NO20085080L - A processing line for vacuum bar assemblies for the production of fiber reinforced composites - Google Patents

A processing line for vacuum bar assemblies for the production of fiber reinforced composites

Info

Publication number
NO20085080L
NO20085080L NO20085080A NO20085080A NO20085080L NO 20085080 L NO20085080 L NO 20085080L NO 20085080 A NO20085080 A NO 20085080A NO 20085080 A NO20085080 A NO 20085080A NO 20085080 L NO20085080 L NO 20085080L
Authority
NO
Norway
Prior art keywords
production
fiber reinforced
processing line
reinforced composites
bar assemblies
Prior art date
Application number
NO20085080A
Other languages
Norwegian (no)
Other versions
NO330083B1 (en
Inventor
Bjorn Pettersen
Pal Francis Hansen
Original Assignee
Frec Technology As
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 Frec Technology As filed Critical Frec Technology As
Priority to NO20085080A priority Critical patent/NO330083B1/en
Priority to PCT/NO2009/000419 priority patent/WO2010064928A1/en
Priority to EP09830634.3A priority patent/EP2373475A4/en
Publication of NO20085080L publication Critical patent/NO20085080L/en
Publication of NO330083B1 publication Critical patent/NO330083B1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/0227Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using pressure vessels, e.g. autoclaves, vulcanising pans
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/544Details of vacuum bags, e.g. materials or shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0471Layered armour containing fibre- or fabric-reinforced layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • B29C2035/0822Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using IR radiation
NO20085080A 2008-12-04 2008-12-04 A processing line for vacuum bar assemblies for the production of fiber reinforced composites NO330083B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
NO20085080A NO330083B1 (en) 2008-12-04 2008-12-04 A processing line for vacuum bar assemblies for the production of fiber reinforced composites
PCT/NO2009/000419 WO2010064928A1 (en) 2008-12-04 2009-12-04 A processing line for vacuum bag frame assemblies for the manufacturing of fibre-reinforced composites
EP09830634.3A EP2373475A4 (en) 2008-12-04 2009-12-04 A processing line for vacuum bag frame assemblies for the manufacturing of fibre-reinforced composites

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NO20085080A NO330083B1 (en) 2008-12-04 2008-12-04 A processing line for vacuum bar assemblies for the production of fiber reinforced composites

Publications (2)

Publication Number Publication Date
NO20085080L true NO20085080L (en) 2010-06-07
NO330083B1 NO330083B1 (en) 2011-02-14

Family

ID=42233429

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20085080A NO330083B1 (en) 2008-12-04 2008-12-04 A processing line for vacuum bar assemblies for the production of fiber reinforced composites

Country Status (3)

Country Link
EP (1) EP2373475A4 (en)
NO (1) NO330083B1 (en)
WO (1) WO2010064928A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8985174B2 (en) 2011-08-26 2015-03-24 The Boeing Company Integrally stiffened, reusable vacuum bag and method of making the same

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4863540A (en) * 1987-08-28 1989-09-05 American Temporing, Inc Process for manufacturing architectural glass
US5026514A (en) * 1989-05-05 1991-06-25 Hauwiller Paul B Incremental forming of thermoplastic composites
US5238519A (en) * 1990-10-17 1993-08-24 United Solar Systems Corporation Solar cell lamination apparatus
US5589016A (en) * 1994-04-29 1996-12-31 The Boeing Company Prescored foam for panel fabrication
US6149856A (en) * 1998-11-13 2000-11-21 Anvik Corporation Ultraviolet-based, large-area scanning system for photothermal processing of composite structures
US7326044B2 (en) * 2003-05-05 2008-02-05 Ortho-Active Holdings Inc. Rapid thermoform pressure forming process and apparatus
US7842209B2 (en) * 2006-02-21 2010-11-30 The Boeing Company Vacuum debulk and radiation cure method
ITTO20060477A1 (en) * 2006-06-28 2007-12-29 Alenia Aeronautica Spa METHOD, SYSTEM AND EQUIPMENT TO REALIZE COMPOSITE MATERIAL PARTS, IN PARTICULAR REINFORCED PARTS FOR AIRCRAFT FUSELAGE
US8409389B2 (en) * 2006-12-13 2013-04-02 The Boeing Company Method and apparatus for adhesive bond curing
US7803309B2 (en) * 2006-12-20 2010-09-28 The Boeing Company Infusion monitoring system and method

Also Published As

Publication number Publication date
EP2373475A1 (en) 2011-10-12
NO330083B1 (en) 2011-02-14
EP2373475A4 (en) 2016-10-12
WO2010064928A1 (en) 2010-06-10

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