AU2001262912A1 - Laminated composite radius filler - Google Patents

Laminated composite radius filler

Info

Publication number
AU2001262912A1
AU2001262912A1 AU2001262912A AU6291201A AU2001262912A1 AU 2001262912 A1 AU2001262912 A1 AU 2001262912A1 AU 2001262912 A AU2001262912 A AU 2001262912A AU 6291201 A AU6291201 A AU 6291201A AU 2001262912 A1 AU2001262912 A1 AU 2001262912A1
Authority
AU
Australia
Prior art keywords
laminated composite
radius filler
composite radius
filler
laminated
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
AU2001262912A
Inventor
Panagiotis E. George
Kirk B Kajita
Barry P. Van West
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of AU2001262912A1 publication Critical patent/AU2001262912A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545—Perforating, cutting or machining during or after moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • B29D99/0005—Producing noodles, i.e. composite gap fillers, characterised by their construction
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • Y10T428/24116—Oblique to direction of web
    • 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.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers
    • 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.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of 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.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24281—Struck out portion type
    • Y10T428/24289—Embedded or interlocked
AU2001262912A 2000-02-25 2001-02-23 Laminated composite radius filler Abandoned AU2001262912A1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US18487100P 2000-02-25 2000-02-25
US60184871 2000-02-25
US09/793,810 US6562436B2 (en) 2000-02-25 2001-02-23 Laminated composite radius filler
US09793810 2001-02-23
PCT/US2001/005687 WO2001062495A2 (en) 2000-02-25 2001-02-23 Laminated composite radius filler

Publications (1)

Publication Number Publication Date
AU2001262912A1 true AU2001262912A1 (en) 2001-09-03

Family

ID=26880551

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001262912A Abandoned AU2001262912A1 (en) 2000-02-25 2001-02-23 Laminated composite radius filler

Country Status (4)

Country Link
US (3) US6562436B2 (en)
EP (1) EP1261787A2 (en)
AU (1) AU2001262912A1 (en)
WO (1) WO2001062495A2 (en)

Families Citing this family (141)

* 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
EP1261787A2 (en) * 2000-02-25 2002-12-04 The Boeing Company Laminated composite radius filler
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
EP1534175B1 (en) 2002-08-19 2011-10-12 Crucible Intellectual Property, LLC Medical implants made of amorphous alloys
US6964723B2 (en) * 2002-10-04 2005-11-15 The Boeing Company Method for applying pressure to composite laminate areas masked by secondary features
US8211530B2 (en) * 2003-02-03 2012-07-03 Northrop Grumman Systems Corporation Adhesive fillets and method and apparatus for making same
DE602004032122D1 (en) * 2003-02-24 2011-05-19 Bell Helicopter Textron Inc CONTACT MAKER FOR CONSTRUCTION SKIN
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
US7531058B2 (en) * 2005-02-24 2009-05-12 The Boeing Company Reinforced rampdown for composite structural member and method for same
DE102005030939A1 (en) * 2005-06-30 2007-01-04 Airbus Deutschland Gmbh Method for producing a substantially cup-shaped component
EP1762357B1 (en) 2005-09-09 2015-02-25 Saab Ab Compression moulding method and device for making preforms for composite structures of an aircraft
DE102005057907B4 (en) * 2005-12-02 2012-03-22 Eurocopter Deutschland Gmbh Aircraft pressure cabin door made of fiber composite material
US8034278B2 (en) * 2006-01-13 2011-10-11 Hexcel Corporation Pressurized molding of composite parts
US8333858B2 (en) * 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US9102103B2 (en) * 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US7807005B2 (en) * 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US8691137B2 (en) 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US8491745B2 (en) 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
DE102006026167B3 (en) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Lightweight structural panel
DE102006031326B4 (en) * 2006-07-06 2010-09-23 Airbus Deutschland Gmbh Mold core and method for producing a fiber composite component for the aerospace industry
DE102006031325B4 (en) * 2006-07-06 2010-07-01 Airbus Deutschland Gmbh Method for producing a fiber composite component for aerospace applications
DE102006031323B4 (en) * 2006-07-06 2010-07-15 Airbus Deutschland Gmbh Method for producing a fiber composite component for aerospace applications
DE102006031336B4 (en) * 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Method for producing a fiber composite component in the aerospace industry
DE102006031334A1 (en) * 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Process to manufacture omega-shaped aircraft fuselage stringer using removable form core of parallel flexible tubes
DE102006031335B4 (en) * 2006-07-06 2011-01-27 Airbus Operations Gmbh Method for producing a fiber composite component for aerospace applications
US7823490B2 (en) * 2006-10-04 2010-11-02 The Boeing Company Cutting sequence for net trimming a composite layup at an oblique angle
US7997534B2 (en) * 2006-10-13 2011-08-16 Airbus Operations Gmbh Connecting structure for an aircraft or spacecraft and method for producing the same
US8475895B2 (en) 2006-11-21 2013-07-02 General Electric Company Articles comprising composite structures having mounting flanges
US8966754B2 (en) 2006-11-21 2015-03-03 General Electric Company Methods for reducing stress on composite structures
US7871486B2 (en) 2006-11-21 2011-01-18 General Electric Company Methods for making structures having mounting flanges
US20080157418A1 (en) * 2006-12-27 2008-07-03 Lee Alan Blanton Methods for fabricating composite structures with flanges having tethered corners
US7749927B2 (en) * 2006-12-27 2010-07-06 General Electric Company Tethered corners and flanges and articles comprising the same
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US8016970B2 (en) * 2007-08-02 2011-09-13 The Boeing Company Method for applying a pre-cured composite strip to a composite component to minimize inconsistencies appearing on a surface of the composite component
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US7943227B2 (en) * 2007-10-11 2011-05-17 The Boeing Company Ceramic heat shield
US7927686B2 (en) * 2007-10-11 2011-04-19 The Boeing Company Composite heat shield
US7874829B2 (en) * 2007-11-09 2011-01-25 Spirit Aerosystems, Inc. Method and apparatus for forming adhesive strips
US8540833B2 (en) 2008-05-16 2013-09-24 The Boeing Company Reinforced stiffeners and method for making the same
US10399709B2 (en) 2008-07-18 2019-09-03 The Boeing Company Method of making a device for controlling stress in joints at cryogenic temperatures
US8656571B2 (en) 2008-07-18 2014-02-25 The Boeing Company Strong bonded joints for cryogenic applications
US9453293B2 (en) 2008-07-18 2016-09-27 The Boeing Company Method of making a composite tank having joint with softening strip
US8216499B2 (en) 2008-12-09 2012-07-10 The Boeing Company Extrusion of adhesives for composite structures
GB0906686D0 (en) * 2009-04-20 2009-06-03 Airbus Uk Ltd Edge seal for fibre-reinforced composite structure
BRPI0924562A2 (en) * 2009-06-11 2016-03-01 Saab Ab nano-reinforced radius filler for an aircraft structure and a method of producing an aircraft structure comprising such filler.
CA2763259A1 (en) 2009-06-11 2010-12-16 Saab Ab A structural longitudinal composite joint for aircraft structure
US20110039057A1 (en) * 2009-08-17 2011-02-17 The Boeing Company Laminated composite rod and fabrication method
US20110054850A1 (en) * 2009-08-31 2011-03-03 Roach James T Composite laminate construction method
US8449260B2 (en) * 2009-10-30 2013-05-28 General Electric Company Composite load-bearing rotating ring and process therefor
DE102009060693A1 (en) * 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Stiffening element for an aircraft and sheet with such a stiffening element
US10821653B2 (en) * 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
DE102010003114A1 (en) * 2010-03-22 2011-09-22 Repower Systems Ag web connection
US8974135B2 (en) 2010-07-22 2015-03-10 The Boeing Company Fabric preform insert for a composite tank Y-joint
US8976531B2 (en) * 2011-01-05 2015-03-10 The Boeing Company Translating equipment rack system
US8939407B2 (en) 2011-02-15 2015-01-27 The Boeing Company Common bulkhead for composite propellant tanks
US8763253B2 (en) 2011-05-19 2014-07-01 The Boeing Company Vertical laminate noodle for high capacity pull-off for a composite stringer
US8776375B2 (en) * 2011-05-19 2014-07-15 The Boeing Company Aircraft structure for high capacity pull off
JP6009236B2 (en) * 2011-08-10 2016-10-19 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ Vertical laminated noodles for high-performance pull-off of composite stringers
US8440045B2 (en) 2011-09-14 2013-05-14 Sikorsky Aircraft Corporation Conformal deltoid noodle for a composite structure
EP2610165B1 (en) * 2011-12-28 2017-02-08 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Composite gusset filler and method of manufacture of said composite gusset filler
EP2666622B1 (en) 2012-05-22 2017-04-12 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Skin-stiffener transition assembly, method of manufacture and application of said skin-stiffener transition assembly
US9352822B2 (en) * 2012-05-30 2016-05-31 The Boeing Company Bonded composite airfoil
US8758879B2 (en) 2012-06-24 2014-06-24 The Boeing Company Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same
US9616594B2 (en) 2012-08-06 2017-04-11 The Boeing Company Radius fillers for composite structures, composite structures that include radius fillers, and systems and methods of forming the same
US9370921B2 (en) * 2012-11-01 2016-06-21 The Boeing Company Composite radius fillers and methods of forming the same
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
US9327470B1 (en) 2012-12-05 2016-05-03 The Boeing Company Variable-radius laminated radius filler and system and method for manufacturing same
US9463880B2 (en) 2013-02-07 2016-10-11 The Boeing Company Method and system of making composite structures having gap fillers with chopped fiber material
US10239289B2 (en) * 2013-04-12 2019-03-26 Hexcel Corporation Multi-component composite structures
WO2014197233A1 (en) * 2013-06-04 2014-12-11 United Technologies Corporation Vane assembly including two- and three-dimensional arrangements of continuous fibers
US10144203B2 (en) 2013-10-03 2018-12-04 The Boeing Company Pre-formed thermoplastic filler for thermoset structure
US9855702B1 (en) 2013-10-03 2018-01-02 The Boeing Company Method and apparatus for making composite fillers
US9415577B1 (en) 2013-10-03 2016-08-16 The Boeing Company Automated fabrication of composite fillers
FR3012764B1 (en) * 2013-11-05 2016-07-01 Eads Composites Aquitaine METHOD FOR MANUFACTURING A NAIL HEAD AND COMPOSITE STRUCTURE COMPRISING AT LEAST ONE SUCH NAIL HEAD
US9359060B2 (en) 2013-11-07 2016-06-07 The Boeing Company Laminated composite radius filler with geometric shaped filler element and method of forming the same
EP2878435B1 (en) * 2013-11-28 2018-07-18 Airbus Operations, S.L. Method for manufacturing an integrated composite trailing edge
US9827710B2 (en) 2014-02-04 2017-11-28 The Boeing Company Radius filler and method of manufacturing same
US9566739B2 (en) 2014-02-18 2017-02-14 The Boeing Company Composite filler
ES2799179T3 (en) * 2014-03-06 2020-12-15 Airbus Defence & Space Gmbh Fibrous composite component with radiation cross-linked filler body
US10035309B2 (en) * 2014-04-03 2018-07-31 The Boeing Company Radius fillers for composite structures, composite structures that include radius fillers, and systems and methods of forming the same
US10059068B2 (en) * 2014-04-21 2018-08-28 The Boeing Company Composite structure and method of forming thereof
US9856008B2 (en) 2014-05-19 2018-01-02 The Boeing Company Composite structure and methods of forming thereof
US10695958B2 (en) 2014-06-13 2020-06-30 The Boeing Company Lattice reinforced radius filler
US10040274B2 (en) 2014-06-17 2018-08-07 The Boeing Company Pre-filled radius layups
US10225891B2 (en) 2014-07-09 2019-03-05 The Boeing Company In-situ induction cured radius filler
US9475256B2 (en) * 2014-07-10 2016-10-25 The Boeing Company Composite filler
US9440414B2 (en) 2014-07-25 2016-09-13 The Boeing Company Fabric jacketed unidirectional noodle
US9517606B2 (en) 2014-08-06 2016-12-13 The Boeing Company Composite structure and method of forming thereof
US20160039514A1 (en) * 2014-08-08 2016-02-11 Brian T. Pitman Lateral ply layup of composite spar
US10105942B2 (en) 2014-08-20 2018-10-23 The Boeing Company Systems and methods for forming radius fillers for composite structures
US9643395B2 (en) 2014-08-20 2017-05-09 The Boeing Company Systems and methods for forming radius fillers for composite structures
US10232572B2 (en) * 2014-08-27 2019-03-19 The Boeing Company Composite filler forming apparatus
US9630376B2 (en) * 2014-09-22 2017-04-25 The Boeing Company Composite filler
US9592651B2 (en) * 2014-09-30 2017-03-14 The Boeing Company Composite structures having reduced area radius fillers and methods of forming the same
US9850102B2 (en) 2014-10-20 2017-12-26 The Boeing Company Devices and methods for handling radius fillers
US9637354B2 (en) 2014-10-20 2017-05-02 The Boeing Company Devices and methods for handling radius fillers
JP6501511B2 (en) * 2014-12-15 2019-04-17 三菱重工業株式会社 Design method of corner fillet section and aircraft
US10195817B2 (en) * 2015-01-02 2019-02-05 The Boeing Company Skin-stringer design for composite wings
US10513101B2 (en) * 2015-03-13 2019-12-24 The Boeing Company Apparatuses and methods for creating layered tape composite structures
EP3081370B1 (en) 2015-04-15 2018-01-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A composite radius filler for filling a void space in a skin-stiffener transition assembly
GB201507519D0 (en) * 2015-05-01 2015-06-17 Vestas Wind Sys As Reinforcing Structure for a Wind Turbine Blade
US9463864B1 (en) 2015-07-28 2016-10-11 The Boeing Company Radius filler containing vertical ply stacks and thin plies
US20170029577A1 (en) * 2015-07-29 2017-02-02 The Boeing Company Noodle Comprised of a Matrix of Discontinuous Filaments
US20170036375A1 (en) * 2015-08-07 2017-02-09 Hexcel Corporation Multi-sectional composite tooling
CN106428510A (en) * 2015-08-07 2017-02-22 空中客车美国工程有限公司 Composite beam lateral layer sheet stacking
CN106428523A (en) * 2015-08-10 2017-02-22 空中客车美国工程有限公司 Longitudinal layer piece laying structural component of composite wing beam
US9809297B2 (en) * 2015-08-26 2017-11-07 The Boeing Company Structures containing stiffeners having transition portions
US9808988B2 (en) 2015-11-30 2017-11-07 The Boeing Company Carbon fiber reinforced plastic (CFRP) stringer termination softening with stacked CFRP noodle
US10001337B2 (en) 2016-01-14 2018-06-19 Proof Research, Inc. Composite multi-lobe projectile barrel
US10329030B2 (en) * 2016-03-04 2019-06-25 The Boeing Company Conductive radius filler system and method
US20180086429A1 (en) * 2016-09-28 2018-03-29 The Boeing Company Airfoil-Shaped Body Having Composite Base Skin with Integral Hat-Shaped Spar
US10046525B2 (en) 2016-09-30 2018-08-14 The Boeing Company Advanced variable radius laminated composite radius filler
US10562244B2 (en) 2017-01-23 2020-02-18 The Boeing Company Systems and methods for forming a composite part based on volume
US10421252B2 (en) 2017-02-06 2019-09-24 Schott Gemtron Corp. Thermally insulating glass laminates with a non-uniform coating layer and a plurality of sealed cavities of gas molecules
CN106945311A (en) * 2017-04-28 2017-07-14 成都联科航空技术有限公司 A kind of many beam box section co-curing shapings of composite make frock and manufacture craft with enhancement layer
US10569481B2 (en) * 2017-06-26 2020-02-25 General Electric Company Shaped composite ply layups and methods for shaping composite ply layups
WO2019020152A1 (en) * 2017-07-27 2019-01-31 Vestas Wind Systems A/S Web foot for a shear web
US10875625B2 (en) * 2017-08-23 2020-12-29 The Boeing Company Co-cured spar and stringer center wing box
JP6978957B2 (en) * 2018-02-13 2021-12-08 三菱重工業株式会社 Assembly manufacturing method, reinforcement members, and assembly
CN108407324B (en) * 2018-03-02 2020-07-03 沈阳飞机工业（集团）有限公司 Tool scheme for manufacturing net-size composite material
US10941665B2 (en) 2018-05-04 2021-03-09 General Electric Company Composite airfoil assembly for an interdigitated rotor
US10677075B2 (en) 2018-05-04 2020-06-09 General Electric Company Composite airfoil assembly for an interdigitated rotor
US11966671B2 (en) * 2018-12-03 2024-04-23 The Boeing Company Method for determining noodle and interface residual stresses and properties under hygrothermal-mechanical loadings
US11325688B2 (en) 2019-05-09 2022-05-10 The Boeing Company Composite stringer and methods for forming a composite stringer
US10857751B2 (en) 2019-05-09 2020-12-08 The Boeing Company Composite stringer and methods for forming a composite stringer
US10913215B2 (en) 2019-05-09 2021-02-09 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10919256B2 (en) 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US11325689B2 (en) 2019-05-09 2022-05-10 The Boeing Company Composite stringer and methods for forming a composite stringer
US10919260B2 (en) 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US11242127B2 (en) 2020-04-22 2022-02-08 The Boeing Company Composite stringer assembly and methods for transmitting a load through a composite stringer assembly
US11156110B1 (en) 2020-08-04 2021-10-26 General Electric Company Rotor assembly for a turbine section of a gas turbine engine
CN112477203A (en) * 2020-10-22 2021-03-12 中国航空制造技术研究院 Pre-setting method for filling core material of integrally-formed composite material structure
CN112406134A (en) * 2020-10-29 2021-02-26 中国商用飞机有限责任公司北京民用飞机技术研究中心 Formed composite stringer prepreg twisting strip module and preparation method thereof
US11725519B2 (en) 2021-03-01 2023-08-15 Raytheon Technologies Corporation Platform for an airfoil of a gas turbine engine
US11655719B2 (en) 2021-04-16 2023-05-23 General Electric Company Airfoil assembly
CN113044203B (en) * 2021-04-21 2023-11-21 中国商用飞机有限责任公司北京民用飞机技术研究中心 Sacrificial layer for aircraft and paving method
JP7183350B1 (en) * 2021-07-14 2022-12-05 三菱重工業株式会社 Composite material structure and method for manufacturing composite material structure

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US112A (en) * 1837-01-21 Saddle for removing- the sick and for other purposes
US428A (en) * 1837-10-18 Improveivient in the process of separating and removing the bitterings from the kettles
US2124668A (en) * 1935-03-27 1938-07-26 Dayton Rubber Mfg Co Belt
US2796911A (en) * 1952-12-05 1957-06-25 Dayton Rubber Company Method of manufacturing belts
US4331723A (en) * 1980-11-05 1982-05-25 The Boeing Company Advanced composite
US4789594A (en) 1987-04-15 1988-12-06 The Boeing Company Method of forming composite radius fillers
DE19537663A1 (en) 1995-10-10 1997-04-17 Pott Richard 45 DEG reinforcing fiber scrim, fixed by means of adhesive threads, as well as method and device for producing the same
US5843355A (en) * 1996-01-24 1998-12-01 The Boeing Company Method for molding a thermoplastic composite sine wave spar structure
US5789061A (en) * 1996-02-13 1998-08-04 Foster-Miller, Inc. Stiffener reinforced assembly and method of manufacturing same
US5833786A (en) 1996-05-16 1998-11-10 The Boeing Company Titanium radius filler for use in composite interfaces
US5639535A (en) 1996-06-06 1997-06-17 The Boeing Company Composite interleaving for composite interfaces
EP1261787A2 (en) * 2000-02-25 2002-12-04 The Boeing Company Laminated composite radius filler

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