CURABLE RUBBER COMPOSITION

Abstract: A curable rubber composition is provided as a laminate comprising a rubber layer containing the curable rubber, and a curative layer comprising a curing agent for the rubber and a polymer which is inert to the curing agent. The two layers are separated by an inert intermediate layer which prevents curing of the rubber whilst the composition is in laminar form.

Description: CURABLE RUBBER COMPOSITION This invention relates to rubber compositions in laminar form, and to a method of joining rubber sheets together using compositions derived from such laminates. Particularly, but not exclusively, the method is concerned with the splicing of rubber sheets in roofing applications. It is known to splice rubber sheets by using adhesives applied between the overlapping regions of the sheets. Typically, cured EPDM sheeting is used in roofing applications, and it is necessary that any joints between adjacent sheets be long-lasting and watertight. One method of joining together overlapping sheets is to apply a layer of adhesive to the surface of one sheet, place an intermediate tape onto the adhesive layer, apply a further adhesive layer onto the intermediate tape and then to apply the second rubber sheet to this further adhesive layer. The joint develops by normal curing of the adhesives, and there may be some crosslinking at ambient temperature which yields a relatively strong bond between the cured EPDM sheet and the intermediate layer, which is usually of a plastic material. A second method commonly known for joining together cured EPDM sheets is to apply a tacky tape between the overlapping sheet regions. After pressing together the two sheets, there may be partial crosslinking of the tape at ambient temperature to improve the bonding. Hitherto, the most widely used method of sheet splicing, particularly for roofing applications, makes use of a so-called hot bonding tape. Such a tape is constituted by a rubber composition including curable rubber and a curative therefor, which curative is substantially only active at elevated temperatures. In use, the tape is laid between the overlapping regions of the sheets, and curing of the tape is achieved by use of a portable, high-temperature (usually greater than 1800C) press, the pressure applied generally being from 2 to 3 atmospheres (200-300 kPa). A drawback of this technique is that it is somewhat inconvenient to use a curing press in situ, for example on a roof. Moreover, it is essential that the rubber sheets to be bonded together are dry before the splicing procedure takes place, and that the sheets have not been vulcanised by use of a steam curing technique. Operating at temperatures in excess of 180 ec means that any absorbed water carried in the rubber sheeting gasifies and generates a vapour cushion between the tape and the sheet, which of course prevents or hinders adhesion. A further disadvantage of the hot bonding tape technique is that although the curative incorporated therein is high temperature active, some curing of the rubber component of the tape will inevitably take place at ambient temperatures, and so the storage life of such tapes is limited, usually to periods of 1 to 3 months. There is a need, therefore, for a means of splicing together rubber sheets which gives a good bond, and also is relatively easy to use in situ, for example on rooftops. According to one aspect of the present invention, there is provided a laminate which comprises (a) a rubber layer comprising a curable rubber; (b) a curative layer comprising a curing agent for the rubber and a polymer which is inert to the curing agent; and (c) an intermediate layer comprising a material which is inert and impermeable to the curing agent, which intermediate layer is disposed between the rubber layer and the curative layer to prevent contact between the curable rubber and the curing agent. A second aspect of the invention provides a method of splicing first and second rubber sheets which comprises (i) providing a laminate which comprises (a) a rubber layer comprising a curable rubber; (b) a curative layer comprising a curing agent for the rubber and a polymer which is inert to the curing agent; and (c) an intermediate layer comprising a material which is inert and impermeable to the curing agent, which intermediate layer is disposed between the rubber layer and the curative layer to prevent contact between the curable rubber and the curing agent; (ii) masticating the laminate to form a substantially homogeneous composition comprising curable rubber and curing agent therefor; (iii) applying the composition to the region of at least one of the sheets to be spliced which, in the spliced product will form an area of sheet overlap; and (iv) bringing together the overlap areas of the sheets and curing the composition in contact with said sheets to form a cured rubber joint therebetween. The term curing the composition in contact with said sheets is intended to include simply allowing the composition to cure under the ambient conditions which obtain in the location where the splicing is effected, for example on a roof. Of course, curing can, if desired, be promoted by the application of heat, but it is a feature of the invention that low temperature curative systems may be employed, in contrast to the hot bonding technique described hereinbefore. It is particularly preferred that the laminate be in the form of an elongate tape, and particular aspects and embodiments of the invention will be described with reference to laminates in tape form, although other laminar forms are equally applicable. Preferred features of the laminate as described herein are to be construed as applying equally to the use of the laminate in the method of the invention. It is furthermore intended that the scope of this invention shall extend to the product of the method defined hereinbefore, that is to first and second rubber sheets which have been joined together by the method. Such product also includes a plurality of such spliced sheets, which may constitute, for example, a finished roof or covering for some other element of substantial size. As is described hereinafter the method using the laminate is particularly suited to sheet splicing in situ, that is in the immediate vicinity where the finished spliced product will serve its function. However, the method is equally applicable to the production of large areas of sheeting in, for example, a factory, from smaller rubber sheets which may have been produced, for example, on sheeting presses calenders or mills which have a maximum product dimension which is smaller than the dimensions required for the final product. The curable rubber used in the rubber layer of the tape according to the invention may be, for example, EPM or EPDM rubber, butyl rubber or halogenated butyl rubber (chlorobutyl or bromobutyl). The curing agent is of course selected so as to be effective for curing such rubber when the tape is masticated into a homogeneous composition. The curing agent may be selected from the well known curatives, zinc oxide, peroxides, phenolic resins, thiourea compounds, mercapto compounds, dithiocarbamates and mixtures thereof being mentioned by way of example. It is particularly preferred that the inert polymer with which the curing agent is admixed to form the curative layer, and the inert material which is employed to form the intermediate layer are the same substance. They will hence have the same viscosity, and mixing of the composition as a whole when performing the method of the invention will thereby be facilitated. The inert material of the intermediate layer acts as a barrier between the curable rubber and the curing agent, preventing any cure of the rubber taking place prior to the mastication stage when performing the method of the invention. The inert material may be, for example, a copolymer of ethylene and an unnaturated carboxylic acid ester, such as EVA, although it is particularly preferred to use polyisobutylene, which is saturated and, hence, unreactive with respect to the curing agent, but which, moreover, is a good tackifier. Hence, in performing the method of the invention, the polyisobutylene promotes the wetting of the rubber sheets to be joined by the composition employed as the jointing material. Of course, in addition to being unreactive, the inert material of the intermediate layer is impermeable to the curing agent, by which is meant that the material acts as a physical barrier and serves to prevent migration of the curing agent to the curable rubber, or vice versa. The components of the curative layer and the intermediate layer will of course be selected within the skill in the art to be compatible with the rubber of the sheets to be spliced in accordance with the method of the invention. In one preferred embodiment, the rubber layer of the tape includes a substance which, when mixed with the curing agent of the curative layer, promotes the curing effect of that agent on the curable rubber. The substance, which may be termed a cure activator or accelerator, does not itself cure the rubber in the absence of the curing agent. It will be well appreciated in the art which particular combinations of curing agent and accelerator/activator will be effective for particular curable rubbers. By way of example, a curing agent which is zinc oxide may be activated by, for example, stearic acid for curing of chlorobutyl rubber. It is a particular feature of the invention that the curing agent may be selected such that, when formed into a homogeneous mixture with the curable rubber, it gives curing of the rubber at ambient temperature. This has advantages when rubber sheets are to be joined together in roofing applications, since the application of heat to initiate curing is not necessary. Of course, the curing agent and any accelerators/activators may also be selected as desired to be heat activated, and in use of the method, heat may be supplied if desired, for example, by hot air or steam techniques. It will also be recognised that subsequent to sheet splicing, if the product comprises a roof, then this may well naturally be subjected to high temperatures. As will be appreciated by those of ordinary skill in the art, the respective layers comprising the laminate of the invention may, in addition to the defined components, also include additives and process aids which are conventionally incorporated into rubbery compositions. For example, fillers, oils, tackifiers and scorch control agents may be included in one or more of the layers. Referring now specifically to the method of the invention, use of the tape (laminate) means that a homogeneous mixture of constant composition can be applied, after mastication of the tape, to the sheets to be spliced, without there being undesirable variation in the actual composition of the jointing compound. This is particularly valuable since roofing sheets are usually spliced in situations where close control of the components of the jointing compound is not possible: roofing is usually assembled by those skilled in the building trades, not by skilled rubber technologists who would be aware of the importance of the jointing compound in ensuring a good, long lasting bond. It is convenient for mastication to be performed in an extruder, so that the homogeneous composition may be delivered directly to the regions of the sheets to be spliced which, when brought together, constitute the sheet overlap areas. Put simply, the jointing compound is applied to the surface of one or both sheets to be spliced and the sheets are brought together for curing of the composition to take place with the composition being in contact with and forming a seal between the two sheets. For roofing applications a small portable extruder has been found to be particularly useful. Preferably after application of the homogeneous composition to the sheets, the overlapping areas are consolidated through a hand-roll pressing device. Depending on the nature of the rubber/curative system, the joint may simply be left to cure naturally at ambient temperature, or heat may be applied to promote curing. It is usual that roofing sheets are cured EPDM, and the method of the invention is particularly suitable for joining such sheets, since the jointing compound becomes fully cured internally and, whilst not wishing to be bound by theoretical considerations, it is believed that simultaneously some covulcanisation takes place with regard to the sites of residual unsaturation contained in the cured EPDM. A particularly strong joint is therefore possible with crosslinking taking place from the first sheet, through the jointing compound, and into the second sheet. The result is a strong and coherent bonding of the two EPDM sheets. The rubber material of the sheets to be spliced may if desired correspond with the curable rubber contained in the tape used to produce the homogeneous jointing composition, although it is generally preferred to employ chlorobutyl rubber as the curable rubber component when joining together EPDM sheets, since it is tacky and cures well at room temperature (depending on the curative selected). The laminates of the invention may be produced by known techniques. For example, each layer may be independently prepared by extrusion, and thereafter the layers put together. Alternatively, the layers may be produced by calendering. Conveniently for a tape form laminate, each layer is, for example, from 2 to 3 cm wide and for example from 1 to 3 mm thick. The following Examples illustrate the invention. EXAMPLES Six laminar tapes (A-F) according to the invention were prepared by forming the respective layer compositions in an extruder and extruding layers each 2.5 cm wide and 0.3cm thick. The appropriate rubber, curative and intermediate layers, designated (a), (b) and (c) respectively, were then combined to form the tapes as specified in Table 1, in which the proportions indicated are in parts by weight. The six tapes were used to splice together EPDM sheets produced from a sheeting compound as shown in Table 2. The sheets were 2mm thick, 25cm wide, produced by calendering ana cured-for 60 minutes in an autoclave at 5.5 kg/m2 (161'C) using steam or hot air. The components/abbreviations of Tables 1 and 2 are as follows: Vistanex L 100 - polyisobutylene having viscosity average molecular weight of 1.06 to 1.44 x 106 DETU - diethylthiourea (accelerator) DPTU - diphenylthiourea (accelerator) Koresin - aromatic hydrocarbon tackifier resin MT black - low reinforcing carbon black filler FEF black - reinforcing carbon black filler Chlorobutyl 1066 - chlorobutyl rubber of Mooney ML(1+8) at 100"C = 49-58 Suprex clay - filler MVT - talc filler MBTS - mercapto benzo thiazyl disulphide MD 82-3 - high unsaturation, fast curing EPDM of Mooney ML(1+8) at 127"C = 60 Esso Butyl 365 - fast curing butyl rubber of Mooney ML(1+8) at 100etc = 41-49 SRF black - semi reinforcing carbon black GMF - dibenzoquinone dioxime MBT - mercaptobenzothiazole (accelerator) ZDBDC - zinc dibutyldithiocarbamate VULCACIT P EXTRAN - dithiocarbamate accelerator VULKACIT ZP - organic dithiocarbamate TEA - triethanolamine MD 83-1 - low Mooney, highly reactive fast curing EPDM of Mooney ML(1+8) at 1270C = 35 MD 725 - normal curing EPDM of Mooney ML(1+8) at 1270C = 50 FEF N550 - fast extruding furnace carbon black Martinal OL III - aluminium hydrate filler Staybelite ester 10 - tackifier Sunpar 2280 - paraffinic oil Agerite resin D - antioxidant ZMTI - zinc mercapto toluene imidazole (antioxidant) NDBDC - nickel dibutyl dithiocarbamate (accelerator/ antioxidant) DTDM - dithiodimorpholine disulphide (accelerator) TMTDS - tetra methyl thiuram disulphide (accelerator) Splices were prepared using each tape by masticating the tape in a laboratory extruder of diameter 25mm, length/ diameter ratio 5:1 at conditions of feed: room temperature; body: 80 C; die 100µC; speed 60 rpm. The homogeneous composition resulting was extruded as a 2.5cm wide, 0.3cm thick layer which was applied directly to the overlap region of the cured EPDM sheets to be spliced. The sheets were then brought together to form a splice of width 2.5cm and thickness 0.3cm. Shear (at room temperature) and peel (at room temperature and 70µC) characteristics of the splices were measured (in k on splices of 2.5cm width, 5cm length) using an Instrom tensile tester at a separation rate of Scm/min. Results are shown in Table 3, from which it will be seen that four different conditions were used for the production of the splices and measurement of their characteristics, as follows: Condition 1: no prior ageing of the tape; spliced assembly aged for 1 month at room temperature prior to testing; EPDM sheet hot air cured. Condition 2: no prior ageing of the tape; spliced assembly aged for 3 days at 800C prior to testing; EPDM sheet hot air cured. Condition 3: as Condition 2; but EPDM sheet was steam cured. Condition 4: as Condition 2, but tape was prior aged for 2 weeks at 70eC. From Table, 3, various conclusions may be drawn. Thus, a comparison of the results obtained at Condition 2 with those of Condition 4 show that the tapes were stable on storage, there being no substantive difference in the characteristics of the splices derived from aged and unaged tapes. Condition 3 measurements show that the method of the invention gives bonding even when the EPDM sheeting has been steam cured. The bond strength is lower than with hot air cured sheets, but this is to be compared with the use of the known hot bonding technique with steam cured EPDM sheets, which gives no measurable adhesion between the sheets. Also for reference, it is noted that the known hot bonding technique used for splicing hot air cured EPDM sheets typically gives peel (room temperature/ 70'C) values of 4.5/1.5 (kg) and shear (room temperature) values of 13.5 (kg). Typical values obtained with the use of conventional splicing adhesives (both air cured and steam cured sheets) are peel (RT/70'C): 2.0/0.3; shear (RT): 12. A comparison of Condition 1 results with those of Condition 2 leads to the conclusion that the spliced assembly will continue curing after formation of the splice. Thus in roofing applications the strength of the bond will increase with time. A further series of tests was performed on tapes produced from compositions A, C and E by calendering each layer to 1.5mm thickness, giving tapes of total thickness 4.5mm and width 2cm. This time the tapes were masticated and applied to the EPDM sheet overlap regions using a portable extruder (MINEX-miniextruder) operating at room temperature feed and 1100C body temperature. The homogeneous composition was applied to cured EPDM sheets to form a splice width of 2.5cm, thickness of 0.3cm, and the strength of the splice was measured as before, again under four different conditions as follows: Condition 5: air cured EPDM; splice assembly aged for 3 days at room temperature. Condition 6: air cured EPDM; splice assembly aged for 3 days at 80-C. Condition 7: as Condition 5, but steam cured EPDM. Condition 8: as Condition 6 but steam cured EPDM. Results are shown in Table 4, from which it may be seen that the ability of splices to continue curing in situ is confirmed, and splice strength values at least as good as those typical of the known hot bonding technique are obtained. TABLE 1 Tape A layer (a) (c) (b) Esso Chlorobutyl 1066 100 - - Vistanex L 100 - 100 100 MT Black 30 30 30 FEF Black 30 30 30 Paraffinic oil 15 30 30 Koresin 15 15 15 ZnO - - 11 DETU - - 1.7 DPTU - - 3.3 MgO 0.5 - Stearic acid 4 - - TABLE 1 Tape B layer (a) (c) (b) Esso Chlorobutyl 1066 100 - - Vistanex L 100 - 100 100 MT Black - 30 30 FEF Black 10 30 30 Paraffinic oil 10 30 30 Koresin 15 15 15 ZnO - - 11 SnCl2 - - 1.7 ZnCl2 - - 1.7 Suprex clay 45 - - Mistron vapour talc 45 - Stearic acid 4 - TABLE 1 Tape C layer (a) (c) (b) MD 82-3 50 - ESSO Butyl 365 50 - Vistanex L 100 - 100 100 MT Black - 30 30 FEF Black - 30 30 Paraffinic oil 30 30 30 Koresin 15 15 15 Red lead - - 7.6 MBTS - - 1.9 SRF Black 70 - Stearic acid 4 - ZnO 5 - GMF 4.5 - - TABLE 1 Tape D layer (a) (c) (b) MD 82-3 50 - ESSO Butyl 365 50 - Vistanex L 100 - 100 100 MT Black - 30 30 FEF Black - 30 30 Paraffinic oil 30 30 30 Koresin 15 15 15 S - - 1.4 MBT - - 0.5 ZDBDC - - 2.9 VULKACIT P EXTRA N - VULKACIT ZP - TEA - - 0.5 SRF Black 70 - Stearic acid 4 - ZnO 5 - TABLE 1 Tape E layer (a) (c) (b) MD 82-3 50 MD 83-1 50 Vistanex L 100 - 100 100 MT Black - 30 30 FEF Black 45 30 30 Paraffinic oil 50 30 30 Koresin 15 15 15 S - - 1.2 MBT - - 0.4 ZDBDC - - 2.4 VULKACIT P EXTRA N - - 0.6 VULKACIT ZP - - 0.8 TEA - - 0.4 SRF Black 45 - Stearic acid 4 - - ZnO 5 TABLE 1 Tape F layer (a) (c) (b) ESSO Butyl 365 100 - Vistanex L 100 - 100 100 MT Black - 30 30 FEF Black - 30 30 Paraffinic oil 30 30 30 Koresin 15 15 15 Red lead - - 8 MBTS - - 2 SRF Black 60 - Stearic acid 1 - ZnO 5 - - GMF 4.5 - TABLE 2 EPDM SHEETING COMPOUND MD 725 100 FEF N550 70 MARTINAL OL III 50 SUNPAR 2280 40 ZINC OXIDE 10 STEARIC ACID 2 STAYBELITE ESTER 10 5 AGERITE RESIN D 0.4 ZMTI 1.6 NDBDC 2 DTDM 2.5 TMTDS 2.5 TABLE 3 SPLICING PERFORMANCE EMI23.1 Conditions <SEP> 1 <SEP> 2 <SEP> 3 <SEP> 4 <tb> Shear <SEP> Peel <SEP> Sheal <SEP> Peel <SEP> Sheal <SEP> Peel <SEP> Sheal <SEP> Peel <tb> Test <SEP> Temperature <SEP> RT <SEP> RT/70 C <SEP> RT <SEP> RT/70 C <SEP> RT <SEP> RT/70 C <SEP> RT <SEP> RT/70 C <tb> Tape <tb> A <SEP> 0.75 <SEP> 0.5 <SEP> / <SEP> * <SEP> 17.0 <SEP> 12.0/1.4 <SEP> 6.7 <SEP> 3.0/0.3 <SEP> 18.0 <SEP> 11.5/1.3 <tb> <SEP> B <SEP> 1.1 <SEP> 0.65 <SEP> / <SEP> * <SEP> 18.0 <SEP> 10.5/1.2 <SEP> 5.6 <SEP> 2.0/0.15 <SEP> 17.5 <SEP> 12.0/1.1 <tb> C <SEP> 1.2 <SEP> 0.65 <SEP> / <SEP> * <SEP> 18.0 <SEP> 12.0/1.0 <SEP> 6.5 <SEP> 2.0/0.1 <SEP> 18.2 <SEP> 12.0/0.9 <tb> D <SEP> 3.0 <SEP> 0.3 <SEP> / <SEP> * <SEP> 17.6 <SEP> 5.4/7.5 <SEP> 8.5 <SEP> 3.2/0.26 <SEP> 16.8 <SEP> 6.0/0.7 <tb> E <SEP> 1.75 <SEP> 0.55 <SEP> / <SEP> * <SEP> 16.9 <SEP> 7.0/0.4 <SEP> 6.5 <SEP> 2.1/0.27 <SEP> 16.5 <SEP> 7.2/0.3 <tb> F <SEP> 2.3 <SEP> 0.65 <SEP> / <SEP> * <SEP> 16.9 <SEP> 7.1/0.4 <SEP> 8.2 <SEP> 2.3/0.4 <SEP> 16.5 <SEP> 6.9/0.3 <tb> * = too low to measure TABLE 4 EMI24.1 Condition <SEP> 5 <SEP> 6 <SEP> 7 <SEP> 8 <tb> Shear <SEP> Peel <SEP> Shear <SEP> Peel <SEP> Shear <SEP> Peel <SEP> Shear <SEP> Peel <tb> Test <SEP> Temperature <SEP> RT/70 C <SEP> RT/70 C <SEP> RT/70 C <SEP> RT/70 C <SEP> RT/70 C <SEP> RT/70 C <SEP> RT/70 C <SEP> RT/70 C <tb> Tape <tb> A <SEP> 4.8/1.4 <SEP> 3.0/0.05 <SEP> 22.0/5.2 <SEP> 8.5/1.0 <SEP> 5.0/1.5 <SEP> 3.0/0.07 <SEP> 6.0/2.5 <SEP> 2.0/0.8 <tb> C <SEP> 6.8/1.4 <SEP> 1.0/0.05 <SEP> 17.5/3.0 <SEP> 9.5/0.7 <SEP> 5.5/1.8 <SEP> 2.1/0.08 <SEP> 11.0/2.8 <SEP> 4.0/1.0 <tb> E <SEP> 4.8/1.4 <SEP> 3.5/0.15 <SEP> 13.0/4.3 <SEP> 9.2/1.3 <SEP> 4.0/1.7 <SEP> 3.2/0.2 <SEP> 12.0/2.7 <SEP> 6.0/1.4 <tb>

Claims: CLAIMS 1. A laminate which comprises (a) a rubber layer comprising a curable rubber; (b) a curative layer comprising a curing agent for the rubber and a polymer which is inert to the curing agent; and (c) an intermediate layer comprising a material which is inert and impermeable to the curing agent, which intermediate layer is disposed between the rubber layer and the curative layer to prevent contact between the curable rubber and the curing agent. 2. A laminate according to claim 1, wherein the inert polymer of the curative layer and the inert material of the intermediate layer are the same substance. 3. A laminate according to claim 1 or 2, wherein the inert polymer and/or the inert material comprises polyisobuty lene or ethyl enevinyl acetate copolymer. 4. A laminate according to any one of the preceding claims, wherein the rubber layer comprises a cure activator or accelerator which does not itself cure the rubber but which in admixture with the curing agent contained in the curative layer promotes curing of said rubber. 5. A laminate according to any one of the preceding claims, wherein the curing agent, optionally in combination with an activator or accelerator, is effective for curing the rubber at ambient temperature. 6. A laminate according to any one of claims 1 to 4, wherein the curing agent is effective for curing the rubber at elevated temperature using steam or hot air as heating medium. 7. A laminate according to any one of the preceding claims, wherein the curing agent is selected from zinc oxide, peroxides, phenolic resins thiourea compounds, mercapto compounds, dithiocarbamates, and mixtures thereof. 8. A laminate according to any one of the preceding claims, wherein the curable rubber comprises EPM, EPDM, butyl or halogenated butyl rubber 9. A laminate according to any one of the preceding claims, wherein the rubber layer and/or curative layer and/or intermediate layer includes conventional rubber comp osition additives and/or process aids selected from fillers, oils and tackifiers. 10. A laminate according to any one of the preceding claims when in the form of an elongate tape. 11. A method of splicing first and second rubber sheets which comprises (i) providing a laminate according to any one of the preceding claims; (ii) masticating the laminate to form a substantially homogeneous composition comprising curable rubber and curing agent therefor; (iii) applying the composition to the region of at least one of the sheets to be spliced which, in the spliced product, will form an area of sheet overlap; and (iv) bringing together the overlap areas of the sheets and curing the composition in contact with said sheets to form a cured rubber joint therebetween. 12. A method according to claim 11, wherein the rubber of the sheets is the same as the curable rubber of the laminate. 13. A method accoraing to claim 11 or 12, wherein the rubber of the sheet comprises EPM, EPDM, butyl or halogenated butyl rubber. 14 A method according to claim 11 wherein the rubber of the sheet is EPDM and the curable rubber of the laminate is chlorinated butyl rubber. 15. A method according to claim 13 or 14, wherein the rubber of the sheet is in cured form. 16. A method according to any one of claims 11 to 15, wherein mastication of the laminate and application of the resulting composition is carried out by means of an extruder. 17. A method according to any one of claims 11 to 16, wherein curing of the composition is carried out at ambient temperature. 18. A method according to any one of claims 11 to 16, wherein curing of the composition is carried out at elevated temperature. 19 Two or more rubber sheets when spliced together by the method according to any one of claims 11 to 18. 20 A roof or roofing element comprising sheets according to claim 19.

Inventors: KNAEPEN, MARC, STELLA, GIANDOMENICO
Applicants: EXXON RESEARCH AND ENGINEERING COMPANY
Application year: 1985
Main classification: B32B25
IPC codes: B32B25, C08J3