WO2007053156A3 - One-piece barrel assembly cart - Google Patents

One-piece barrel assembly cart Download PDF

Info

Publication number
WO2007053156A3
WO2007053156A3 PCT/US2005/042472 US2005042472W WO2007053156A3 WO 2007053156 A3 WO2007053156 A3 WO 2007053156A3 US 2005042472 W US2005042472 W US 2005042472W WO 2007053156 A3 WO2007053156 A3 WO 2007053156A3
Authority
WO
WIPO (PCT)
Prior art keywords
assembly cart
barrel
piece
assembly
cart
Prior art date
Application number
PCT/US2005/042472
Other languages
French (fr)
Other versions
WO2007053156A2 (en
Inventor
Noel A Spishak
David L Wagner
Darrell D Jones
Matthew K Lum
Vincent T Olson
Joseph A Appleton
Thomas D Hall
Original Assignee
Boeing Co
Noel A Spishak
David L Wagner
Darrell D Jones
Matthew K Lum
Vincent T Olson
Joseph A Appleton
Thomas D Hall
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, Noel A Spishak, David L Wagner, Darrell D Jones, Matthew K Lum, Vincent T Olson, Joseph A Appleton, Thomas D Hall filed Critical Boeing Co
Priority to EP05858629A priority Critical patent/EP1831072A2/en
Priority to JP2007545505A priority patent/JP5046955B2/en
Publication of WO2007053156A2 publication Critical patent/WO2007053156A2/en
Publication of WO2007053156A3 publication Critical patent/WO2007053156A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B5/00—Clamps
    • B25B5/14—Clamps for work of special profile
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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
    • Y10T29/49904—Assembling a subassembly, then assembling with a second subassembly
    • 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
    • Y10T29/49998—Work holding
    • 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
    • Y10T29/53—Means to assemble or disassemble
    • Y10T29/53978—Means to assemble or disassemble including means to relatively position plural work parts

Abstract

A one-piece barrel assembly cart (10) includes a right assembly cart base (210) connected with a left assembly cart base (220) and at least three stabilizer rings (17, 18, 19) that are attached to the assembly cart base. The one-piece barrel assembly cart may be used to stabilize a tapered cured composite barrel (31), for example the large fuselage barrel of the aft section of a large new generation aircraft, such as a 7E7 Boeing airplane. A modular assembly cart (40) includes at least two identical modules (41). Each of these modules includes a cart base (42) and a stabilizer ring (43). The diameter of the inner surface of the stabilizer ring may vary as needed. Other modules including a fuselage support may be added. By providing modular assembly carts any shape and size of a one-piece composite barrel may be stabilized after curing of the composite material.
PCT/US2005/042472 2004-12-07 2005-11-22 One-piece barrel assembly cart WO2007053156A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP05858629A EP1831072A2 (en) 2004-12-07 2005-11-22 One-piece barrel assembly cart
JP2007545505A JP5046955B2 (en) 2004-12-07 2005-11-22 Integrated barrel assembly cart

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/005,667 US7624488B2 (en) 2004-12-07 2004-12-07 One-piece barrel assembly cart
US11/005,667 2004-12-07

Publications (2)

Publication Number Publication Date
WO2007053156A2 WO2007053156A2 (en) 2007-05-10
WO2007053156A3 true WO2007053156A3 (en) 2007-10-04

Family

ID=36572884

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/042472 WO2007053156A2 (en) 2004-12-07 2005-11-22 One-piece barrel assembly cart

Country Status (4)

Country Link
US (1) US7624488B2 (en)
EP (1) EP1831072A2 (en)
JP (1) JP5046955B2 (en)
WO (1) WO2007053156A2 (en)

Families Citing this family (79)

* 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
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
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
DE102006062794B4 (en) 2006-03-29 2010-04-22 Ima Materialforschung Und Anwendungstechnik Gmbh Testing device for frame reinforced hull shells
ITTO20060518A1 (en) 2006-07-14 2008-01-15 Alenia Aeronautica Spa METHOD, EQUIPMENT AND PLANT FOR THE MANUFACTURE OF SHELL STRUCTURES
US7849729B2 (en) 2006-12-22 2010-12-14 The Boeing Company Leak detection in vacuum bags
DE102007018325B4 (en) 2007-04-18 2019-10-10 Airbus Operations Gmbh Mounting device and method for mounting a fuselage section
US8266778B2 (en) * 2007-04-18 2012-09-18 Airbus Deutschland Gmbh Assembly apparatus for the assembly of a fuselage section
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
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
CN101795822B (en) * 2007-05-31 2013-09-18 罗尔工业私人有限公司 Apparatus for fabrication of structural members
US8936695B2 (en) 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US8707766B2 (en) 2010-04-21 2014-04-29 The Boeing Company Leak detection in vacuum bags
US8333864B2 (en) 2008-09-30 2012-12-18 The Boeing Company Compaction of prepreg plies on composite laminate structures
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US8916010B2 (en) * 2007-12-07 2014-12-23 The Boeing Company Composite manufacturing method
US8752293B2 (en) 2007-12-07 2014-06-17 The Boeing Company Method of fabricating structures using composite modules and structures made thereby
US8025499B2 (en) 2008-11-03 2011-09-27 Rohr, Inc. Multi-segment tool and method for composite formation
FR2944723B1 (en) * 2009-04-27 2011-04-22 Eurocopter France TOOLS FOR MAINTAINING LOW-THICK METAL COMPONENTS COMPRISING A HOLLOW STRUCTURE, FOR THEIR WELDING TO ONE BY FRICTION
FR2946024B1 (en) * 2009-05-27 2011-07-22 Airbus France INSTALLATION FOR CARRYING OUT AN AIRCRAFT FUSELAGE TRUNK
KR101093357B1 (en) 2009-06-11 2011-12-14 한국항공우주연구원 A Horizontal Handling Tool for Launch Vehicle characterizing Flexible Horizontal Handling Stability
JP5576652B2 (en) * 2009-12-25 2014-08-20 川崎重工業株式会社 Mandrel decomposition method and mandrel decomposition apparatus for manufacturing composite material structure
JP5576651B2 (en) * 2009-12-25 2014-08-20 川崎重工業株式会社 Mandrel assembling method and mandrel assembling apparatus for manufacturing composite material structure
US8914979B2 (en) * 2011-07-21 2014-12-23 Spirit AcroSystems, Inc. System and method for assembling aircraft components
US8671536B2 (en) * 2012-03-08 2014-03-18 General Electric Company Apparatus for installing a turbine case
CN102745338B (en) * 2012-07-05 2014-04-16 浙江大学 Digitalized assembly system for bodies of large planes
US8789837B2 (en) 2012-09-18 2014-07-29 The Boeing Company Transport and assembly system and method for composite barrel segments
US10160076B2 (en) * 2012-09-18 2018-12-25 The Boeing Company Edge stabilizing system and method for composite barrel segments
KR101416830B1 (en) * 2012-10-15 2014-07-08 한국항공우주산업 주식회사 Jig for fixing a primary structure of an aircraft
US8974618B1 (en) 2012-12-04 2015-03-10 The Boeing Company Systems and methods for assembling a skin of a composite structure
US9314976B2 (en) 2013-02-15 2016-04-19 The Boeing Company Systems and methods for compacting a charge of composite material
CN103192330B (en) * 2013-03-25 2014-11-05 广州飞机维修工程有限公司 Maintaining clamp for jet braking C duct of civil aviation passenger plane
JP6219055B2 (en) * 2013-03-29 2017-10-25 三菱重工業株式会社 Airframe coupling method and strong back
US9211679B1 (en) 2013-05-03 2015-12-15 The Boeing Company Systems and methods of forming a skin for a composite structure and composite structures including the same
US9375908B2 (en) 2013-05-03 2016-06-28 The Boeing Company Flexible material transfer devices, flexible vacuum compaction devices, flexible vacuum chucks, and systems and methods including the same
US10046865B2 (en) * 2013-05-09 2018-08-14 The Boeing Company Apparatus and method for installation of a frame assembly to a body
JP6037948B2 (en) * 2013-06-12 2016-12-07 三菱日立パワーシステムズ株式会社 Rotating shaft lifting jig and rotating shaft lifting method
US9144959B1 (en) 2013-09-04 2015-09-29 The Boeing Company Methods for assembling a skin of a composite structure
US9511548B1 (en) 2013-10-16 2016-12-06 The Boeing Company Systems and methods for assembling a skin of a composite structure
JP6310268B2 (en) * 2014-02-10 2018-04-11 株式会社とわに Scrap processing equipment for aircraft
US10427254B2 (en) * 2014-04-30 2019-10-01 The Boeing Company Flexible manufacturing for aircraft structures
US10017277B2 (en) 2014-04-30 2018-07-10 The Boeing Company Apparatus, system, and method for supporting a wing assembly
US10000298B2 (en) 2014-04-30 2018-06-19 The Boeing Company Metrology system for positioning assemblies
US10046381B2 (en) 2014-07-09 2018-08-14 The Boeing Company Metrology-based system for operating a flexible manufacturing system
CN104149989B (en) * 2014-08-07 2016-05-11 天津航天长征火箭制造有限公司 For the adjustable rotation mechanism for wind of multiple diameter specification rocket rocket body
KR101687554B1 (en) * 2014-12-30 2016-12-19 한국항공우주산업 주식회사 Aircraft fuselage automatic mounting and dismounting device
US10982805B2 (en) * 2015-03-23 2021-04-20 Lockheed Martin Corporation Ergonomic device for suspending aircraft flight control apparatuses
KR101743993B1 (en) * 2015-05-19 2017-06-09 한국항공우주산업 주식회사 Separable fixing equipment use aircraft parts and that method
US10723085B2 (en) * 2015-12-17 2020-07-28 Rohr, Inc. Method of extracting mandrel for hollow-hat panel production
US20160249598A1 (en) * 2016-05-02 2016-09-01 Robert Savino Mattress and Furniture Processor
CN106428621A (en) * 2016-10-19 2017-02-22 中航飞机股份有限公司西安飞机分公司 Supporting tool for airplane main landing gear wheel
US10414004B1 (en) * 2016-11-15 2019-09-17 Mathey Investments, Inc. Pipe alignment system
USD915945S1 (en) 2016-12-20 2021-04-13 Michael Kloepfer Cylindrical semi-trailer
CN110603208B (en) 2016-12-20 2021-11-09 迈克尔·克洛普弗 Trailer, railcar, cylindrical cargo container, and squeeze panel
WO2018112622A1 (en) * 2016-12-20 2018-06-28 Titan Trailers Inc. Cylindrical cargo container construction
CN106736553A (en) * 2017-03-09 2017-05-31 尚鳌自动化工程（上海）有限公司 For airframe section curved track drilling equipment and application method
CN107128506B (en) * 2017-03-28 2019-03-26 浙江大学 A kind of adaptive support device for composite wing siding
US10895082B1 (en) 2017-06-27 2021-01-19 Gary Werlinger Rebar cage fabrication system and related methods
CA3090466C (en) 2017-09-22 2021-03-02 Titan Trailers Inc. Quasi-cylindrical cargo container and construction
DE102017125763A1 (en) * 2017-11-03 2019-05-09 Airbus Operations Gmbh Method for producing an aircraft fuselage
US11400553B2 (en) * 2017-12-15 2022-08-02 The Boeing Company Tube fixture and system
GB201802847D0 (en) * 2018-02-22 2018-04-11 Rolls Royce Power Eng Plc Component Carrier
CN108894930B (en) * 2018-06-28 2019-09-06 北京金风科创风电设备有限公司 Support assembly, assembling tool and assembling method
CN109570429B (en) * 2018-11-26 2020-12-15 首都航天机械有限公司 Super large diameter section of thick bamboo casing and # -shaped roof beam high accuracy suit instrument
US10870180B2 (en) * 2019-01-10 2020-12-22 The Boeing Company Automated engagement and handling of a structure
CN109774964A (en) * 2019-01-28 2019-05-21 陕西智翔航空科技发展有限公司 Composite material fuselage pairing type frame
US11254408B2 (en) * 2019-10-25 2022-02-22 LTA Research and Exploration, LLC Methods and apparatus for constructing airships
CN110805502A (en) * 2019-11-05 2020-02-18 西安长峰机电研究所 Multifunctional butt joint device of double-pulse engine
FR3106576B1 (en) 2020-01-28 2022-02-11 Airbus Method of assembling on a trolley a central section of an aircraft fuselage
CN113665819A (en) * 2020-05-15 2021-11-19 中航西飞民用飞机有限责任公司 Aircraft suspended structure
CN112192481B (en) * 2020-11-30 2021-04-13 中国航空制造技术研究院 A dimension shape positioner for fuselage section transfers appearance
EP4011783B1 (en) * 2020-12-09 2023-08-30 The Boeing Company Fractional pulse line for aircraft fuselage manufacturing
EP4011784A1 (en) * 2020-12-14 2022-06-15 The Boeing Company Methods and apparatuses for decoupling a fuselage from a mandrel
CN113247296B (en) * 2021-05-31 2022-08-26 浙江万丰飞机制造有限公司 Manufacturing method of installation tool for thin-wall part of airplane
CN113830324B (en) * 2021-10-09 2023-12-26 江苏航空职业技术学院 Splicing device and splicing method for middle section of airplane body
FR3138121A1 (en) * 2022-07-25 2024-01-26 Airbus Operations Assembly platform intended to manipulate at least one lower hull of an aircraft without deforming it with a view to assembling an aircraft fuselage body.

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE688453C (en) * 1938-04-10 1940-02-21 Messerschmitt Boelkow Blohm Process for the production of aircraft fuselages, wings and the like. like
US2374894A (en) * 1943-06-16 1945-05-01 Ford Motor Co Method and apparatus for assembling aircraft fuselages
GB572378A (en) * 1940-06-15 1945-10-05 Francis Logan Luxmoore Improvements in or relating to devices for use in repairing aircraft
EP0507033A1 (en) * 1991-04-05 1992-10-07 Manuel Torres Martinez Machine tool installation for supporting and machining workpieces
FR2702982A1 (en) * 1993-03-23 1994-09-30 Aerospatiale Device for positioning a tool support or the like on the outer face of a tubular structure, especially an aircraft fuselage
RU2042918C1 (en) * 1993-04-15 1995-08-27 Юрий Семенович Соломонов Process of assembly of stages of multi-stage flying vehicle in sections of transportation-and-launching container
FR2788743A1 (en) * 1999-01-22 2000-07-28 Torres Ingenieria De Procesos Assembly jig for aircraft fuselage sections has frame with mountings to support fuselage halves and components for assembly
DE10122092A1 (en) * 2001-05-07 2002-11-21 Mechanik Ct Erlangen Gmbh Fuselage element processing device has basic holding device in which fuselage element can be placed and turned

Family Cites Families (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3374528A (en) * 1965-04-01 1968-03-26 Union Tank Car Co Hopper car fabrication
US3879245A (en) 1972-06-27 1975-04-22 Composite Structures Corp Method of making composite cored structures
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
US4170813A (en) * 1976-11-26 1979-10-16 J. O. & R. H. Baird Limited Clamp for strapping ingot moulds
US4310132A (en) 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US4356615A (en) * 1980-04-17 1982-11-02 Dearman Timothy Charles Apparatus and methods for use in welding
DE3277865D1 (en) * 1982-07-19 1988-02-04 Boeing Co Method and apparatus for fiber lamination
JPS60102294A (en) * 1983-11-10 1985-06-06 Kawasaki Heavy Ind Ltd Method and device for operation in production of structural member for transporting equipment 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
US4608220A (en) * 1984-12-20 1986-08-26 The Boeing Company Method of forming composite material articles
US4693678A (en) * 1986-01-15 1987-09-15 The Boeing Company Male layup-female molding system for fabricating reinforced composite structures
US4780262A (en) * 1986-01-15 1988-10-25 The Boeing Company Method for making composite structures
US4699683A (en) * 1986-02-07 1987-10-13 The Boeing Company Multiroving fiber laminator
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
FR2632604B1 (en) * 1988-06-08 1991-07-12 Aerospatiale FRAME OF COMPOSITE MATERIAL IN PARTICULAR FOR AIRCRAFT FUSELAGE, AND METHOD FOR MANUFACTURING SAME
US5058497A (en) * 1990-12-17 1991-10-22 Mcdonnell Douglas Corporation Compliant pressure roller
US5337647A (en) * 1992-03-13 1994-08-16 The Boeing Company 3 dimensional braiding apparatus
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
US6045651A (en) * 1993-09-07 2000-04-04 The Boeing Company Hand assisted lamination system
DE4344506C2 (en) * 1993-12-24 1998-04-16 Knecht Filterwerke Gmbh Cyclone for separating oil
US5439549A (en) * 1993-12-28 1995-08-08 The Boeing Company Double edged pressure sensitive folded tape application apparatus
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
US5683646A (en) * 1995-05-10 1997-11-04 Mcdonnell Douglas Corporation Fabrication of large hollow composite structure with precisely defined outer surface
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
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
US5963660A (en) * 1996-09-26 1999-10-05 The Boeing Company Method and apparatus for detecting and measuring laps and gaps in composite materials
US6692681B1 (en) * 1997-01-29 2004-02-17 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
KR100583036B1 (en) * 1997-05-06 2006-05-24 스피릿 에어로시스템즈, 인크. Hybrid lay-up tool
US6074716A (en) * 1997-06-10 2000-06-13 Mcdonnell Douglas Corporation Weavable metal matrix impregnated tow composite material
US6276058B1 (en) * 1997-06-20 2001-08-21 Trn Business Trust System and method for manufacturing a railcar
US5979531A (en) * 1997-10-01 1999-11-09 Mcdonnell Douglas Corporation Bi-directional fiber placement head
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
DE19844035C1 (en) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Shell component for an aircraft, and method for its production
US6170141B1 (en) * 1998-09-25 2001-01-09 Stanley Aviation Corporation Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine
US6112792A (en) * 1998-11-19 2000-09-05 The Boeing Company Fiber placement mid-span redirect
GB9925610D0 (en) * 1999-10-29 1999-12-29 British Aerospace Workpiece support
US6390169B1 (en) * 2000-02-23 2002-05-21 The Boeing Company Conformable compaction apparatus for use with a fiber placement machine
US6451152B1 (en) * 2000-05-24 2002-09-17 The Boeing Company Method for heating and controlling temperature of composite material during automated placement
US6480271B1 (en) * 2001-01-08 2002-11-12 The Boeing Company Traversing laser locating system
US7171033B2 (en) 2001-03-28 2007-01-30 The Boeing Company System and method for identifying defects in a composite structure
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
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

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE688453C (en) * 1938-04-10 1940-02-21 Messerschmitt Boelkow Blohm Process for the production of aircraft fuselages, wings and the like. like
GB572378A (en) * 1940-06-15 1945-10-05 Francis Logan Luxmoore Improvements in or relating to devices for use in repairing aircraft
US2374894A (en) * 1943-06-16 1945-05-01 Ford Motor Co Method and apparatus for assembling aircraft fuselages
EP0507033A1 (en) * 1991-04-05 1992-10-07 Manuel Torres Martinez Machine tool installation for supporting and machining workpieces
FR2702982A1 (en) * 1993-03-23 1994-09-30 Aerospatiale Device for positioning a tool support or the like on the outer face of a tubular structure, especially an aircraft fuselage
RU2042918C1 (en) * 1993-04-15 1995-08-27 Юрий Семенович Соломонов Process of assembly of stages of multi-stage flying vehicle in sections of transportation-and-launching container
FR2788743A1 (en) * 1999-01-22 2000-07-28 Torres Ingenieria De Procesos Assembly jig for aircraft fuselage sections has frame with mountings to support fuselage halves and components for assembly
DE10122092A1 (en) * 2001-05-07 2002-11-21 Mechanik Ct Erlangen Gmbh Fuselage element processing device has basic holding device in which fuselage element can be placed and turned

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JP2008522898A (en) 2008-07-03
US20060118235A1 (en) 2006-06-08
EP1831072A2 (en) 2007-09-12
JP5046955B2 (en) 2012-10-10
US7624488B2 (en) 2009-12-01
WO2007053156A2 (en) 2007-05-10

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