform structure for joining intersecting structural members of an airframe and the like
DE3331494A1 (en) 1983-09-01 1985-03-21 Rudolf 8900 Augsburg Güthler Multi-web laying machine
US4542055A (en) 1983-10-19 1985-09-17 Conceptual Arts, Ltd. Three-dimensional fabric painting surfaces
US4736566A (en) * 1984-01-17 1988-04-12 Krotsch Harold V Modular fabrication panel system
US4548017A (en) * 1984-01-23 1985-10-22 Liverpool Industries, Inc. Building panel
IT1173394B (en) 1984-02-28 1987-06-24 Rockwell Rimoldi Spa DIFFERENTIAL TRANSPORT SEWING MACHINE TRANSPORT DEVICE
DE3412846A1 (en) 1984-04-05 1985-10-17 Hoechst Ag, 6230 Frankfurt AREA SHAPED SANDWICH MOLDED BODY
US4877471A (en) * 1984-08-24 1989-10-31 The Boeing Company Method and apparatus for delivering a resin-impregnated, multifilament band
US4548859A (en) * 1984-10-12 1985-10-22 The Boeing Company Breather material and method of coating fabric with silicone rubber
US4571355A (en) 1984-11-28 1986-02-18 The Boeing Company Fiber reinforced resin composites formed of basic ply blankets
US4622091A (en) 1984-11-29 1986-11-11 The Boeing Company Resin film infusion process and apparatus
US4608220A (en) * 1984-12-20 1986-08-26 The Boeing Company Method of forming composite material articles
JPS61169394A (en) 1985-01-21 1986-07-31 日立造船株式会社 Method of molding fuselage of aircraft
FR2579130B1 (en) 1985-03-25 1987-10-09 Aerospatiale METHOD AND DEVICE FOR PRODUCING A HOLLOW PART OF COMPLEX SHAPE BY FILAMENTARY WINDING IN CONTACT
US4615935A (en) 1985-04-29 1986-10-07 The Boeing Company Glass fiber reinforced ceramic preform and method of casting it
US4966802A (en) 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
US4780262A (en) 1986-01-15 1988-10-25 The Boeing Company Method for making composite structures
US4693678A (en) * 1986-01-15 1987-09-15 The Boeing Company Male layup-female molding system for fabricating reinforced composite structures
US4699683A (en) * 1986-02-07 1987-10-13 The Boeing Company Multiroving fiber laminator
SE453156B (en) * 1986-04-30 1988-01-18 Elekta Instr Sa RADIATION KNIFE INCLUDING A LARGE NUMBER WITHIN A PROTECTION PROTECTED
DE3614618A1 (en) 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm SHELL STRUCTURE MADE OF FIBER REINFORCED PLASTIC
US4830298A (en) * 1986-09-30 1989-05-16 The Boeing Company Self-centering sheave for filaments
US4760444A (en) * 1987-07-22 1988-07-26 Csd International, Inc. Machine visual inspection device and method
US4941182A (en) * 1987-07-29 1990-07-10 Phoenix Software Development Co. Vision system and method for automated painting equipment
JPH0725649B2 (en) 1987-10-12 1995-03-22 而至歯科工業株式会社 Disinfectant-containing alginate impression material
JP2604607B2 (en) 1987-12-09 1997-04-30 三井金属鉱業株式会社 Defect distribution measurement method and equipment
US4959110A (en) 1988-05-11 1990-09-25 Morton Thiokol Inc. Method for lining the inner surface of a cylindrical or domed cylindrical member with an elastomeric material
FR2632604B1 (en) * 1988-06-08 1991-07-12 Aerospatiale FRAME OF COMPOSITE MATERIAL IN PARTICULAR FOR AIRCRAFT FUSELAGE, AND METHOD FOR MANUFACTURING SAME
GB2224000B (en) 1988-11-10 1992-05-27 Genrikh Vasilievich Novozhilov Aircraft fuselage or other pressure vessel.
US4942013A (en) 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
US5251849A (en) * 1989-12-26 1993-10-12 Florida International University For Board Of Regents Strain reduced airplane skin
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
US5086997A (en) * 1990-04-02 1992-02-11 The Boeing Company Structural joint and a method for joining in reinforced thermoplastic fabrication
FR2661872B1 (en) 1990-05-11 1992-09-04 Rockwell Automotive Body Syst METHOD OF MANUFACTURING A FABRIC-COVERED SUN VISOR.
US5058497A (en) * 1990-12-17 1991-10-22 Mcdonnell Douglas Corporation Compliant pressure roller
US5262220A (en) 1991-06-18 1993-11-16 Chem-Tronics, Inc. High strength structure assembly and method of making the same
US5240376A (en) 1991-07-31 1993-08-31 Mcdonnell Douglas Corporation SPF/DB hollow core fan blade
US5337647A (en) * 1992-03-13 1994-08-16 The Boeing Company 3 dimensional braiding apparatus
US5281388A (en) 1992-03-20 1994-01-25 Mcdonnell Douglas Corporation Resin impregnation process for producing a resin-fiber composite
JPH05286493A (en) * 1992-04-08 1993-11-02 Honda Motor Co Ltd Fuselage structure of aircraft
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage
US5297760A (en) * 1992-08-21 1994-03-29 Mcdonnell Douglas Corporation Aircraft skin lap splice
US5651600A (en) * 1992-09-28 1997-07-29 The Boeing Company Method for controlling projection of optical layup template utilizing cooperative targets
US5450147A (en) * 1992-09-28 1995-09-12 The Boeing Company Method for controlling projection of optical layup template utilizing cooperative targets
US5560102A (en) * 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly
US5951800A (en) * 1992-11-18 1999-09-14 Mcdonnell Douglas Corp. Fiber/metal laminate splice
JPH06226889A (en) * 1993-02-05 1994-08-16 Sky Alum Co Ltd Panel material and composite panel using the same
US5765329A (en) * 1993-06-28 1998-06-16 Huang; Chihshu Roof construction of corrugated sheets
US6045651A (en) * 1993-09-07 2000-04-04 The Boeing Company Hand assisted lamination system
US5439549A (en) * 1993-12-28 1995-08-08 The Boeing Company Double edged pressure sensitive folded tape application apparatus
DE4408476C2 (en) * 1994-03-14 1996-04-11 Daimler Benz Aerospace Airbus Fuselage skin for an airplane
RU2083371C1 (en) * 1994-04-28 1997-07-10 Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения Carrying tubular housing of composite materials, method and holder- adapter for manufacturing thereof
US5540126A (en) * 1994-05-26 1996-07-30 Piramoon Technologies Automatic lay-up machine for composite fiber tape
US5562788A (en) 1994-09-20 1996-10-08 The Boeing Company Composite material laser flaw detection
US5622733A (en) * 1994-10-04 1997-04-22 Rockwell International Corporation Tooling for the fabrication of composite hollow crown-stiffened skins and panels
US5683646A (en) 1995-05-10 1997-11-04 Mcdonnell Douglas Corporation Fabrication of large hollow composite structure with precisely defined outer surface
US5619837A (en) * 1995-07-26 1997-04-15 Disanto; Fabricio N. Corrugated panel structure
RU2099194C1 (en) * 1995-12-01 1997-12-20 Акционерное общество "Центр перспективных разработок" Акционерного общества "Центральный научно-исследовательский институт специального машиностроения" Carrying pipe-shell in the form of body of revolution made of composite materials, method and mandrel for its manufacture
US5893534A (en) * 1995-12-22 1999-04-13 The Boeing Company Structural apparatus and design to prevent oil can movement of webs in aircraft pressure bulkheads
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US5700337A (en) 1996-03-01 1997-12-23 Mcdonnell Douglas Corporation Fabrication method for composite structure adapted for controlled structural deformation
US5746553A (en) * 1996-04-08 1998-05-05 The Boeing Company Dual purpose lay-up tool
US6205239B1 (en) * 1996-05-31 2001-03-20 Texas Instruments Incorporated System and method for circuit repair
US6013341A (en) * 1996-08-19 2000-01-11 Mcdonnell Douglas Corporation Carrying (bearing) pipe-casing made of composite materials, the method and the setting (straightening device) for its manufacturing
US5809805A (en) 1996-09-03 1998-09-22 Mcdonnell Douglas Corporation Warp/knit reinforced structural fabric
US5963660A (en) 1996-09-26 1999-10-05 The Boeing Company Method and apparatus for detecting and measuring laps and gaps in composite materials
US6187411B1 (en) * 1996-10-04 2001-02-13 The Boeing Company Stitch-reinforced sandwich panel and method of making same
AU6137798A (en) 1997-01-29 1998-08-18 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
US6692681B1 (en) * 1997-01-29 2004-02-17 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
DE59806899D1 (en) * 1997-02-05 2003-02-20 Anatoli J Vassiliev Airplane for passenger and / or freight transportation
US6051089A (en) 1997-02-07 2000-04-18 Mcdonnell Douglas Corporation Reinforcing member for composite workpieces and associated methods
JPH10258463A (en) * 1997-03-19 1998-09-29 Fuji Heavy Ind Ltd Rib of composite material and forming method thereof
KR100583036B1 (en) * 1997-05-06 2006-05-24 스피릿 에어로시스템즈, 인크. Hybrid lay-up tool
US5954917A (en) * 1997-06-02 1999-09-21 Boeing North American, Inc. Automated material delivery system
US6074716A (en) * 1997-06-10 2000-06-13 Mcdonnell Douglas Corporation Weavable metal matrix impregnated tow composite material
US5902535A (en) 1997-07-30 1999-05-11 Mcdonnell Douglas Corporation Resin film infusion mold tooling and molding method
DE19735452C2 (en) * 1997-08-16 1999-07-22 Bodenseewerk Geraetetech Pipe connection, in particular for connecting two tubular fuselage parts of a missile
US5979531A (en) 1997-10-01 1999-11-09 Mcdonnell Douglas Corporation Bi-directional fiber placement head
US5931107A (en) 1997-12-22 1999-08-03 Mcdonnell Douglas Corporation Advanced stitching head for making stitches in a textile article having variable thickness
US5915317A (en) 1997-12-22 1999-06-29 Thrash; Patrick J. Automated gantry-type stitching system
US6128545A (en) 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Automated apparatus and method of generating native code for a stitching machine
US5953231A (en) 1997-12-22 1999-09-14 Mcdonnell Douglas Corporation Automated quality control for stitching of textile articles
US6198983B1 (en) 1997-12-22 2001-03-06 Mcdonnell Douglas Corporation Table-driven software architecture for a stitching system
US6099906A (en) 1998-06-22 2000-08-08 Mcdonnell Douglas Corporation Immersion process for impregnation of resin into preforms
US6231941B1 (en) 1998-07-14 2001-05-15 The Boeing Company Radius fillers for a resin transfer molding process
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
US6086696A (en) * 1998-07-21 2000-07-11 The Boeing Company Method of forming a seamless, cylindrical, thermoplastic structure with a multiple compaction roller winder
FI982095A (en) * 1998-09-29 2000-03-30 Nokia Networks Oy Method of implementing memory and memory arrangement
US6112792A (en) * 1998-11-19 2000-09-05 The Boeing Company Fiber placement mid-span redirect
US6190484B1 (en) * 1999-02-19 2001-02-20 Kari Appa Monolithic composite wing manufacturing process
WO2000052886A1 (en) 1999-03-02 2000-09-08 Microsoft Corporation Scalable multiparty conferencing and collaboration system and method of dynamically allocating system resources
US6261675B1 (en) 1999-03-23 2001-07-17 Hexcel Corporation Core-crush resistant fabric and prepreg for fiber reinforced composite sandwich structures
US6319447B1 (en) 1999-04-09 2001-11-20 The Boeing Company Resin transfer molding process
US6136237A (en) 1999-04-13 2000-10-24 The Boeing Company Method of fabricating a fiber-reinforced ceramic matrix composite part
US6510961B1 (en) 1999-04-14 2003-01-28 A&P Technology Integrally-reinforced braided tubular structure and method of producing the same
US6431837B1 (en) 1999-06-01 2002-08-13 Alexander Velicki Stitched composite fan blade
US7132161B2 (en) 1999-06-14 2006-11-07 Energy Science Laboratories, Inc. Fiber adhesive material
BR0013763A (en) * 1999-09-03 2002-07-02 Lockheed Corp Welding applied with friction agitation as a rivet replacement technology
US6510861B1 (en) * 1999-10-12 2003-01-28 Harvey F. Mead Universal golf umbrella
US6374750B1 (en) * 1999-11-16 2002-04-23 Aero Transportation Products, Inc. Structural panel system
US6129031A (en) 1999-11-16 2000-10-10 The Boeing Company Robotic stitching apparatus and end effector therefor
US6241710B1 (en) * 1999-12-20 2001-06-05 Tricardia Llc Hypodermic needle with weeping tip and method of use
US6390169B1 (en) * 2000-02-23 2002-05-21 The Boeing Company Conformable compaction apparatus for use with a fiber placement machine
AU2001262912A1 (en) 2000-02-25 2001-09-03 The Boeing Company Laminated composite radius filler
ES2185443B1 (en) * 2000-03-07 2004-09-01 Airbus España S.L. PROCEDURE FOR MANUFACTURING OF PREPARED PARTS IN COMPOSITE MATERIAL WITH RIGIDIZERS APPLIED IN FRESH STATE.
JP4425422B2 (en) 2000-04-14 2010-03-03 本田技研工業株式会社 Method for producing composite material structure and composite material structure produced thereby
JP4318381B2 (en) * 2000-04-27 2009-08-19 本田技研工業株式会社 Manufacturing method of fuselage structure made of fiber reinforced composite material, and fuselage structure manufactured thereby
JP4425424B2 (en) * 2000-05-01 2010-03-03 本田技研工業株式会社 Method for producing semi-cured article with joggle made of fiber reinforced composite material, and method for producing preformed structure using the same
US6451152B1 (en) * 2000-05-24 2002-09-17 The Boeing Company Method for heating and controlling temperature of composite material during automated placement
US6620484B1 (en) 2000-06-06 2003-09-16 The Boeing Company Variable density stitched-composite structural elements for energy absorption
US6415581B1 (en) * 2000-07-17 2002-07-09 Deck West, Incorporated Corrugated stiffening member
DE10037307B4 (en) 2000-07-28 2004-02-05 Honsel Gmbh & Co Kg Structural element for an aircraft, in particular an aircraft door
EP1307350B1 (en) * 2000-07-31 2005-01-26 Société de Technologie Michelin Tyre for two-wheeler comprising anti-vibration means
JP4526698B2 (en) * 2000-12-22 2010-08-18 富士重工業株式会社 COMPOSITE MATERIAL AND MANUFACTURING METHOD THEREOF
US6480271B1 (en) 2001-01-08 2002-11-12 The Boeing Company Traversing laser locating system
US6743504B1 (en) 2001-03-01 2004-06-01 Rohr, Inc. Co-cured composite structures and method of making them
US7171033B2 (en) 2001-03-28 2007-01-30 The Boeing Company System and method for identifying defects in a composite structure
SE519185C2 (en) * 2001-06-07 2003-01-28 Saab Ab aircraft Panel
US6840750B2 (en) 2001-06-11 2005-01-11 The Boeing Company Resin infusion mold tool system and vacuum assisted resin transfer molding with subsequent pressure bleed
FR2831479B1 (en) 2001-10-26 2004-01-02 Coriolis Composites METHOD FOR MANUFACTURING PROFILES HAVING A SPECIFIC SURFACE CONDITION IN FIBER REINFORCED SYNTHETIC RESINS AND MACHINE FOR CARRYING OUT THE METHOD
US6799619B2 (en) * 2002-02-06 2004-10-05 The Boeing Company Composite material collation machine and associated method for high rate collation of composite materials
US20030190455A1 (en) 2002-04-05 2003-10-09 The Boeing Company Textile joint reinforcement and associated method
JP2005527410A (en) 2002-05-29 2005-09-15 ザ・ボーイング・カンパニー Controlled atmospheric pressure resin injection process
US6860957B2 (en) 2002-06-13 2005-03-01 Kawasaki Jukogyo Kabushiki Kaisha Automatic prepreg laminating method and apparatus for carrying out the same
JP2004025946A (en) * 2002-06-24 2004-01-29 Honda Motor Co Ltd Wing structure of aircraft
US6871684B2 (en) * 2002-08-13 2005-03-29 The Boeing Company System for identifying defects in a composite structure
US6622974B1 (en) 2002-08-14 2003-09-23 The Boeing Company Geometric morphing wing with expandable spars
US20040035979A1 (en) * 2002-08-23 2004-02-26 Mccoskey William Robert Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same
FR2844510B1 (en) 2002-09-12 2006-06-16 Snecma Propulsion Solide THREE-DIMENSIONAL FIBROUS STRUCTURE OF REFRACTORY FIBERS, PROCESS FOR THE PRODUCTION THEREOF AND APPLICATION TO THERMOSTRUCTURAL COMPOSITE MATERIALS
US20040086341A1 (en) 2002-11-05 2004-05-06 Conoco Inc. Metal lined composite risers in offshore applications
US7137182B2 (en) 2002-11-22 2006-11-21 The Boeing Company Parallel configuration composite material fabricator
US20040222080A1 (en) 2002-12-17 2004-11-11 William Marsh Rice University Use of microwaves to crosslink carbon nanotubes to facilitate modification
US6896841B2 (en) 2003-03-20 2005-05-24 The Boeing Company Molding process and apparatus for producing unified composite structures
TWI221554B (en) 2003-03-21 2004-10-01 Micro Star Int Co Ltd Method in BIOS for shadow memory assignment
US8246882B2 (en) 2003-05-02 2012-08-21 The Boeing Company Methods and preforms for forming composite members with interlayers formed of nonwoven, continuous materials
US20040219855A1 (en) 2003-05-02 2004-11-04 Tsotsis Thomas K. Highly porous interlayers to toughen liquid-molded fabric-based composites
JP3782072B2 (en) 2003-05-30 2006-06-07 川崎重工業株式会社 Method and apparatus for molding composite mold
CA2529626C (en) 2003-06-16 2012-08-07 William Marsh Rice University Fabrication of carbon nanotube reinforced epoxy polymer composites using functionalized carbon nanotubes
US6957518B1 (en) * 2003-06-17 2005-10-25 Valmont Industries, Inc. Two-plate splice connection assembly
US7236625B2 (en) * 2003-07-28 2007-06-26 The Boeing Company Systems and method for identifying foreign objects and debris (FOD) and defects during fabrication of a composite structure
US7080441B2 (en) 2003-07-28 2006-07-25 The Boeing Company Composite fuselage machine and method of automated composite lay up
US7282107B2 (en) 2003-08-22 2007-10-16 The Boeing Company Multiple head automated composite laminating machine for the fabrication of large barrel section components
US7048024B2 (en) 2003-08-22 2006-05-23 The Boeing Company Unidirectional, multi-head fiber placement
US7083698B2 (en) 2003-08-22 2006-08-01 The Boeing Company Automated composite lay-up to an internal fuselage mandrel
US7228611B2 (en) 2003-11-18 2007-06-12 The Boeing Company Method of transferring large uncured composite laminates
US7289656B2 (en) 2003-12-02 2007-10-30 The Boeing Company Systems and methods for determining inconsistency characteristics of a composite structure
US7039485B2 (en) * 2004-03-12 2006-05-02 The Boeing Company Systems and methods enabling automated return to and/or repair of defects with a material placement machine
US7195201B2 (en) 2004-03-29 2007-03-27 The Boeing Company Adaptable payload enabling architecture
US7093797B2 (en) * 2004-03-29 2006-08-22 The Boeing Company Adaptable payload apparatus and methods
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7134629B2 (en) 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7193696B2 (en) 2004-04-12 2007-03-20 United Technologies Corporation Systems and methods for using light to indicate defect locations on a composite structure
ES2529448T3 (en) 2004-04-21 2015-02-20 Ingersoll Machine Tools, Inc. Automated fiber placement using multiple placement heads, replaceable stools and replaceable placement heads
US7080805B2 (en) * 2004-05-05 2006-07-25 The Boeing Company Stiffened structures and associated methods
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7802413B2 (en) * 2004-10-04 2010-09-28 The Boeing Company Apparatus and methods for reinforcing a structural panel
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US20060118244A1 (en) * 2004-12-02 2006-06-08 The Boeing Company Device for laying tape materials for aerospace applications
US7624488B2 (en) * 2004-12-07 2009-12-01 The Boeing Company One-piece barrel assembly cart
US7850387B2 (en) * 2005-01-06 2010-12-14 The Boeing Company System for reducing stress concentrations in lap joints
US7278198B2 (en) * 2005-02-01 2007-10-09 The Boeing Company Mandrel segment loader
US7360340B2 (en) * 2005-04-12 2008-04-22 Grundman Curtis M Means for securing the lower end of a wind turbine tower to a foundation
US8148276B2 (en) 2005-11-28 2012-04-03 University Of Hawaii Three-dimensionally reinforced multifunctional nanocomposites
US20080041009A1 (en) * 2006-08-18 2008-02-21 General Electric Flangeless support structures
FR2906008B1 (en) * 2006-09-15 2008-11-07 Airbus France Sa SMOOTH CHEST AND ORBITAL JUNCTION DEVICE
US7735779B2 (en) * 2006-11-02 2010-06-15 The Boeing Company Optimized fuselage structure
FR2911112B1 (en) * 2007-01-05 2009-02-13 Airbus France Sas FUSELAGE SECTION FOR AIRCRAFT AND AIRCRAFT COMPRISING SUCH A SECTION
FR2915458B1 (en) * 2007-04-25 2010-01-01 Airbus France ASSEMBLY OF FUSELAGE PANELS OF AN AIRCRAFT
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
DK2006471T3 (en) * 2007-06-20 2009-12-14 Siemens Ag Wind turbine tower and method for building a wind turbine tower
DE102007029500B4 (en) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Method for coupling stiffening profile elements and structural component
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
FR2922516B1 (en) * 2007-10-18 2010-04-16 Airbus France LIGHTING OF OMEGA STIFFENERS AT THE CIRCUMFERENTIAL JUNCTION OF AN AIRCRAFT FUSELAGE
FR2922517B1 (en) * 2007-10-18 2010-04-23 Airbus France AIRCRAFT COMPRISING SUNNY ARRESTOR JUNCTIONS AND METHOD OF MANUFACTURING SUCH A PLANE
DE102008010197B4 (en) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Method for connecting two fuselage sections with the creation of a transverse joint and transverse joint connection
DE102008012252B4 (en) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Composite as well as aircraft or spacecraft with such a composite
US8220745B2 (en) * 2008-04-14 2012-07-17 Airbus Deutschland Gmbh Connection arrangement for connecting a first and second reinforcing element for an aircraft or spacecraft, and a shell component
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
FR2931720B1 (en) * 2008-06-02 2010-12-17 Airbus France METHOD FOR ORBITAL ASSEMBLY OF AIRCRAFT STRINGS IN COMPOSITE MATERIAL
US8056297B2 (en) * 2008-09-25 2011-11-15 General Electric Company Flangeless wind tower
FR2940785B1 (en) * 2009-01-08 2012-10-26 Airbus France LONGITUDINAL JUNCTION FOR AIRCRAFT FUSELAGE PANELS IN COMPOSITE MATERIALS
US8282042B2 (en) * 2009-06-22 2012-10-09 The Boeing Company Skin panel joint for improved airflow
FR2947522B1 (en) * 2009-07-03 2011-07-01 Airbus Operations Sas FUSELAGE ELEMENT COMPRISING A FUSELAGE STRING AND JUNCTION MEANS, FUSELAGE PORTION, FUSELAGE AND AIRCRAFT
FR2947523B1 (en) * 2009-07-03 2011-07-22 Airbus Operations Sas FUSELAGE ELEMENT COMPRISING A FUSELAGE STRING AND JUNCTION MEANS
ES2400768B1 (en) * 2010-06-30 2014-02-12 Airbus Operations, S.L. INTERNAL AIRCRAFT STRUCTURE IN COMPOSITE MATERIAL.
US8196358B2 (en) * 2010-08-25 2012-06-12 Mitsubishi Heavy Industries, Ltd. Wind turbine generator tower
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
FR2976916B1 (en) * 2011-06-27 2013-07-26 Airbus Operations Sas DEVICE AND METHOD FOR ASSEMBLING TWO TRUNCONS OF AIRCRAFT FUSELAGE
US8844108B2 (en) * 2011-07-12 2014-09-30 The Boeing Company Large area repair of composite aircraft
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US8985514B2 (en) * 2012-06-20 2015-03-24 The Boeing Company Composite structural panels and aircraft fuselages
US8939406B2 (en) * 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
US9153853B2 (en) * 2012-08-24 2015-10-06 Wake Skykeeper, Llc Monopole tower reinforcement configuration and related methods
US8960606B2 (en) * 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
EP2746149B1 (en) * 2012-12-19 2019-06-19 Airbus Operations GmbH Method for the production of a connecting element, connecting element, and aircraft or spacecraft
DE102014103438A1 (en) * 2013-07-16 2015-01-22 Airbus Operations Gmbh Injection molding process for making a primary structural fastener
US9586667B2 (en) * 2014-12-02 2017-03-07 The Boeing Company Splice assembly for joining structural components
DK3277952T3 (en) * 2015-04-02 2019-06-03 Arcelormittal Tower section for wind power plant, wind power plant tower and method for assembly
US10308342B2 (en) * 2016-09-07 2019-06-04 The Boeing Company Method of repairing damage to fuselage barrel and associated apparatus and system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
US6155450A (en) * 1996-10-29 2000-12-05 Mcdonnell Douglas Corporation Composite shell shaped as a body of revolution
US6613258B1 (en) * 1997-07-22 2003-09-02 Aerospatiale Societe Nationale Industrielle Method for making parts in composite material with thermoplastic matrix
US6364250B1 (en) * 1998-09-25 2002-04-02 Daimlerchrysler Aerospace Airbus Gmbh Shell component for an aircraft fuselage and method of manufacturing the same
US20030080251A1 (en) * 2001-10-30 2003-05-01 The Boeing Company Light weight and high strength fuselage

Also Published As

Publication number Publication date
JP2008514484A (en) 2008-05-08
US8869403B2 (en) 2014-10-28
US20160251071A1 (en) 2016-09-01
ES2606242T3 (en) 2017-03-23
EP1794050A2 (en) 2007-06-13
US7325771B2 (en) 2008-02-05
CA2583535C (en) 2013-05-14
US20170183075A1 (en) 2017-06-29
CA2583535A1 (en) 2007-01-04
US20120061512A1 (en) 2012-03-15
JP5130045B2 (en) 2013-01-30
US20060060705A1 (en) 2006-03-23
US8882040B2 (en) 2014-11-11
US20140165361A1 (en) 2014-06-19
US8061035B2 (en) 2011-11-22
US20080111026A1 (en) 2008-05-15
US9738371B2 (en) 2017-08-22
JP5602705B2 (en) 2014-10-08
EP1794050B1 (en) 2016-11-09
WO2007001365A2 (en) 2007-01-04
JP2012066818A (en) 2012-04-05
US10689086B2 (en) 2020-06-23

Similar Documents

Publication Publication Date Title
WO2007001365A3 (en) Splice joints for composite aircraft fuselages and other structures
WO2008054499A3 (en) Composite wing-body joint
US8915471B2 (en) Bonded splice joint
KR101858274B1 (en) Circumference splice for joining shell structures
RU2427500C2 (en) Aircraft skin-to-butt plate joint, aircraft design, wing and method of producing aircraft skin-to-butt plate joint
US7371304B2 (en) Apparatuses and methods for joining structural members, such as composite structural members
CA2817735C (en) Splice and associated method for joining fuselage sections
JP2008514484A5 (en)
US8746621B2 (en) Connector for stiffening frames between an aircraft fuselage and a wing box
ES2908176T3 (en) Bonding of Composite Fuselage Sections Along Window Bands
WO2009017864A3 (en) Fastener-free primary structural joint for sandwich panels
RU2482997C2 (en) Aircraft wing-fuselage assembly component for connection of two wings and fuselage section
WO2008152248A8 (en) Aircraft structural element located at the interface between a wing and the fuselage
US9216811B2 (en) Aircraft comprising an improved connection zone between a front beam and a front lower fuselage section
JP2012162147A5 (en)
WO2004057120A3 (en) Large composite structures and a process for fabricating large composite structures
US20050183260A1 (en) Device for assembly of several elements by riveting and procedure for assembly of panels especially for aircraft fuselages by means of said device
CN210950759U (en) Edge sealing structure and edge sealing connecting structure
CA2845453A1 (en) Composite panels and assemblies

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 2583535

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 2007533538

Country of ref document: JP

NENP Non-entry into the national phase

Ref country code: DE

121 Ep: the epo has been informed by wipo that ep was designated in this application
REEP Request for entry into the european phase

Ref document number: 2005858121

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2005858121

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 2005858121

Country of ref document: EP