CN105358315B - 热塑性夹层结构 - Google Patents

热塑性夹层结构 Download PDF

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Publication number
CN105358315B
CN105358315B CN201480038863.6A CN201480038863A CN105358315B CN 105358315 B CN105358315 B CN 105358315B CN 201480038863 A CN201480038863 A CN 201480038863A CN 105358315 B CN105358315 B CN 105358315B
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CN
China
Prior art keywords
thermoplastic
mold
consolidation
layer
core layer
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.)
Active
Application number
CN201480038863.6A
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English (en)
Chinese (zh)
Other versions
CN105358315A (zh
Inventor
M·R·马森
J·L·马尔考
A·W·巴特尔
J·B·莫泽
B·I·里昂
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Boeing Co
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Boeing Co
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Publication date
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Publication of CN105358315A publication Critical patent/CN105358315A/zh
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Classifications

    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/52—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles soluble or fusible
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • 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
    • B29D24/00—Producing articles with hollow walls
    • 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
    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • B29C2035/0811—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using induction
    • 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
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/004—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having vertical or oblique ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2101/00—Use of unspecified macromolecular compounds as moulding material
    • B29K2101/12—Thermoplastic materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3085—Wings
    • 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)
  • Health & Medical Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Toxicology (AREA)
  • Electromagnetism (AREA)
  • Thermal Sciences (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
CN201480038863.6A 2013-07-09 2014-06-16 热塑性夹层结构 Active CN105358315B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/937,269 US9358703B2 (en) 2013-07-09 2013-07-09 Thermoplastic sandwich structures
US13/937,269 2013-07-09
PCT/US2014/042467 WO2015006016A1 (en) 2013-07-09 2014-06-16 Thermoplastic sandwich structures

Publications (2)

Publication Number Publication Date
CN105358315A CN105358315A (zh) 2016-02-24
CN105358315B true CN105358315B (zh) 2017-08-08

Family

ID=51257558

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201480038863.6A Active CN105358315B (zh) 2013-07-09 2014-06-16 热塑性夹层结构

Country Status (7)

Country Link
US (1) US9358703B2 (enExample)
JP (1) JP6353042B2 (enExample)
CN (1) CN105358315B (enExample)
BR (1) BR112015029835B1 (enExample)
CA (1) CA2852873A1 (enExample)
RU (1) RU2667543C2 (enExample)
WO (1) WO2015006016A1 (enExample)

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US9469087B2 (en) 2013-07-09 2016-10-18 The Boeing Company Thermoplastic and titanium sandwich structures
US10538050B2 (en) 2015-10-12 2020-01-21 C&D Zodiac, Inc. Aircraft panel assembly with reinforcement layers
US10131416B2 (en) 2015-10-12 2018-11-20 C&D Zodiac, Inc. Integrally molded attachment members for panels for aircraft liners
FR3051135B1 (fr) * 2016-05-10 2019-05-31 Roctool Dispositif et procede pour le moulage et la consolidation d’une preforme textile
US10743377B2 (en) * 2017-12-14 2020-08-11 The Boeing Company Induction heating cells comprising tensioning members with non-magnetic metal cores
DE102018127807A1 (de) * 2018-04-26 2019-10-31 Hanon Systems Vorrichtung und Verfahren zum thermischen Fügen insbesondere eines Wärmeübertragers für ein Kraftfahrzeug
DE102018132799B4 (de) * 2018-12-19 2021-01-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Formwerkzeug zur Herstellung eines profilversteiften Faserverbundbauteils
US11485096B2 (en) * 2019-05-17 2022-11-01 The Boeing Company Method and system for manufacturing composite structures using a magnesium bladder
US11572644B2 (en) * 2019-06-28 2023-02-07 The Boeing Company Pulsed-pressure consolidation of braided preforms for composite parts
US11383461B2 (en) 2019-12-18 2022-07-12 The Boeing Company Method and apparatus for forming a composite fuselage structure
US11541579B2 (en) * 2019-12-18 2023-01-03 The Boeing Company Method and apparatus for forming a composite fuselage structure
US11987389B2 (en) * 2019-12-18 2024-05-21 The Boeing Company Method and apparatus for forming a composite fuselage structure
US11498293B2 (en) 2019-12-18 2022-11-15 The Boeing Company Method and apparatus for forming a composite fuselage structure
EP4129607A4 (en) * 2020-03-26 2023-09-13 Mitsubishi Chemical Corporation METHOD FOR MANUFACTURING A FIBER-REINFORCED RESIN PRODUCT, AND CORE
DE102020134901A1 (de) * 2020-12-23 2022-06-23 Airbus Operations Gmbh Formkern zur Herstellung eines Bauteils aus Faserverbundmaterial
US12157572B2 (en) 2021-08-31 2024-12-03 The Boeing Company Method of making a control surface
CN114670378A (zh) * 2022-04-07 2022-06-28 内蒙古工业大学 可调节固体火箭发动机硫化脱模装置
US11987353B2 (en) * 2022-04-19 2024-05-21 The Boeing Company Thermoplastic skin panels, torque box and method

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US5587098A (en) * 1991-04-05 1996-12-24 The Boeing Company Joining large structures using localized induction heating
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Also Published As

Publication number Publication date
BR112015029835A2 (pt) 2017-07-25
BR112015029835B1 (pt) 2020-11-17
CA2852873A1 (en) 2015-03-09
WO2015006016A1 (en) 2015-01-15
JP6353042B2 (ja) 2018-07-04
RU2015144566A3 (enExample) 2018-03-28
RU2015144566A (ru) 2017-08-14
RU2667543C2 (ru) 2018-09-21
JP2016529133A (ja) 2016-09-23
US20150013883A1 (en) 2015-01-15
CN105358315A (zh) 2016-02-24
US9358703B2 (en) 2016-06-07

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