CN105314090B - 织物置于套内的单向填面 - Google Patents

织物置于套内的单向填面 Download PDF

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Publication number
CN105314090B
CN105314090B CN201510156139.XA CN201510156139A CN105314090B CN 105314090 B CN105314090 B CN 105314090B CN 201510156139 A CN201510156139 A CN 201510156139A CN 105314090 B CN105314090 B CN 105314090B
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China
Prior art keywords
core
strip
strips
length
prepreg
Prior art date
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CN201510156139.XA
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English (en)
Chinese (zh)
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CN105314090A (zh
Inventor
J·扎弗斯
V·安德尤科夫
D·坎贝尔
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
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Boeing Co
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Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of CN105314090A publication Critical patent/CN105314090A/zh
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    • 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
    • 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
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/0076—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised in that the layers are not bonded on the totality of their surfaces
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/16—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
    • B32B37/18—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of discrete sheets or panels only
    • 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
    • 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
    • B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/07—Parts immersed or impregnated in a matrix
    • B32B2305/076—Prepregs
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
CN201510156139.XA 2014-07-25 2015-04-03 织物置于套内的单向填面 Active CN105314090B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/340,982 2014-07-25
US14/340,982 US9440414B2 (en) 2014-07-25 2014-07-25 Fabric jacketed unidirectional noodle

Publications (2)

Publication Number Publication Date
CN105314090A CN105314090A (zh) 2016-02-10
CN105314090B true CN105314090B (zh) 2020-08-11

Family

ID=53016532

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510156139.XA Active CN105314090B (zh) 2014-07-25 2015-04-03 织物置于套内的单向填面

Country Status (5)

Country Link
US (2) US9440414B2 (enExample)
EP (2) EP2977192B1 (enExample)
JP (1) JP6542021B2 (enExample)
CN (1) CN105314090B (enExample)
ES (1) ES2749216T3 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2975970B1 (fr) * 2011-05-30 2013-05-17 Aircelle Sa Ensemble pour une nacelle d'aeronef
US10072632B2 (en) * 2015-06-30 2018-09-11 General Electric Company Spar cap for a wind turbine rotor blade formed from pre-cured laminate plates of varying thicknesses
EP3658767B1 (en) * 2017-07-27 2022-12-14 Vestas Wind Systems A/S Web foot for a shear web
US10717239B2 (en) * 2017-09-28 2020-07-21 The Boeing Company Fabrication of gap fillers for composite parts that exhibit varying radii of curvature
CN107901454A (zh) * 2017-12-28 2018-04-13 振石集团华美新材料有限公司 一种用于多层织物拉挤工艺的预成型设备及其预成型方法
US10800128B2 (en) 2018-01-24 2020-10-13 General Electric Company Composite components having T or L-joints and methods for forming same
JP6978957B2 (ja) * 2018-02-13 2021-12-08 三菱重工業株式会社 組立体の製造方法、補強部材、及び組立体
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

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4331723A (en) * 1980-11-05 1982-05-25 The Boeing Company Advanced composite
JPH0436905Y2 (enExample) * 1987-02-03 1992-08-31
WO1996018494A1 (en) 1994-12-13 1996-06-20 Dow-United Technologies Composite Products, Inc. Shaped unidirectional fiber filler
US6562436B2 (en) 2000-02-25 2003-05-13 The Boeing Company Laminated composite radius filler
DE102007018052A1 (de) * 2007-04-17 2008-10-23 Airbus Deutschland Gmbh Pultrusionsverfahren zur Herstellung eines endlosen Profils
US8540833B2 (en) 2008-05-16 2013-09-24 The Boeing Company Reinforced stiffeners and method for making the same
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 (ja) * 2011-08-10 2016-10-19 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 複合ストリンガの高能力プルオフのための垂直積層ヌードル
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
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

Also Published As

Publication number Publication date
EP3482923A1 (en) 2019-05-15
US20160325525A1 (en) 2016-11-10
EP2977192B1 (en) 2019-07-10
ES2749216T3 (es) 2020-03-19
JP2016030440A (ja) 2016-03-07
EP2977192A1 (en) 2016-01-27
CN105314090A (zh) 2016-02-10
US9440414B2 (en) 2016-09-13
US9802385B2 (en) 2017-10-31
EP3482923B1 (en) 2022-12-07
US20160023431A1 (en) 2016-01-28
JP6542021B2 (ja) 2019-07-10

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