GB2099365A - Process for the production of friction discs - Google Patents
Process for the production of friction discs Download PDFInfo
- Publication number
- GB2099365A GB2099365A GB8215631A GB8215631A GB2099365A GB 2099365 A GB2099365 A GB 2099365A GB 8215631 A GB8215631 A GB 8215631A GB 8215631 A GB8215631 A GB 8215631A GB 2099365 A GB2099365 A GB 2099365A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fibres
- winding
- process according
- strip
- layers
- 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
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/83—Carbon fibres in a carbon matrix
-
- 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
- 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
- B32B5/06—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 a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
- D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
- D04H1/44—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling
- D04H1/46—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres
- D04H1/498—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by needling or like operations to cause entanglement of fibres entanglement of layered webs
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H18/00—Needling machines
- D04H18/02—Needling machines with needles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D65/12—Discs; Drums for disc brakes
- F16D65/125—Discs; Drums for disc brakes characterised by the material used for the disc body
- F16D65/126—Discs; Drums for disc brakes characterised by the material used for the disc body the material being of low mechanical strength, e.g. carbon, beryllium; Torque transmitting members therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Compositions of linings; Methods of manufacturing
- F16D69/023—Composite materials containing carbon and carbon fibres or fibres made of carbonizable material
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/514—Oriented
-
- 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
- B32B2475/00—Frictional elements
Abstract
Friction discs of carbon-carbon composite materials are produced by winding a strip of material 8 composed of fibres around a cylindrical mandrel 13, and carrying out one or both of the following operations: (a) at the time as the strip of material 8 composed of fibres is wound around the mandrel 13, it is subjected to a radial needling operation, the strip then comprising two or more layers of fibres of different orientations and lengths according to the layers formed, and (b) the winding produced is radially compressed by 12a, 12b so as to produce circumferential undulations in all the layers forming the winding 8. The invention is particularly intended for the manufacture of brake and clutch discs. <IMAGE>
Description
SPECIFICATION
Process for the production of friction discs
The present invention concerns the production of friction discs of carbon-carbon composite materials, which are particuiarly intended for use as friction members having structural strength in brakes or clutches comprising one or more discs associated with other discs or with pads or shoes.
It is known that a member comprising carboncarbon composite material may be produced by preparing a fibrous substrate of carbon or carbon precursor material which is carbonised, then followed by densification of the substrate. This operation results in a member comprising carbon fibres embedded in a carbonaceous "matrix".
Densification of the substrate may be effected for example by chemical deposit of carbon in the vapour phase, by means of one or more cycles comprising liquid impregnation of carbonisable materials, carbonisation and graphitation, or by a combination of those two methods.
It is also known that the properties of the member that is finally produced largely depend on the arrangement of the initial fibrous substrate.
In accordance with the present invention, there is provided a process for the production of friction discs of carbon-carbon composite material by winding a strip of material composed of fibres around a cylindrical mandrel, in which at least one of the following operations is carried out: (a) at the same time as the strip of material composed of fibres is wound around the mandrel, it is subjected to a radial needling operation, the strip then comprising two or more layers of fibres of different orientations and lengths according to the layers formed, and (b) the winding produced is radially compressed so as to produce circumferential undulations in all the layers forming the winding.
The present invention can be carried out easily and economically to produce, after convention carbonisation and/or densification, friction discs with a good performance.
The roll produced after one or other or both operations is optionally carbonised, if the fibres used comprise a carbon precursor material, and then cut up perpendicularly to its axis to form a large number of disc members which form the substrate of a plurality of discs, if the width of the strip is sufficient for that purpose.
The roll or the disc members is/are then subjected to a densification treatment, either by putting them in a furnace so that they receive, at a temperature of 1000"C, a chemical deposit of carbon in the vapour phase, which forms the matrix of the material, or by impregnating them at least once with liquid hydrocarbons such as coal tar, followed by carbonisation and graphitation.
This second possible process, which is intended if necessary to remove local porosity in the substrate or to reduce the total period of time required for producing the matrix, may be effected between a third and four-fifths of production of the finai density by chemical vapour-phase deposition.
The densified discs are then subjected to a heat treatment at a temperature of from 1600 to 2500 C, depending on the use to which they are to be put.
The brake discs produced in accordance with the present invention can have the following advantages:
no wastage of fibres during production of the disc;
speed and ease of deposit of the matrix, due to the form of the substrate;
ease of production of the substrate on an industrial scale;
very good mechanical strength in respect of braking couple;
good resistance to wear, due to the generally highly inclined orientation of the fibres with respect to the friction surfaces;
excellent dimensional stability of the disc during the heating effect caused by braking;
in regard to the disc, the condition of parellelism of the faces is retained because of the zero coefficient of expansion in respect of thickness;
in regard to the fibres or groups of fibres, there cannot be any local geometrical change in the surface that could promote the occurrence of hot spots;;
very good resistance to radial delamination due to the radical needling action and/orthe undulations, those two processes separately or in combination reducing the adverse effects of the polar anisotropy of the winding;
a very high level of compression and tensile strength in the axial direction of the disc; and
the heat due to the friction effect can be very easily removed towards the interior of the disc.
It should be noted that the above-indicated process includes a number of variations, which are also part of the present invention.
In the accompanying drawings, which are given to illustrate but not to limit the invention,
Figure lisa diagrammatic view of the windingneedling operation,
Figure 2 is a diagrammatic view of a preferred type of circumferential undulation,
Figures 3A and 3B are diagrammatic view of means for producing the circumferential undulations shown in Figure 2, and
Figure 4 shows the operation of winding a particular strip of fibres.
Referring to Figure 1, four layers of fibres are wound simultaneously around a cylindrical mandrel 1. The mat layers 2a and 2b are formed by short fibres (for example from 3 to 5 cm) which are disposed randomly in the plane of the layer.
The layers 3 and 4 are formed by unidirectional fibres 5 which are possibly disposed on a thin plastic carrier which can be removed by heat, and which are oriented, with respect to the axis of the mandrel:
- towards the right, in respect of the layer 3, and
- towards the left, in respect of the layer 4.
The angles at which the fibres are oriented may be for example between 30 and 60 , according to circumstances. Figure 1 shows the angles as being equal at 45D The mandrel 1 rotates in the direction indicated by arrow 9.
While the winding 8 is progressively being formed, a needling bar 6 provided with a large number of needles 7 continuaily alternatively perforates the winding 8. By virtue of the projections or spurs on the needies, the result of the needling operation isto pull out shortfibres which are initially disposed on the mat layers comprising short fibres 2a and 2b, and to arrange them in radial directions with respect to the winding 8.
When the needled winding S is sufficiently large in diameter, the mandrel 1 is removed.
The winding 8 enjoys very good cohesion and can be handled without having to take special precautions. It is advantageous for the winding 8 to be made from layers of fibres of carbon precursor material such as cross-linked polyacrylonitrile. This results in the winding being less fragile, which permits both the needling operation and the radial compression operation. In that case, the substrate is subjected to an additional carbonisation operation.
Figure 2 shows undulations in the layers at the inside periphery pf of the radially compressed winding, which are as marked as the undulations in the layers at the outside periphery Pf. In order to produce that type of undulation, it will be seen that it is essential in the radial compression operation substantially and simultaneously to reduce the diameters of the outside and inside peripheries Pi and p ofthe winding.
Figure 2 also shows that there are real undulations around any circumference of the winding, thereby forming notches or recesses which are disposed in a staggered arrangement relative to each other, atthe inside and outside peripheries.
Referring now to Figures 3A and 3B, the needled winding 8 is disposed within a rigid cylinder 10, coaxially therewith (axis 11). Radial compression sector members 12a and 12b are disposed between the cylinder 10 and the winding 8. The longitudinal direction of the sector members is and remains
parallel to the axis of the cylinder throughout the compression operation. The sector members are identical in length to the winding 8 and the cylinder
10.
A radial force and a radial movement are imparted to the sector members 12a and 12b in such a way that the sector members 12b are displaced radially at a higher speed than the sector members 1 2a.
Disposed at the centre of the needled winding 8, coaxiallytherewith and with the cylinder 10, is a compressible cylindrical core member 13 which is of the same axial length as the members 10 and 8.
The core member 13 may either comprise an
elastomer or an assembly of mechanical compo
nents, but in both cases the diameter of the core
member must be reduced during the radial com
pression operation. At its periphery (and over its
entire axial length), the core member 13 has raised
surface portions 13a, the longitudinal direction of which is parallel to the axis of the core member 13.
There is a regular alternation as between sector
members 12b and raised surface portions 13a in the
angular space which is around the axis 11, thereby to
produce properly repetitive undulations such as those which can be seen in Figures 2 and 3B, in the radial compression operation.
The resulting winding with undulations is then cut up perpendicularly to its axis into ring or disc members which form substrates for discs and which are subjected to a densification treatment.
The discs which are finally produced, being provided with their notches or recesses, can be put to many uses. Mention may be made of the following:
when the disc is used as a rotor or rotary member, it will be driven in rotation by key or pin members which are fixed to the inside of an aircraft wheel rim, for example, by way of all or some of the notches formed by the undulations in the outside periphery of the disc, and
when the disc is used as a stator, it will be immobilised by means of key or pin members which are fixed to a non-rotating shaft, by means of all or some of the notches formed by undulations in the inside periphery of the disc.
A first alternative form in accordance with the invention concerns producing discs, the wound substrate of which is subjected only to the operations disclosed in Figure 1. Therefore, that substrate is not subjected to the operation of forming the undulations by radial compression as described with reference to Figures 2, 3A and 3B, but except for that step, the method of producing the discs is strictly the same.
A second alternative form according to the invention concerns the production of discs wherein the wound substrate is not subjected to the radial needling operation, but on the other hand is subjected to the operation of forming undulations by radial compression and all the operations described hereinbefore.
In this second alternative form of the process, referring to Figure 1, the substrate may comprise:
- either the succession of layers 2a, 3, 2b, 4 as described hereinbefore (but without being radially needled),
- or the succession of layers 3 and 4, the layers 2a and 2b thus being omitted,
- or a strip as illustrated in Figure 4.
In the single case of the strip shown in Figure 4, the substrate is made disc by disc and not by long cylinder members which can subsequently be cut up into discs, as in all the other embodiments.
The strip illustrated in Figure 4 comprises a warp 14, the width b of which is only two thirds of the total width a of the disc. The weft 15 of the strip on the other hand is of a width corresponding to the full width a of the finished disc.
Thus, the friction surfaces of the disc will be subjected to wear, in braking operations, in regard to a disc thickness which has only weft threads which are therefore perpendicular to the disc surfaces. In order to enhance the final operational stability of the surfaces of the disc, the weft threads are notwoven with warp threads but are simply assembled by two sets of stitches which are produced by machine
parallel to the longitudinal axis of the strip.
Athird alternative form in accordance with the
invention is concerned with the production of discs from a substrate which is wound and radially needled in a manner strictly in accordance with the description relating to Figure 1. The substrate is then placed in the equipment described with reference to
Figures 3A and 3B, except that the equipment is slightly modified: all the parts outside the winding (cylinder member 10 and section members 12a and 12b) are unchanged, but the compressible core member 13 with the raised surface portions 13a is replaced by an incompressible core member, the diameter of which is identical to that of the mandrel 1 shown in Figure 1.The radial compression operation is then performed, which has the effect of producing undulations which are clearly marked in the peripheral regions of the winding 8, and undulations which are increasingly less marked at diameters which progressively move towards the diameter of the mandrel 1.
This third embodiment of the process of the invention therefore makes use of a property of radial compressibility of the wound needled substrate, which makes it possible to reduce and form undulations in the initial outside periphery of the winding, without reducing or forming undulations in the inside periphery.
Such radial compressibility of the substrate will be enhanced (see Figure 1) if on the one hand the thickness of the short4ibre layers 2a and 2b is increased and if on the other hand no circumferential tension is applied to the layers of fibre during the winding and needling operations.
The attraction of the alternative forms of the invention may be that they permit a saving in production, if use of the discs is limited in each of the cases in question, to particular situations of use.
Claims (17)
1. A process for the production of friction discs of carbon-carbon composite material by winding a strip of material composed of fibres around a cylindrical mandrel, in which at least one of the following operations is carried out: (a) at the same time as the strip of material composed of fibres is wound around the mandrel, it is subjected to a radial needling operation, the strip then comprising two or more layers of fibres of different orientations and lengths according to the layers formed, and (b) the winding produced is radially compressed so as to produce circumferential undulations in all the layers forming the winding.
2. A process according to Claim 1 in which, in order to produce the circumferential undulations, a cylindrical core member of the same length as the winding is introduced without clearance into the winding and coaxially with it, and sector members that are alternately long and short are applied to the periphery of the winding and subjected to a centripetal radial force.
3. A process according to Claim 2 in which the cylindrical core member comprises a compressible material which thus permits of simultaneous reduction in its internal and external diameters when the winding is radially compressed.
4. A process according to Claim 3 in which the cylindrical core member carries raised surface portions.
5. A process according to Claim 2,3 or 4 in which the circumferential undulations are so formed that they produce notches disposed in a staggered arrangement relative to one another on the external and internal peripheries of the winding such that each notch of a periphery is disposed facing the middle of the arc between two successive notches of the other periphery.
6. A process according to Claim 5 in which the notches are distributed and shaped such that at least some of them serve as key-way grooves.
7. A process according to Claim 2 in which the cylindrical core member comprises incompressible material.
8. A process according to any one of Claims 1 to 7 in which the strip of material composed of fibres is formed by four layers, viz.
(a) a layer of randomly disposed short fibres, (b) a layer of unidirectional fibres oriented in a direction inclined with respect to the axis of the mandrel, (c) another layer of short randomly disposed fibres, and (d) a layer of unidirectional fibres oriented in another inclined direction with respect to the axis of the mandrel,
the four layers being wound simultaneously and needled during the same period and the winding produced not being subjected to the radial compression operation.
9. A process according to any one of Claims 1 to 7 in which the strip of material composed of fibres is formed by four layers, viz.
(a) a layer of randomly disposed short fibres, (b) a layer of unidirectional fibres oriented in a direction inclined with respect to the axis of the mandrel, (c) another layer of short randomly disposed fibres, and (d) a layer of unidirectional fibres oriented in another inclined direction with respect to the axis of the mandrel,
the four layers being wound simultaneously and then being subjected to the radial compression operation.
10. A process according to any one of Claims 1 to 7 in which the strip of material composed of fibres is formed by layers of unidirectional fibres that are not needled, and the resulting winding is then subjected to the radial compression operation.
11. A process according to any one of Claims 8 to 10 in which the fibres comprise carbon precursor material.
12. A process according to Claim 11 in which the material is cross-linked polyacrylonitrile.
13. A process according to any one of Claims 8 to 10 in which the winding produced is cut into disc members and subsequently subjected to densification.
14. A process according to Claim 11 or 12 in which the winding produced is carbonised and then cut into disc members and subsequently subjected to densification.
15. A process according to any one of Claims 1 to 7 in which the strip of material composed of fibres is formed by a strip of carbon threads, the warp width of which is less than that of the carbon thread strip and the weft width of which is equal to that of the carbon thread strip, the said carbon thread strip not being needled and the winding formed by it then being subjected to the radial compression operation and subsequently to densification.
16. A process according to Claim 15 in which the warp and weft threads of the carbon thread strip are straight and intersect one another at right angles.
17. A process according to Claim 15in which the warp and weft threads are joined by stitching.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8110881A FR2506672A1 (en) | 1981-06-02 | 1981-06-02 | METHOD FOR MANUFACTURING FRICTION DISCS |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2099365A true GB2099365A (en) | 1982-12-08 |
GB2099365B GB2099365B (en) | 1984-11-28 |
Family
ID=9259094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8215631A Expired GB2099365B (en) | 1981-06-02 | 1982-05-28 | Process for the production of friction discs |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS58643A (en) |
CA (1) | CA1198268A (en) |
DE (1) | DE3220306C2 (en) |
FR (1) | FR2506672A1 (en) |
GB (1) | GB2099365B (en) |
IT (1) | IT1151237B (en) |
NL (1) | NL181888C (en) |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0147297A2 (en) * | 1983-12-28 | 1985-07-03 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Process and apparatus for producing tridimensional rotational structures |
FR2587992A1 (en) * | 1985-10-02 | 1987-04-03 | Europ Propulsion | CARBON-CARBON COMPOSITE MATERIAL FOR FRICTION COMPONENTS, AND ITS APPLICATION TO BRAKING DEVICES |
US4790052A (en) * | 1983-12-28 | 1988-12-13 | Societe Europeenne De Propulsion | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
FR2619104A1 (en) * | 1987-08-05 | 1989-02-10 | Kobe Steel Ltd | PROCESS FOR THE PREPARATION OF CARBON-REINFORCED CARBON-BASED COMPOSITE MATERIAL AND CARBON-REINFORCED CARBON-BASED COMPOSITE MATERIAL |
GB2177345B (en) * | 1985-06-27 | 1989-07-12 | Europ Propulsion | Process for manufacturing three-dimensional structures of fibrous material |
EP0524052A1 (en) * | 1991-07-16 | 1993-01-20 | Centre Technique Industriel dit: INSTITUT TEXTILE DE FRANCE | Process and apparatus for manufacturing a non-woven structure and non-woven for use therein |
US5217770A (en) * | 1991-08-15 | 1993-06-08 | The B. F. Goodrich Company | Braided shaped filamentary structures and methods of making |
FR2696219A1 (en) * | 1992-09-30 | 1994-04-01 | Dunlop Ltd | Brake disc made of carbon composite material and stack of brake discs comprising this disc. |
US5504979A (en) * | 1994-07-25 | 1996-04-09 | The Bfgoodrich Company | Process for forming fibrous preform structures |
US5546880A (en) * | 1994-12-29 | 1996-08-20 | The Bf Goodrich Company | Annular filamentary structures and methods of making |
US5609707A (en) * | 1991-09-04 | 1997-03-11 | The B. F. Goodrich Company | Carbon fiber reinforced carbon/carbon composite and method of its manufacture |
US5662855A (en) * | 1994-05-17 | 1997-09-02 | The B.F. Goodrich Company | Method of making near net shaped fibrous structures |
FR2754031A1 (en) * | 1996-09-30 | 1998-04-03 | Carbone Ind | DEVELOPMENT OF FIBROUS PREFORMS FOR THE MANUFACTURE OF COMPOSITE MATERIAL BRAKE DISCS |
WO1998053218A1 (en) * | 1997-05-23 | 1998-11-26 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Solid construction friction unit, specially a brake disc with several friction bodies |
US5858890A (en) * | 1994-07-25 | 1999-01-12 | The B. F. Goodrich Company | Laminar fibrous structure having Z-fibers that penetrate a constant number of layers |
US5908792A (en) * | 1995-10-04 | 1999-06-01 | The B. F. Goodrich Company | Brake disk having a functional gradient Z-fiber distribution |
US6029327A (en) * | 1994-07-25 | 2000-02-29 | The B.F. Goodrich Company | Process for forming fibrous structures with predetermined Z-fiber distributions |
US6105223A (en) * | 1997-04-30 | 2000-08-22 | The B. F. Goodrich Company | Simplified process for making thick fibrous structures |
CN1078276C (en) * | 1995-06-19 | 2002-01-23 | 航空发动机的结构和研究公司 | Method and apparatus for making ring-shaped parts out of composite material, as well as preforms therefor |
US6405417B1 (en) | 1994-07-25 | 2002-06-18 | Goodrich Corporation | Process for forming fibrous structures with predetermined Z-fiber distributions |
WO2009063210A1 (en) * | 2007-11-16 | 2009-05-22 | Tom Lloyd Halstead | A method of manufacturing a fibrous structure and an apparatus therefor |
WO2012114061A1 (en) * | 2011-02-22 | 2012-08-30 | Marathon Belting Limited | A carbon or carbonizable fibrous structure and a method of manufacturing same |
US20170328429A1 (en) * | 2014-10-10 | 2017-11-16 | Petroceramics S.P.A. | Method for making brake discs in material reinforced with fibres and brake disc made with such method |
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Publication number | Priority date | Publication date | Assignee | Title |
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DE3343505A1 (en) * | 1983-12-01 | 1985-06-13 | Sachs Systemtechnik Gmbh, 8720 Schweinfurt | FRICTION DISC COUPLING |
FR2584107B1 (en) * | 1985-06-27 | 1988-07-01 | Europ Propulsion | METHOD FOR MANUFACTURING THREE-DIMENSIONAL REVOLUTION STRUCTURES BY NEEDLEING LAYERS OF FIBROUS MATERIAL AND MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS |
US5388320A (en) | 1987-01-27 | 1995-02-14 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5882781A (en) * | 1986-01-28 | 1999-03-16 | Aerospace Preforms Limited | Shaped fibrous fabric structure comprising multiple layers of fibrous material |
US5323523A (en) * | 1986-01-28 | 1994-06-28 | Aerospace Preforms Limited | Production of shaped filamentary structures |
FR2597798A1 (en) * | 1986-04-25 | 1987-10-30 | Elf France | DEVICE FOR COUPLING IN ROTATION OF A WHEEL HUB |
US5705264A (en) * | 1987-01-27 | 1998-01-06 | Aerpspace Preforms Limited | Production of shaped filamentary structures |
EP0484391B1 (en) * | 1989-07-25 | 1995-09-20 | Dunlop Limited | Manufacture of carbon fibre preform |
GB2250520B (en) * | 1989-07-25 | 1993-06-09 | Dunlop Ltd | Manufacture of carbon fibre preform |
JPH03194227A (en) * | 1990-10-26 | 1991-08-23 | Toho Rayon Co Ltd | Carbon brake |
JPH03194228A (en) * | 1990-10-26 | 1991-08-23 | Toho Rayon Co Ltd | Carbon brake with reinforced periphery |
CN1279550C (en) | 2001-10-12 | 2006-10-11 | 矢崎总业株式会社 | Wire recycling method |
CN103429422B (en) | 2011-01-12 | 2016-08-31 | 小利兰斯坦福大学理事会 | Composite lamainated structure and production and preparation method thereof |
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US3772115A (en) * | 1966-12-13 | 1973-11-13 | Carborundum Co | Process for producing reinforced carbon and graphite bodies |
US3552533A (en) * | 1968-10-01 | 1971-01-05 | Abex Corp | Carbonized friction article |
BE757208A (en) * | 1969-10-08 | 1971-04-07 | Monsanto Co | COMPLETELY CARBON COMPOSITE STRUCTURE |
US3712428A (en) * | 1970-06-22 | 1973-01-23 | Carborundum Co | Reinforced carbon bodies |
US3759353A (en) * | 1970-06-22 | 1973-09-18 | Carborundum Co | Disc brake containing reinforced carbon bodies |
US3897582A (en) * | 1970-08-21 | 1975-07-29 | Atlantic Res Corp | Braking elements |
GB1410090A (en) * | 1973-03-21 | 1975-10-15 | Atomic Energy Authority Uk | Reinforced carbon structures |
DE2722575A1 (en) * | 1976-05-18 | 1977-12-22 | Morganite Modmor Ltd | COAL-CHARCOAL COMPOSITE |
JPS5365549A (en) * | 1976-11-22 | 1978-06-12 | Akebono Brake Ind Co Ltd | A method to manufacture vehicle clutch facing |
AU517708B2 (en) * | 1978-01-12 | 1981-08-20 | Dunlop Limited | Carbon composite brake disc manufacture |
-
1981
- 1981-06-02 FR FR8110881A patent/FR2506672A1/en active Granted
-
1982
- 1982-05-13 NL NLAANVRAGE8202003,A patent/NL181888C/en not_active IP Right Cessation
- 1982-05-25 IT IT21473/82A patent/IT1151237B/en active
- 1982-05-28 DE DE3220306A patent/DE3220306C2/en not_active Expired
- 1982-05-28 JP JP57092072A patent/JPS58643A/en active Pending
- 1982-05-28 GB GB8215631A patent/GB2099365B/en not_active Expired
- 1982-06-01 CA CA000404180A patent/CA1198268A/en not_active Expired
Cited By (41)
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FR2557550A1 (en) * | 1983-12-28 | 1985-07-05 | Europ Propulsion | PROCESS AND APPARATUS FOR THE MANUFACTURE OF THREE-DIMENSIONAL REVOLUTION STRUCTURES |
EP0147297A3 (en) * | 1983-12-28 | 1985-08-28 | Societe Europeenne De Propulsion Societe Anonyme Dite: | Process and apparatus for producing tridimensional rotational structures |
US4790052A (en) * | 1983-12-28 | 1988-12-13 | Societe Europeenne De Propulsion | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
EP0147297A2 (en) * | 1983-12-28 | 1985-07-03 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Process and apparatus for producing tridimensional rotational structures |
GB2177345B (en) * | 1985-06-27 | 1989-07-12 | Europ Propulsion | Process for manufacturing three-dimensional structures of fibrous material |
FR2587992A1 (en) * | 1985-10-02 | 1987-04-03 | Europ Propulsion | CARBON-CARBON COMPOSITE MATERIAL FOR FRICTION COMPONENTS, AND ITS APPLICATION TO BRAKING DEVICES |
EP0223642A1 (en) * | 1985-10-02 | 1987-05-27 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Carbon-carbon composite material for friction members and its use in brakes |
US4983451A (en) * | 1987-08-05 | 1991-01-08 | Kabushiki Kaisha Kobe Seiko Sho | Carbon fiber-reinforced carbon composite material and process for producing the same |
FR2619104A1 (en) * | 1987-08-05 | 1989-02-10 | Kobe Steel Ltd | PROCESS FOR THE PREPARATION OF CARBON-REINFORCED CARBON-BASED COMPOSITE MATERIAL AND CARBON-REINFORCED CARBON-BASED COMPOSITE MATERIAL |
EP0524052A1 (en) * | 1991-07-16 | 1993-01-20 | Centre Technique Industriel dit: INSTITUT TEXTILE DE FRANCE | Process and apparatus for manufacturing a non-woven structure and non-woven for use therein |
US5325571A (en) * | 1991-07-16 | 1994-07-05 | Centre Technique Industriel Dit: Institut Textile De France | Method and device for producing a shaped non-woven, non-woven obtained and use thereof |
US5217770A (en) * | 1991-08-15 | 1993-06-08 | The B. F. Goodrich Company | Braided shaped filamentary structures and methods of making |
US5312660A (en) * | 1991-08-15 | 1994-05-17 | The B. F. Goodrich Company | Braided shaped filamentary structures and methods of making |
US5609707A (en) * | 1991-09-04 | 1997-03-11 | The B. F. Goodrich Company | Carbon fiber reinforced carbon/carbon composite and method of its manufacture |
FR2696219A1 (en) * | 1992-09-30 | 1994-04-01 | Dunlop Ltd | Brake disc made of carbon composite material and stack of brake discs comprising this disc. |
US5503254A (en) * | 1992-09-30 | 1996-04-02 | Dunlop Limited | Toughened carbon composite brake discs |
US5782320A (en) * | 1992-09-30 | 1998-07-21 | Dunlop Limited | Toughened carbon composite brake discs |
US5662855A (en) * | 1994-05-17 | 1997-09-02 | The B.F. Goodrich Company | Method of making near net shaped fibrous structures |
US6029327A (en) * | 1994-07-25 | 2000-02-29 | The B.F. Goodrich Company | Process for forming fibrous structures with predetermined Z-fiber distributions |
US5581857A (en) * | 1994-07-25 | 1996-12-10 | The B. F. Goodrich Co. | Process for forming fibrous preform structures |
US6405417B1 (en) | 1994-07-25 | 2002-06-18 | Goodrich Corporation | Process for forming fibrous structures with predetermined Z-fiber distributions |
US5740593A (en) * | 1994-07-25 | 1998-04-21 | The B. F. Goodrich Company | Process for forming fibrous preform structures |
US5504979A (en) * | 1994-07-25 | 1996-04-09 | The Bfgoodrich Company | Process for forming fibrous preform structures |
US5858890A (en) * | 1994-07-25 | 1999-01-12 | The B. F. Goodrich Company | Laminar fibrous structure having Z-fibers that penetrate a constant number of layers |
US5515585A (en) * | 1994-07-25 | 1996-05-14 | The Bf Goodrich Company | Process for forming needled fibrous structures using determined transport depth |
US5546880A (en) * | 1994-12-29 | 1996-08-20 | The Bf Goodrich Company | Annular filamentary structures and methods of making |
CN1078276C (en) * | 1995-06-19 | 2002-01-23 | 航空发动机的结构和研究公司 | Method and apparatus for making ring-shaped parts out of composite material, as well as preforms therefor |
US5908792A (en) * | 1995-10-04 | 1999-06-01 | The B. F. Goodrich Company | Brake disk having a functional gradient Z-fiber distribution |
US6237203B1 (en) | 1995-10-04 | 2001-05-29 | The B. F. Goodrich Company | Process for forming fibrous structures with predetermined Z-fiber distributions |
US6767602B1 (en) | 1996-09-30 | 2004-07-27 | Messier-Bugatti | Preparation of textile preforms for brake discs in composite material |
WO1998014716A1 (en) * | 1996-09-30 | 1998-04-09 | Messier-Bugatti | Preparation of textile preforms for brake discs in composite material |
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FR2754031A1 (en) * | 1996-09-30 | 1998-04-03 | Carbone Ind | DEVELOPMENT OF FIBROUS PREFORMS FOR THE MANUFACTURE OF COMPOSITE MATERIAL BRAKE DISCS |
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US6105223A (en) * | 1997-04-30 | 2000-08-22 | The B. F. Goodrich Company | Simplified process for making thick fibrous structures |
WO1998053218A1 (en) * | 1997-05-23 | 1998-11-26 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Solid construction friction unit, specially a brake disc with several friction bodies |
WO2009063210A1 (en) * | 2007-11-16 | 2009-05-22 | Tom Lloyd Halstead | A method of manufacturing a fibrous structure and an apparatus therefor |
US8381376B2 (en) | 2007-11-16 | 2013-02-26 | Richard Allen | Method of manufacturing a fibrous structure and an apparatus therefor |
WO2012114061A1 (en) * | 2011-02-22 | 2012-08-30 | Marathon Belting Limited | A carbon or carbonizable fibrous structure and a method of manufacturing same |
GB2489076A (en) * | 2011-02-22 | 2012-09-19 | Marathon Belting Ltd | Tubular structure with carbon or carbonizable fibrous intermediate layer having pile |
US20170328429A1 (en) * | 2014-10-10 | 2017-11-16 | Petroceramics S.P.A. | Method for making brake discs in material reinforced with fibres and brake disc made with such method |
Also Published As
Publication number | Publication date |
---|---|
NL181888B (en) | 1987-06-16 |
CA1198268A (en) | 1985-12-24 |
GB2099365B (en) | 1984-11-28 |
IT8221473A0 (en) | 1982-05-25 |
IT1151237B (en) | 1986-12-17 |
DE3220306C2 (en) | 1984-02-23 |
NL181888C (en) | 1987-11-16 |
JPS58643A (en) | 1983-01-05 |
FR2506672A1 (en) | 1982-12-03 |
NL8202003A (en) | 1983-01-03 |
FR2506672B1 (en) | 1984-05-11 |
DE3220306A1 (en) | 1982-12-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19940528 |