GB2160552A - Process for the production of carbon fibre-reinforced elastomer bodies - Google Patents

Process for the production of carbon fibre-reinforced elastomer bodies Download PDF

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Publication number
GB2160552A
GB2160552A GB08514768A GB8514768A GB2160552A GB 2160552 A GB2160552 A GB 2160552A GB 08514768 A GB08514768 A GB 08514768A GB 8514768 A GB8514768 A GB 8514768A GB 2160552 A GB2160552 A GB 2160552A
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United Kingdom
Prior art keywords
fibres
laminar
fibre
production
chopped
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.)
Granted
Application number
GB08514768A
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GB8514768D0 (en
GB2160552B (en
Inventor
Reiner Bode
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Sigri GmbH
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Sigri GmbH
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Filing date
Publication date
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Publication of GB8514768D0 publication Critical patent/GB8514768D0/en
Publication of GB2160552A publication Critical patent/GB2160552A/en
Application granted granted Critical
Publication of GB2160552B publication Critical patent/GB2160552B/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D69/00Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
    • F16D69/02Composition of linings ; Methods of manufacturing
    • F16D69/025Compositions based on an organic binder
    • F16D69/026Compositions based on an organic binder containing fibres
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K3/00Materials not provided for elsewhere
    • C09K3/10Materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K3/1025Materials in mouldable or extrudable form for sealing or packing joints or covers characterised by non-chemical features of one or more of its constituents
    • C09K3/1028Fibres
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/02Inorganic compounds
    • C09K2200/0204Elements
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/02Inorganic compounds
    • C09K2200/0204Elements
    • C09K2200/0208Carbon
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/02Inorganic compounds
    • C09K2200/0239Oxides, hydroxides, carbonates
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/02Inorganic compounds
    • C09K2200/0243Silica-rich compounds, e.g. silicates, cement, glass
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/02Inorganic compounds
    • C09K2200/0243Silica-rich compounds, e.g. silicates, cement, glass
    • C09K2200/0252Clays
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/02Inorganic compounds
    • C09K2200/0278Fibres
    • C09K2200/0282Carbon fibres
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/06Macromolecular organic compounds, e.g. prepolymers
    • C09K2200/0607Rubber or rubber derivatives
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/06Macromolecular organic compounds, e.g. prepolymers
    • C09K2200/0642Copolymers containing at least three different monomers
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K2200/00Chemical nature of materials in mouldable or extrudable form for sealing or packing joints or covers
    • C09K2200/06Macromolecular organic compounds, e.g. prepolymers
    • C09K2200/0645Macromolecular organic compounds, e.g. prepolymers obtained otherwise than by reactions involving carbon-to-carbon unsaturated bonds
    • C09K2200/067Condensation polymers of aldehydes or ketones

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
  • Reinforced Plastic Materials (AREA)
  • Braking Arrangements (AREA)

Abstract

In the production of laminar elastomer bodies which contain carbon fibres as reinforcing components, carbon fibre multifilament yarn is coated with a latex dispersion and, after drying, is chopped up into pieces which are whirled to form a loose fibre feed. The coated fibres do not break up on incorporation in a elastomer matrix and adhere to it well. The thus produced reinforced laminar elastomer bodies may be used in manufacture of flat seals, brake and clutch linings.

Description

SPECIFICATION Process for the production of carbon fibre-reinforced elastomer bodies This invention relates to a process for the production of laminar elastomer bodies reinforced with carbon fibres.
The carbon fibres produced almost exclusively by pyrolysis of polymers present in fibre form are used predominantly as reinforcement for synthetic resins, for example epoxy, polyester and polyamide resins.
Carbon fibre-reinforced synthetic resins have, for what are lower masses than metallic materials, a greater strength and rigidity and are correspondingly especially advantageous materials in vehicle construction, for example for spacecraft, aircraft and surface vehicles. Carbon fibres are likewise used as replacements for asbestos in seals and friction linings which chiefly contain an elastomer as matrix.
The most important starting fibres for carbon fibres are fibres formed of polyacrylonitrile and pitch. On heating the fibres to about 200 to 300 C, in general in an oxidising atmosphere, the starting materials are cross-linked or thermally stabilised while retaining the fibre form. The stabilised fibres are infusible and are denoted hereinafter, like the completely pyrolysed, exclusively carbon containing fibres, as carbon fibres. Cross-linking and pyrolysis produce temperature-resistant fibres with high strength and rigidity which, in principle, can be worked with like other textile fibres. At the same, the brittleness and the low breaking strength disadvantageously make their handling and working up to textiles increasingly difficult.
It is known that the capacity of carbon fibres for handling is improved by coating with sizing compositions. Differing from the coating usual even with other textile fibres, problems then arise with the use of sizing compositions if the coated fibres are employed in a matrix. Sizing compositions should at least not influence the bonding of the fibres with the matrix, improving this as much as possible, i.e. they must be compatible with the matrix in question. Apparently there are no sizing compositions which make possible a satisfactory working up of the carbon fibres in textiles and also are compatible with all the usual and technically necessary matrix systems. Correspondingly, sizing compositions have only become known, which fulfil the requirements for one or a few matrix resins.For example carbon fibres covered with diglycidyl ethers of bisphenol A bond well with an epoxy resin matrix, but insufficiently in a polybutylene terephthalate matrix (US-A 4 364 993). For specific thermoplastic matrix resins, such as polycarbonate or polyamide, coatings with polyurethane solutions and dispersions should be of advantage (DE-A-33 02 012). These sizing compositions named by way of example, and others which have become known, are not suitable however for bonding carbon fibres in an elastomer matrix. With laminar elastomer bodies, which can be used as seals, clutch and brake linings, carbon fibres there employed as reinforcing material are not as a rule distributed and bonded uniformly in the elastomer matrix, so that the properties of the products will only correspond partially and sometimes not at all to the requirements imposed by the intended use.
According to the present invention, there is provided a process for the production of a laminar elastomer body reinforced with carbon fibres, in which a) carbon multifilament yarn with at least 40,000 filaments is sized with a latex dispersion, the coated yarn is dried, chopped up into 0.5 to 20 mm long pieces and a feed is formed from the chopped up fibres by whirling them in a current of air, and b) the fibre feed is mixed with an elastomer composition and the mixture is rolled out to a laminar form.
This invention represents an improvement over prior art and processes for the production of laminar structures from carbon fibre-containing elastomers, especially the handling of the carbon fibres, under the conditions prevailing in the production of the composite body, in that the numbr of fibre breakages is reduced, and the fibres are distributed uniformly in the elastomer matrix and strongly bound therein. The product obtained after the rolling out stage is suitable for working up to form seals, brake or clutch linings.
When carrying out the invention, it is necessary firstly to coat the carbon fibres with a sizing composition compatible with the matrix and then to bring the coated fibres into the form of a loose feed. The sizing of fibres formed of rayon, polyamides and, after a special pre-treatment, even of polyesters and arylamides, with latex dispersions and the working-in of the coated fibres into elastomers and the improved bonding of such treated fibres in the elastomer matrix is known as such. However on account of the basically different condition of the surface of carbon fibres, the man skilled in the art could not expect that carbon fibres coated with latex behave similarly in admixture with elastomers and in particular that the coated brittle fibres are not broken up on working into the elastomer materials and destroyed.The effect is however only achieved if the coated carbon fibres are whirled in a current of air to form a fibre feed. Without the formation of a loose feed, there is also no success in distributing the fibres uniformly in the elastomer matrix.
The carbon fibres are coated with an aqueous latex dispersion, preferably with such dispersion containing additionally a butadiene-styrene-vinylpyridine copolymer, with which the bonding effect is somewhat better. It is likewise of advantage to add to the dispersion a resorcinol-formaldehyde precondensate which contains these substances approximately in a ratio of 10:1 to 2:1. The precondensate content in the dispersion should not amount to more than 10% by weight, since with higher contents the filaments of the yarn can stick to one another. Amounts of precondensate in the dispersion less than 2% by weight are generally insufficient.In accordance with current nomenclature, what is understood by the term "elastomer" are natural and synthetic materials whose glass transition temperature is less than O"C and less than the use temperature; such elastomers are typically natural and synthetic rubber. The carbon fibre yarn used for the reinforcement of the elastomer - including yarn formed of thermally stabilised fibres - should contain at least 40,000 filaments, since a uniform distribution is not achieved with yarns of smaller filament count. The yarns are conveniently drawn through a trough filled with the latex dispersion and for drying, through a drying channel or furnace and the coated yarns are chopped up into pieces 0.5 to 20 mm in length. For cutting up of the yarn, basically any tools used for the production of short cut fibres are suitable, for example cutting bars or rotating knives.The fibre pieces are then whirled in a current of air and a fibre feed whose bulk density amounts advantageously to 20 to 200 gil is separated off in a filter or cylcone. The length of the fibre pieces and the density of the fibre feed are determined in each case according to the use for the fibre reinforced elastomer material and can be determined by simple preliminary experiments. The length of the fibres contained in the fibre feed preferably amounts to approximately 1 to 20 mm and the bulk density preferably is 20 to 200 girl. The fibre feed is incorporated in the elastomer matrix with the aid of the usual rotary mixer and the mixture is rolled out to a laminar shape.The fibre content is dependent on the intended use of the elastomer body, amounting to about 5 to 20% by weight for friction linings and to more than 20% by weight for seals.
The following Example illustrates the invention: Example A multifilament yarn formed of thermally stabilised polyacrylonitrile, with 320,000 filaments, a titre of 42 ktex and a density of 1.40 g/cm3 was coated with an aqueous latex dispersion which had the composition: Free water 61.5% by wt.
Ammonia 0.2% by wt.
Latex dispersion contain- 30.0% by wt. (Solids ing butadiene-styrene- content - 40%) vinylpyridine copolymer Resorcinol-formaldehyde 8.3% by wt. (Solids precondensate content - 30%) The dispersions containing the butadiene-styrene- vinylpyridine copolymer are commercially available products.
The multifilament yarn was drawn through a trough filled with the dispersion; the immersion time amounted to about 1 minute. The coated yarn was warmed at room temperature and in a drying channel to about 130 to 140"C, chopped up in a cutting mill into pieces of about 3 to 10 mm length and then whirled in a current of air. The fibre feed with a bulk density of about 50 gll was separated off in a cyclone, was incorporated in chloroprene rubber in a rotary mixer and fillers and vulcanisation agents were added to the mixture whose final composition was: Chloroprene rubber - 20% by wt.
Coated fibres - 18% by wt.
Iron oxide - 15% by wt.
Magnesium oxide - 15% by wt.
Talc - 15%bywt.
Calcium hydroxide - 10% by wt.
Graphite - 5% by wt.
Sulphur - 1% by wt.
Zinc oxide - 1% by wt.
The mixture was granulated and pressed by means of die presses at about 160"C and a pressure of 20 MPa to laminar discs which were post vulcanised by heating in a circulatory furnace to about 180 C.
The microscopic examination of the discs provided as friction lining for disc and drum brakes showed, with the major part of the thermally stabilised polyacrylonitrile fibres, no reduction of the fibre length on mixing and shaping of the elastomer material, uniform distribution of fibres in the matrix and very good fibre bonding. Correspondingiv, the variation in the wear measured on a test bench and in the braking effect (retardation) was small.

Claims (11)

1. A process for the production of a laminar elastomer body reinforced with carbon fibres, in which a) carbon multifilament yarn with at least 40,000 filaments is sized with a latex dispersion, the coated yarn is dried,chopped up into 0.5 to 20 mm long pieces and a feed is formed from the chopped up fibres by whirling them in a current of air, and b) the fibre feed is mixed with an elastomer composition and the mixture is rolled out to a laminar form.
2. A process according to claim 1, in which a latex dispersion containing additionally butadiene-styrene- vinylpyridine copolymer is used to coat the chopped yarn pieces.
3. A process according to claim 1 or 2, in which a latex dispersion additionally containing a resorcinol- formaldehyde precondensate is used to coat the chopped yarn pieces.
4. A process according to claims 3, wherein a dispersion with a precondensate content of 2 to 10% is used.
5. A process according to any one of claims 1 to 4, wherein the fibre feed which is formed has a bulk density of 20 to 200 g/l.
6. A process for the production of a laminar elastomer body, substantially as described in the foregoing Example.
7. A laminar elastomer body, whenever produced by the process claimed in any preceding claim.
8. A flat seal which is formed from a laminar elastomer body as claimed in claim 7.
9. A flat seal as claimed in claim 8, which has a fibre content of at least 20% by weight.
10. A friction lining which is formed from a laminar elastomer body as claimed in claim 7.
11. A friction lining as claimed in claim 10, which has a fibre content of from 5 to 20% by weight.
GB08514768A 1984-06-22 1985-06-11 Process for the production of carbon fibre-reinforced elastomer bodies Expired GB2160552B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843423163 DE3423163A1 (en) 1984-06-22 1984-06-22 METHOD FOR PRODUCING CARBON FIBER REINFORCED ELASTOMER BODIES

Publications (3)

Publication Number Publication Date
GB8514768D0 GB8514768D0 (en) 1985-07-10
GB2160552A true GB2160552A (en) 1985-12-24
GB2160552B GB2160552B (en) 1987-08-26

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GB08514768A Expired GB2160552B (en) 1984-06-22 1985-06-11 Process for the production of carbon fibre-reinforced elastomer bodies

Country Status (4)

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DE (1) DE3423163A1 (en)
FR (1) FR2566315B1 (en)
GB (1) GB2160552B (en)
IT (1) IT1186736B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0647793A1 (en) * 1993-10-06 1995-04-12 Avco Corporation Low cost, asbestos-free friction material
EP1813405A1 (en) * 2006-01-25 2007-08-01 The Goodyear Tire & Rubber Company Curing sleeve reinforced with chopped carbon fibers

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3718035A1 (en) * 1987-05-28 1988-12-15 Haendler & Natermann Process for exhaust air purification and solvent recovery
DE4314193C1 (en) * 1993-04-30 1994-05-26 Baedje K H Meteor Gummiwerke Safety switch with carbon fibre contacts - has contacts housed in elastomer tube produced by extrusion with parallel carbon fibre strips produced at the same time
DE10328373B4 (en) * 2003-06-24 2015-10-08 Continental Automotive Gmbh Piezoelectric component with tempering device and use of the component

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1275412A (en) * 1968-08-03 1972-05-24 Dunlop Holdings Ltd Reinforcing yarns or cords
GB1275258A (en) * 1968-08-03 1972-05-24 Dunlop Holdings Ltd Reinforcing materials
IT948673B (en) * 1971-02-25 1973-06-11 Yamashita M PROCEDURE FOR THE MANUFACTURE OF REINFORCED OBJECTS SYNTHETIC RESIN CABLES
JPS5333998B2 (en) * 1974-01-16 1978-09-18
US4364993A (en) * 1980-07-14 1982-12-21 Celanese Corporation Sized carbon fibers, and thermoplastic polyester based composite structures employing the same
JPS58126375A (en) * 1982-01-22 1983-07-27 東邦レーヨン株式会社 Carbon fiber and resin composition thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0647793A1 (en) * 1993-10-06 1995-04-12 Avco Corporation Low cost, asbestos-free friction material
EP1813405A1 (en) * 2006-01-25 2007-08-01 The Goodyear Tire & Rubber Company Curing sleeve reinforced with chopped carbon fibers

Also Published As

Publication number Publication date
DE3423163C2 (en) 1992-11-19
IT8521251A0 (en) 1985-06-21
GB8514768D0 (en) 1985-07-10
IT1186736B (en) 1987-12-16
GB2160552B (en) 1987-08-26
FR2566315A1 (en) 1985-12-27
FR2566315B1 (en) 1989-05-19
DE3423163A1 (en) 1986-02-27

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940611