Abstract:
A chlorinated polyolefin composition suitable for use in the manufacture of crosslinked, thermoset, flame-retardant articles such as jackets for electrical or fiber optic cables, insulating coatings or layers for electrical conductors, and heat-shrinkable tubing, sheets or other shapes for protection of cable connectors and splices. The composition is thermosetting and moisture curable and comprises a chlorinated polyolefin such as chlorinated polyethylene or chlorosulfonated polyethylene and a non-chlorinated polyolefin which contains moisture crosslinkable silane groups. The non-chlorinated polyolefin preferably comprises polyethylene or a copolymer thereof. Exposure of the composition to moisture causes the formation of intermolecular crosslinks between molecules of the non-chlorinated polyolefin. The compositions can be formed by blending the non-chlorinated polyolefin with a silanated non-chlorinated polyolefin or by silane-grafting a blend of the chlorinated polyolefin and the non-chlorinated polyolefin.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
       [0001]    This application is a continuation-in-part of co-pending U.S. patent application Ser. No. 11/126,540, filed May 11, 2005, which is incorporated by reference herein. 
     
    
     FIELD OF THE INVENTION 
       [0002]    This invention relates to crosslinked, flame-retardant polymer compositions and articles made therefrom. In particular, the invention relates to chlorinated polyolefin-based compositions for use in the manufacture of crosslinked, thermoset articles such as jackets for electrical cables or fiber optic cables, insulating coatings for individual conductors within a cable, and heat-shrinkable tubing, sheets or other shapes for protection of cable connectors and splices. 
       BACKGROUND OF THE INVENTION 
       [0003]    In the manufacture of electrical cable, flame-retardant polymers are used to form an insulating layer over the individual electrical conductors and to form an outer protective jacket surrounding all the conductors. Flame retardancy is typically a major performance requirement for jacketing materials used in wire and cable applications. Cables are generally required to meet standardized industrial specifications of flame-retardancy and to provide a resistance to flame propagation and protect critical electrical circuits in the case of a fire. 
         [0004]    Some of the more commonly used flame-retardant polymers are chlorinated polymers such as polychloroprene, chlorosulfonated polyethylene, polyvinylchloride and chlorinated polyethylene. A big advantage of chlorinated polymers for wire and cable applications is that they are, to a large extent, inherently flame-retardant due to the presence of chlorine in the polymer. This property can also be further enhanced by the addition of flame-retardant additives. Another advantage of chlorinated polymers is their good resistance to oils and chemicals versus non-chlorinated polymers. 
         [0005]    The outer protective jacket of an electrical cable, such as that used in equipment power and instrument control applications, is in contact with the surrounding environment, and can be subjected to harsh conditions. In many cases it is necessary to crosslink the jacket material to meet the demands of industry for these products. Crosslinking renders the material thermoset and imparts much improved performance over un-crosslinked thermoplastic materials in the areas of heat resistance, flame-retardancy, service temperature rating, hot deformation resistance, oil and solvent resistance, toughness, tensile strength, abrasion resistance and cut-through resistance. 
         [0006]    It is known that chlorinated polyolefin-based polymers can be crosslinked by electron beam radiation. However, such radiation crosslinking requires complex equipment and is therefore relatively costly to perform. Furthermore, radiation can cause chlorinated polymers to be degraded by oxidation, dehydrochlorination and chain scission, requiring that they be specially stabilized to prevent this. In addition, costly radiation sensitizers are generally needed to achieve usable levels of crosslinking at doses below the level at which degradation becomes predominant. Furthermore, the sizes of cable which can be handled by commercial radiation equipment are limited, both in terms of jacket thickness and overall diameter of the cable. This limitation is typically manifested as non-uniform crosslinking of the jacket and a resultant variation in physical properties around the circumference of the cable or within the material wall of the jacket. To compensate for this, large diameter cables or cables with thick jackets are usually “over-irradiated” to ensure at least the minimum required dosage is achieved at all points of the jacket. 
         [0007]    It is also well known in the art that chlorinated polyolefin polymers may be crosslinked by chemical methods such as peroxide and, in the case of chlorosulfonated polyethylene, metal oxides and sulfur. However these methods require substantial amounts of heat to effect crosslinking coupled with expensive processing equipment, such as pressurized steam or hot gas caternary lines as used for wire and cable crosslinking. The major disadvantages of using such high temperatures (typically 200 to 350° C.) are potential softening, damage, and oxidative degradation of the polymer. 
         [0008]    Moisture crosslinking (also referred to herein as “moisture curing”) is not subject to these disadvantages. It is also a relatively simple and inexpensive process compared with radiation or traditional chemical crosslinking. Moisture curable compositions contain an organic silane which is grafted to or copolymerized with one or more polymers of the composition. Once the composition is formed into an article, the silane molecules form crosslinks between the polymer chains upon exposure to moisture. In the case of chlorinated polyolefins, attachment of the silane is difficult due to so-called “steric hindrance” of the relatively bulky chlorine atoms preventing access of the silane molecules to the main polymer chain. 
         [0009]    There remains a need for improved moisture crosslinkable, thermosetting polymer compositions containing flame-retardant chlorinated polyolefins for use in the manufacture of crosslinked, thermoset articles such as cable jackets, conductor insulating layers and heat shrinkable tubing, sheets or other shapes for protection of cable connections and splices. 
       SUMMARY OF THE INVENTION 
       [0010]    The present invention overcomes the problems of the prior art mentioned above by providing moisture crosslinked, chlorinated polymer compositions and articles made therefrom. The compositions according to the invention are comprised of a chlorinated polyolefin and a non-chlorinated polyolefin which contains moisture crosslinkable silane groups. The inclusion of the silanated, non-chlorinated polyolefin in the composition overcomes difficulties encountered with direct moisture crosslinking of chlorinated polyolefins. Accordingly, the present invention results in the formation of thermoplastic, moisture crosslinked articles which may possess improved properties over those obtained by the prior art processes. 
         [0011]    In one aspect, the present invention provides a moisture-crosslinked, flame-retardant article formed from a thermosetting, moisture-crosslinkable polymer composition, the polymer composition comprising a blend of: (a) a chlorinated polyolefin; (b) a non-chlorinated polyethylene selected from the group consisting of polyethylene homopolymers and copolymers; (c) hydrolysable silane groups bonded to molecules of the non-chlorinated polyethylene; and (d) a silanol condensation catalyst; wherein the weight ratio of the chlorinated polyolefin to the non-chlorinated polyethylene is at least about 1:1; wherein the hydrolysable silane groups form silane crosslinks between the polyethylene molecules upon exposure to moisture, and wherein the degree of crosslinking is sufficient to provide the article with thermoset properties. 
         [0012]    In another aspect, the present invention provides a method for manufacturing a moisture-crosslinked, flame-retardant article. The method comprises: (a) providing a non-chlorinated, ethylene-based polymer containing hydrolysable silane groups, wherein the ethylene-based polymer comprises ethylene copolymerized with an organic silane, polyethylene homopolymer grafted with an organic silane, or a polyethylene copolymer grafted with an organic silane; (b) blending the ethylene-based polymer with a chlorinated polyolefin and a silanol condensation catalyst to form a moisture-crosslinkable, thermosetting composition, wherein the weight ratio of the chlorinated polyolefin to the ethylene-based polymer is at least about 1:1; (c) melt processing the composition to form the article; (d) exposing the article to moisture so as to hydrolyze at least some of the silane groups of the ethylene-based polymer and thereby form silane crosslinks between molecules of the ethylene-based polymer, wherein the degree of crosslinking is sufficient to impart thermoset properties to the article. 
         [0013]    In yet another aspect, the present invention provides a method for manufacturing a moisture-crosslinked, flame-retardant article. The method comprises: (a) blending together a chlorinated polyolefin, a non-chlorinated polyethylene selected from the group consisting of polyethylene homopolymers and copolymers, and an organic silane; (b) forming a grafted polymer mixture by reacting the organic silane with the non-chlorinated polyethylene, thereby grafting the organic silane to the non-chlorinated polyethylene in the form of hydrolysable silane groups; (c) forming a moisture-crosslinkable, thermosetting composition by blending the grafted polymer mixture with a silanol condensation catalyst; (d) melt processing the composition to form the article; (e) exposing the article to moisture so as to hydrolyze at least some of the silane groups and thereby form silane crosslinks between molecules of the non-chlorinated polyethylene, wherein the degree of crosslinking is sufficient to impart thermoset properties to the article. 
     
    
     DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS 
       [0014]    The present invention provides novel flame-retardant polymer compositions and articles made therefrom. The compositions and articles according to the invention comprise at least the following:
       a chlorinated polyolefin;   either a non-chlorinated, silane-grafted polyethylene resin or a non-chlorinated, silane-ethylene copolymer (sometimes referred to herein as the “non-chlorinated polyolefin”); and   a silane condensation catalyst.       
 
         [0018]    When the composition is formed into an article and exposed to moisture, the silane groups form crosslinks between the polymer chains, thereby providing the article with thermoset properties. As used herein, the term “thermoset” with reference to articles and materials according to the invention means that these articles and materials do not become liquid when heated to a temperature above the crystalline melting point of the highest melting polymer component thereof. The thermoset properties of the articles and materials according to the invention are a result of the silane crosslinking which prevents the molecules from separating when heated. 
         [0019]    The inventors have found that articles produced according to the present invention have properties comparable to articles made of radiation crosslinked flame-retardant polymers, while avoiding problems associated with radiation crosslinking. 
         [0020]    The compositions according to the invention are comprised of polymer resin components and non-resin components. The polymer resin components include the chlorinated polyolefin component and the silane-grafted polyethylene resin or silane-ethylene copolymer resin. Silane-grafted polyethylene resins and silane-ethylene copolymer resins are sometimes collectively referred to herein as “silanated polyethylene resins”. The non-resin components include the silanol condensation catalyst, although the catalyst may be added in the form of a masterbatch which may include one or more polymer resin components, such as polyethylene homopolymers or copolymers. 
         [0021]    Although the term “chlorinated polyolefin” may be used herein in the singular form, it will be appreciated that the chlorinated polyolefin may comprise mixtures of two or more chlorinated polyolefins having different compositions and/or properties. In other words, the chlorinated polyolefin may comprise a mixture of two or more different chlorinated polyolefins, and amounts of chlorinated polyolefins in the compositions and articles disclosed and claimed herein represent the total amounts of all chlorinated polyolefins which may be present in the compositions and articles. 
         [0022]    The chlorinated polyolefin is the predominant resin component of the compositions and articles described and claimed herein. As used herein with reference to the chlorinated polyolefin content, the term “predominant” means that the weight of chlorinated polyolefin component present in the composition is approximately the same or greater than the individual weights of the other components of the composition, including the non-chlorinated polyolefin. In some embodiments, the weight ratio of the chlorinated polyolefin:non-chlorinated polyolefin is at least about 1.5:1, from about 1.5:1 to 2.0:1, from about 2.5:1-3.5:1, or at least about 3:1. 
         [0023]    In terms of weight percent relative to the total polymer resin components, the chlorinated polyolefin is present in an amount of at least 50 weight percent of the polymer resin components. In some embodiments, the chlorinated polyolefin is present in an amount of at least about 60 percent, or at least about 70 percent, or from about 70 to about 75 percent, by weight of the total polymer resin components. In terms of weight percent relative to the total composition and/or article, the chlorinated polyolefin is present in an amount of at least 20 percent, more preferably at least 35 percent by weight of the total composition and/or article. In some preferred embodiments of the invention, the chlorinated polyolefin is present in an amount ranging from about 25 to 75 percent by weight, more preferably from about 35 to 65 percent by weight, for example at least 50 percent by weight, of the total composition and/or article. Maximizing the amount of the chlorinated polyolefin, and the ratio of chlorinated polyolefin:non-chlorinated polyolefin provides the composition and/or article with improved flame retardant properties. 
         [0024]    The chlorinated polyolefin is preferably selected from the group comprising polychloroprene, chlorosulfonated polyethylene, polyvinyl chloride, chlorinated polyethylene and mixtures of any two or more of these chlorinated polyolefins. Preferred chlorinated polyolefins are chlorinated polyethylene, chlorosulfonated polyethylene and mixtures thereof, with chlorinated polyethylene being a particularly preferred chlorinated polyolefin for use either on its own or in combination with one or more other chlorinated polyolefins. 
         [0025]    Where the chlorinated polyolefin component comprises chlorinated polyethylene, it may be prepared commercially by the chlorination of polyethylene. Preferred chlorinated polyethylenes have a chlorine content of between about 25% and 45% by weight and density in the range from about 1.15 g/cm 3  to about 1.25 g/cm 3 . Chlorosulfonated polyethylenes additionally have a sulfur content of between about 0.8% and 1.5% by weight, and density in the range from about 1.10 g/cm 3  to about 1.30 g/cm 3 . 
         [0026]    The non-chlorinated polyolefin component of the composition comprises a non-chlorinated silane-grafted polyethylene, a non-chlorinated silane-ethylene copolymer, or mixtures thereof. Although the term “non-chlorinated polyolefin” may be used herein in the singular form, it will be appreciated that the non-chlorinated polyolefin may comprise mixtures of two or more non-chlorinated polyolefins having different compositions and/or properties. 
         [0027]    The non-chlorinated polyolefin is preferably a polyethylene homopolymer or copolymer, or a mixture thereof, having organic silane crosslinking groups. Suitable polyethylenes for use in the compositions of the invention are selected from the group comprising polyethylene homopolymers and copolymers of ethylene with an olefin other than ethylene having from 3 to 20 carbon atoms. 
         [0028]    Preferred polyethylene homopolymers are selected from the group comprising low density polyethylene, high density polyethylene, linear low density polyethylene, and mixtures of two or more thereof, with high-density polyethylene and linear low-density polyethylene being most preferred. 
         [0029]    Preferred copolymers of ethylene are selected from those in which the olefin other than ethylene is selected from the group comprising propylene, butene, hexene, octene, ethylidene norbornene, vinyl acetate, methyl acrylate, ethyl acrylate and butyl acrylate. The copolymer of ethylene may also comprise an ethylene-propylene or ethylene-propylene-diene elastomer. The copolymers of ethylene may be prepared using so-called metallocene catalysts. 
         [0030]    The non-chlorinated polyolefin preferably comprises from about 50 to about 100% by weight ethylene, more preferably from about 60 to about 90% by weight ethylene, and most preferably from about 80 to about 95% by weight ethylene. The density of the polyethylene or the ethylene co-polymer is preferably in the range of about 0.85 to about 0.95 g/cm 3 . 
         [0031]    The amount of the non-chlorinated polyolefin contained in the composition and/or article preferably ranges from about 5% by weight to about 50% by weight, and more preferably from about 10% to about 30% by weight. It will be appreciated that higher levels of crosslinking can be achieved by adding greater amounts of non-chlorinated polyolefin to the composition. In some embodiments, the content of the non-chlorinated polyolefin, relative to the total polymer resin components, is from about 5 to about 25 percent by weight, and in some embodiments it is present in an amount from about 5 to about 35 percent by weight of the total polymer resin components. 
         [0032]    The organic silane crosslinking groups contained in the compositions according to the invention are derived from silanes having the general formula RR′SiY 2  which are reacted with the non-chlorinated polyolefin as discussed below. The group R represents a monovalent olefinically unsaturated hydrocarbon or hydrocarbonoxy radical, Y represents a hydrolysable organic radical and R′ represents a monovalent olefinically unsaturated hydrocarbon, a hydrocarbonoxy radical, or a hydrolysable organic radical. 
         [0033]    The monovalent olefinically unsaturated hydrocarbon or hydrocarbonoxy radical is preferably selected from the group comprising vinyl, allyl, butenyl, cyclohexenyl, cyclopentadienyl, or cyclohexadienyl radicals. 
         [0034]    The hydrolysable organic radical is preferably selected from the group comprising: alkoxy radicals such as methoxy, ethoxy and butoxy radicals; acyloxy radicals such as formyloxy, acetoxy and propionoxy radicals; oximo radicals such as —ON═C(CH 3 ) 2 , —ON═CCH 3 C 2 H 5  and —ON═C(C 6 H 5 ) 2 ; and substituted amino radicals selected from alkylamino and arylamino radicals such as —NHCH 3 , —NHC 2 H 5  and —NH(C 6 H 5 ) 2 . 
         [0035]    More preferably, the organic silane crosslinking groups are derived from silanes having the general formula RSiY 3 , with the most preferred group R being the vinyl radical, and the most preferred Y group being the methoxy and ethoxy radical. Accordingly, the most preferred organic silanes for use in the present invention are vinyltriethoxysilane and vinyltrimethoxysilane. 
         [0036]    The amount of silane groups reacted with the non-chlorinated polyolefin depends in part upon the reaction conditions and the degree of modification desired in the polyolefin. The proportion may vary from about 0.1 to about 50% by weight based on the total weight of the silanated resin, more preferably from about 0.5 to 10% by weight, and most preferably from about 1.0 to 5.0% by weight. 
         [0037]    The compositions according to the invention can be prepared by a number of different methods. A first preferred method according to the invention involves blending the chlorinated polyolefin, the non-chlorinated polyolefin and the organic silane, together with a free radical initiator, at a temperature sufficient to decompose the initiator and cause grafting of the silane to the polymer components of the composition, in particular to the non-chlorinated polyolefin component. The blending of these components may preferably take place in an extruder at a temperature both above the melt temperature of the polyolefin components and the activation temperature of the free radical initiator. The blend preferably also includes an optional antioxidant processing stabilizer to prevent degradation of the composition in the extruder during the grafting reaction. 
         [0038]    The free radical initiator is preferably an organic peroxide selected from the group comprising 1,1-di(tert-butylperoxy)-3,3,5-trimethylcyclohexane, benzoyl peroxide, dichlorobenzoyl peroxide, dicumyl peroxide and di-tertiary butyl peroxide. The criteria for choosing an appropriate free-radical initiator are known to persons skilled in the art and will not be repeated here. These criteria are also described in U.S. Pat. No. 3,646,155 (Scott), issued on Feb. 29, 1972. The Scott patent is incorporated by reference herein in its entirety. 
         [0039]    Where the silanation takes place in the presence of the chlorinated polyolefin, it is preferred to use a free radical initiator which has a relatively low activation (decomposition) temperature to avoid dehydrochlorination of the chlorinated polyolefin. Under these conditions, the inventors prefer 1,1-di(tert-butylperoxy)-3,3,5-trimethylcyclohexane which has a relatively low activation temperature of about 275-350° F. (135-177° C.). Where the silanation does not take place in the presence of the chlorinated polyolefin, as discussed below, the preferred free radical initiator is dicumyl peroxide. Preferably, the organic peroxide free-radical initiator is added in an amount of from about 0.1 to about 1.0% by weight of the combined polyolefin components, more preferably from about 0.05 to 0.2% by weight. 
         [0040]    During the silanation reaction, the silane will preferentially graft to the non-chlorinated polyolefin component, thereby forming a blend of the chlorinated polyolefin and a silane-grafted polyolefin. The resulting blend may preferably be cooled and pelletized prior to further processing. 
         [0041]    The chlorinated polyolefin/silane-grafted polyolefin blend is then further blended with a silanol condensation catalyst and may also be blended with one or more optional ingredients which are identified below. This mixture is then melt processed, for example by extrusion or co-extrusion, thereby shaping it into an article such as a cable jacket or a tube. Where the article is a cable jacket, it will typically be directly extruded over the cable conductors and the jacketed cable is then wound onto spools. 
         [0042]    The article is then exposed to moisture, preferably at an elevated temperature, causing the silane groups to form intermolecular crosslinks between the non-chlorinated polyolefin molecules via a combined hydrolysis and condensation reaction. The crosslinks encapsulate the chlorinated polyolefin molecules to form a so-called interpenetrating network. There will also be some direct crosslinking of the non-chlorinated and chlorinated polyolefins in cases where some silane groups have reacted with the chlorinated polyolefin, and where the intermolecular distance between the polyolefin molecules is favorable to allow crosslinking to occur. Atmospheric moisture is usually sufficient to permit the crosslinking to occur, but the rate of crosslinking may be increased by the use of an artificially moistened atmosphere, or by immersion in liquid water. Also, subjecting the composition to combined heat and moisture will accelerate the crosslinking reaction. Preferably, crosslinking is effected at a temperature above about 50° C. and most preferably at a temperature of about 85° C. and a relative humidity of about 90-95% for at least about 24 hours. 
         [0043]    Where the article according to the invention comprises a cable jacket, it may not be necessary for the article to be completely moisture crosslinked. Typically, the jacket only needs to be partially crosslinked in order to meet applicable material specifications, such as hot deformation resistance. This test for hot deformation resistance is performed above the melting or softening point of the jacket material. A typical requirement for hot deformation is 30% or less reduction in jacket wall thickness after the application of a 2,000 g weight for 1 hour at 121° C. An example of such a requirement is set out in Underwriters Laboratories Standard UL1277, Electrical Power and Control Cables. In wire and cable manufacture, the jacket is typically crosslinked under ambient conditions, with moisture being supplied by the atmosphere. The crosslinking may occur over a period of several weeks while the spooled cable is awaiting use. 
         [0044]    The silanol condensation catalyst is a non-resin component of the compositions and/or articles according to the invention, and is preferably selected from the group comprising organic bases, carboxylic acids and organometallic compounds including organic titanates and complexes or carboxylates of lead, cobalt, iron, nickel, zinc and tin. More preferably, the catalyst is selected from the group comprising dibutyltin dilaurate, dibutyltin diacetate, dibutyltin octanoate, dioctyltin maleate, dibutyltin oxide and titanium compounds such as titanium-2-ethylhexoxide. The most preferred silanol condensation catalyst is dibutyltin dilaurate, though any material which catalyzes the silane condensation reaction is suitable for the invention. The condensation catalyst is preferably added in an amount sufficient that maximum crosslinking will be achieved after a period of 24 hours at a relative humidity of about 95 percent and a temperature of about 85° C. Preferably, the silanol condensation catalyst is added in an amount from about 0.01 to about 10 percent by weight of the composition, more preferably from about 1 to about 5 percent by weight, and most preferably from about 0.05 to about 2 percent by weight. The catalyst may preferably be added in a masterbatch comprising one or more polymer resin components, such as polyethylene homopolymers or copolymers. 
         [0045]    In a second preferred method according to the invention, the non-chlorinated polyolefin component may be grafted with the silane to form a silane-grafted polyolefin, this step being performed prior to blending the non-chlorinated polyolefin with the chlorinated polyolefin. In this method, the silane-grafted polyolefin component is subsequently blended with the chlorinated polyolefin and the silanol condensation catalyst in the amounts described above. This blend is then melt processed, for example extruded, to form an article such as a cable jacket and is then crosslinked by exposure to moisture, optionally at an elevated temperature, as described above. Methods for grafting a vinyl silane onto an olefin homopolymer or copolymer, followed by catalyzed hydrolysis and condensation of the silane groups, are described in the above-mentioned Scott patent. 
         [0046]    In a third preferred method according to the invention, the silanated polyolefin is purchased as a commercial product. Commercial silanated polyolefins may typically be prepared by copolymerizing the silane with the olefin, as opposed to the polyolefin being grafted with the silane. The commercial silanated polyolefin is blended with the chlorinated polyolefin and the silanol condensation catalyst, followed by melt processing and moisture crosslinking as described above. In addition to the silane, the silanated polyolefin may optionally include one or more co-monomers selected from the group comprising propylene, butene, hexene, octene, ethylidene norbornene, vinyl acetate, methyl acrylate, ethyl acrylate, and butyl acrylate, and dienes. 
         [0047]    The thermosetting properties of the composition according to the invention also make them suitable for the manufacture of heat-shrinkable articles, including cable jackets, insulation for conductors, and heat shrinkable tubing, sheets or other shapes, as mentioned above. Thermoset articles according to the invention can be rendered heat shrinkable by the following steps: softening the article by heating it above the crystalline melting point of the highest melting polymer component; stretching the softened article beyond its original extruded or molded dimensions without rupture using relatively low forces; and “freezing” the article in its stretched state by cooling it rapidly to a temperature below the crystalline melting point. The highest melting component may either be the chlorinated polyolefin or the non-chlorinated polyolefin, depending on the specific polymers selected. Stretching can be accomplished by mechanical, pneumatic or hydraulic means. After cooling, the stretched crosslinks are held in a stable state by the re-formed, solid crystalline regions. Subsequent re-heating of the stretched article above the crystalline melting point will cause the crystalline regions to re-melt and the structure to revert to its original extruded or molded dimensions. The crosslinking also prevents the article from becoming liquid during this shrinking process. 
         [0048]    The compositions according to the invention may include one or more optional ingredients selected from the group comprising pigmenting agents, mineral fillers, flame-retardant additives, plasticizers, antioxidants, process aids, UV stabilizers, lubricants and compatibilizers. The compatibilizers are polymer resin components whereas the other optional ingredients are generally non-resin components. 
         [0049]    The optional compatibilizer is a polymer resin component and may be selected from the group comprising: any of the polyethylenes mentioned above; one or more members of the group comprising ethylene-propylene copolymers; ethylene-propylene diene elastomers; crystalline propylene-ethylene elastomers; thermoplastic polyolefin elastomers; metallocene polyolefins; cyclic olefin copolymers; polyoctenamers; copolymers of ethylene with vinyl acetate, vinyl alcohol, and/or alkyl acrylates; polybutenes; hydrogenated and non-hydrogenated polybutadienes; butyl rubber; polyolefins modified with reactive functional groups selected from the group comprising silanes, alcohols, amines, acrylic acids, methacrylic acids, acrylates, methacrylates, glycidyl methacrylates, and anhydrides; polyolefin ionomers; polyolefin nanocomposites; and block copolymers selected from the group comprising styrene-butadiene, styrene-butadiene-styrene, styrene-ethylene/propylene and styrene-ethylene/butylene-styrene. 
         [0050]    Where a compatibilizing agent is added to the composition of the invention, it is preferably added in an amount from about 1 to about 25 percent by weight. 
         [0051]    The antioxidant, also referred to herein as the process stabilizer, is a non-resin component which may be chosen from any suitable antioxidant or blend of antioxidants designed to prevent degradation of the intermediate resin blends during melt processing. Examples of suitable antioxidant process stabilizers include those classes of chemicals known as hindered phenols, hindered amines, phosphites, bisphenols, benzimidazoles, phenylenediamines, and dihydroquinolines. These may preferably be added in an amount from about 0.1 to 5% by weight of the resin blend, partly depending on the type and quantity of other destabilizing ingredients in the composition, such as halogenated flame-retardants or mineral fillers. 
         [0052]    Mineral fillers are non-resin components which can include silicates such as talc, clay, mica and wollastonite; calcium carbonate; silica; aluminum and magnesium hydroxide; and metal oxides such as magnesium oxide, alumina and antimony trioxide. These fillers may also be treated with surface coupling agents such as silanes and titanates to promote better bonding of the filler to the polymer matrix. 
         [0053]    The flame-retardant additive is a non-resin component which generally comprises one or more organic halogen compounds wherein the halogen is chlorine or bromine, preferably having a high molecular weight and melting point. Preferred flame-retardant additives may be selected from aromatic and aliphatic compounds such as polybrominated diphenylethers, ethylene bistetrabromophthalimide, tetradecabromodiphenoxybenzene, tetrabromobisphenol A derivatives, hexabromocyclododecane, hexachlorocyclopentadiene, and chlorinated paraffins. A preferred example of a polybrominated diphenylether is decabromodiphenyl oxide. 
         [0054]    The organic halogen flame-retardants are preferably used in combination with one or more flame-retardant adjuvants, for example antimony trioxide, which behaves synergistically with the halogen-bearing species, and zinc borate, which acts as both a synergist and smoke suppressor. Since the chlorinated polyolefins already contain halogen, the antimony trioxide synergist may provide sufficient flame-retardancy without the addition of an organic halogen compound. The flame-retardant adjuvant is a non-resin component. 
         [0055]    The flame-retardant additives and adjuvants may preferably be added together as a masterbatch which includes one or more polymer resin components. In one preferred embodiment of the invention, the flame-retardant additive and adjuvant are added as a masterbatch comprising about 30 percent by weight ethylene vinyl acetate copolymer (EVA), about 48 percent by weight decabromobiphenyl oxide, about 16 percent by weight antimony trioxide, along with minor amounts of antioxidants and processing aids. 
         [0056]    The invention is further illustrated by the following examples. 
       Example 1 
       [0057]    A chlorinated polyethylene compound (82.84 weight percent) comprising a chlorinated polyethylene resin and additional ingredients as set out in Table 1 was blended with a polyethylene-silane copolymer (12.16 weight percent) and a catalyst masterbatch (5.00 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The weight ratio of chlorinated polyethylene resin to polyethylene-silane copolymer in this blend was about 3:1. 
         [0058]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. The hot tensile test is a tensile test performed above the melting point of the highest melting point resin component of the material, and it measures the strength, and hence extent, of the crosslinked network created during the curing process. It is typically used to measure the progress of the curing reaction. Mechanical properties together with flame-resistance (using Limiting Oxygen Index) and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that about 75% of maximum crosslinking was achieved after 24 hours in the humidity cabinet. The properties of this sample are set out in Tables 2 and 3. 
       Example 2 
       [0059]    The chlorinated polyethylene compound (82.84 weight percent) of Example 1 was blended with silane-grafted EVA (12.16 weight percent) and a catalyst masterbatch (5.00 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender at 160° C. The weight ratio of chlorinated polyethylene resin to grafted EVA in this blend was about 3:1. 
         [0060]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that about 90% of maximum crosslinking was achieved after 24 hours in the humidity cabinet. The properties of this sample are set out in Tables 2 and 3. 
         [0000]    
       
         
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 1 
               
               
                   
               
               
                   
                   
                 Example 1 
                 Example 2 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated 
                 36.49 
                 36.49 
               
               
                   
                 Polyethylene 
                   
                   
               
               
                   
                 Resin* 
                   
                   
               
               
                   
                 Clay 
                 8.76 
                 8.76 
               
               
                   
                 Mica 
                 13.14 
                 13.14 
               
               
                   
                 Silica 
                 9.24 
                 9.24 
               
               
                   
                 Crosslink Promoter 
                 2.35 
                 2.35 
               
               
                   
                 Antioxidant 
                 2.15 
                 2.15 
               
               
                   
                 Magnesium Oxide 
                 1.95 
                 1.95 
               
               
                   
                 Antimony Trioxide 
                 2.92 
                 2.92 
               
               
                   
                 Process Aid 
                 0.97 
                 0.97 
               
               
                   
                 Diundecyl 
                 4.87 
                 4.87 
               
               
                   
                 Phthalate 
                   
                   
               
               
                   
                 Silane-Grafted 
                 — 
                 12.16 
               
               
                   
                 EVA** 
                   
                   
               
               
                   
                 PE-Silane 
                 12.16 
                 — 
               
               
                   
                 Copolymer*** 
                   
                   
               
               
                   
                 Catalyst 
                 5.00 
                 5.00 
               
               
                   
                 Masterbatch 
                   
                   
               
               
                   
                 Total 
                 100.00 
                 100.00 
               
               
                   
               
               
                 Quantities are expressed in percent by weight. 
               
               
                 *Specific Gravity, 1.16 g/cm 3 ; Chlorine Content, 36%; Mooney Viscosity (1 + 4) @ 121° C., 80. 
               
               
                 **Specific Gravity, 0.94 g/cm 3 ; Melt Index, 2.7g/10 min.; Vinylsilane Graft Content, 2%. 
               
               
                 ***Specific Gravity, 0.92 g/cm 3 ; Melt Index, 0.6 g/10 min.; Vinylsilane Comonomer Content, 4%. 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 2 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. and 40% Elongation 
               
             
          
           
               
                   
                   
                 Tensile Strength (psi) 
               
             
          
           
               
                   
                 Time in Chamber 
                 Example 1 
                 Example 2 
               
               
                   
               
             
          
           
               
                   
                  24 hr 
                 12 
                 11 
               
               
                   
                  48 hr 
                 14 
                 9 
               
               
                   
                 120 hr 
                 18 
                 12 
               
               
                   
                 168 hr 
                 16 
                 9 
               
               
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 3 
               
               
                   
               
               
                   
                   
                 Example 1 
                 Example 2 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Specific Gravity, 
                 1.36 
                 1.32 
               
               
                   
                 g/cm 3   
                   
                   
               
               
                   
                 Tensile Strength, psi 
                 844 
                 660 
               
               
                   
                 Elongation, % 
                 175 
                 430 
               
               
                   
                 Secant Modulus, psi 
                 5210 
                 3800 
               
               
                   
                 Limiting Oxygen 
                 28.7 
                 27.6 
               
               
                   
                 Index, % 
                   
                   
               
               
                   
                 Low Temperature 
                 −10 
                 −15 
               
               
                   
                 Brittleness, ° C. 
                   
                   
               
               
                   
                 Hot Deformation (1 
                 3 
                 27 
               
               
                   
                 hour @ 121° C.), % 
               
               
                   
               
             
          
         
       
     
       Example 3 
       [0061]    A commercially available, pre-compounded thermoplastic chlorinated polyethylene compound (94.74 weight percent), containing about 40 weight percent chlorinated polyethylene resin, was blended with the polyethylene-silane copolymer (5.00 weight percent) of Example 1 and a catalyst masterbatch (0.26 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 4. 
         [0062]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that about 40% of maximum crosslinking was achieved after 24 hours in the humidity cabinet. The properties of this sample are shown in Tables 5 and 6. 
         [0000]    
       
         
               
               
               
             
               
               
               
             
           
               
                 TABLE 4 
               
               
                   
               
               
                   
                   
                 Example 3 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated Polyethylene 
                 94.74 
               
               
                   
                 Compound* 
                   
               
               
                   
                 PE-Silane Copolymer 
                 5.00 
               
               
                   
                 Catalyst Masterbatch 
                 0.26 
               
               
                   
                 Total 
                 100 
               
               
                   
               
               
                 Quantities are expressed in percent by weight. 
               
               
                 *Specific Gravity, 1.28g/cm 3 ; 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 5 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. 
               
             
          
           
               
                   
                   
                 Tensile Strength 
                 Tensile 
               
               
                   
                   
                 (psi) 
                 Strength (psi) 
               
               
                   
                 Time in Chamber 
                 @ 40% Elongation 
                 @ Break 
               
               
                   
               
             
          
           
               
                   
                  24 hr 
                 6 
                 23 
               
               
                   
                  48 hr 
                 6 
                 25 
               
               
                   
                 120 hr 
                 10 
                 36 
               
               
                   
                 168 hr 
                 11 
                 55 
               
               
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
             
           
               
                 TABLE 6 
               
               
                   
               
             
             
               
                   
                 Specific Gravity, g/cm 3   
                 1.25 
               
               
                   
                 Tensile Strength, psi 
                 2730 
               
               
                   
                 Elongation, % 
                 242 
               
               
                   
                 Secant Modulus, psi 
                 26561 
               
               
                   
                 Limiting Oxygen Index, % 
                 28.7 
               
               
                   
                 Low Temperature 
                 −30 
               
               
                   
                 Brittleness, ° C. 
                   
               
               
                   
                 Hot Deformation (1 hour 
                 2 
               
               
                   
                 @ 121° C.), % 
               
               
                   
               
             
          
         
       
     
       Example 4 
       [0063]    The chlorinated polyethylene resin of Example 1 (54.78 weight percent) was blended with the silane-grafted EVA of Example 2 (29.70 weight percent), a catalyst masterbatch (4.38 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst, antioxidant (1.22 weight percent) and an antimony trioxide masterbatch (9.92 weight percent) in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 7. 
         [0064]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring after about 24 hours in the relative humidity cabinet. The properties of this sample are shown in Tables 8 and 9. 
       Example 5 
       [0065]    The chlorinated polyethylene resin of Example 1 (54.78 weight percent) was blended with the polyethylene-silane copolymer of Example 1 (29.70 weight percent), a catalyst masterbatch (4.38 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst, antioxidant (1.22 weight percent) and an antimony trioxide masterbatch (9.92 weight percent) in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 7. 
         [0066]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring after about 24 hours in the relative humidity cabinet. The polyethylene-silane copolymer provides a greater degree of curing but at the expense of flexibility compared with the EVA-based graft. The properties of this sample are shown in Tables 8 and 9. 
         [0000]    
       
         
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 7 
               
               
                   
               
               
                   
                   
                 Example 4 
                 Example 5 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated Polyethylene 
                 54.78 
                 54.78 
               
               
                   
                 Resin 
                   
                   
               
               
                   
                 Silane Grafted EVA 
                 29.70 
                 — 
               
               
                   
                 PE-Silane Copolymer 
                 — 
                 29.70 
               
               
                   
                 Catalyst Masterbatch 
                 4.38 
                 4.38 
               
               
                   
                 Antioxidant 
                 1.22 
                 1.22 
               
               
                   
                 Antimony Trioxide 
                 9.92 
                 9.92 
               
               
                   
                 Total 
                 100.00 
                 100.00 
               
               
                   
               
               
                 Quantities are expressed in percent by weight. 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 8 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. 
               
             
          
           
               
                   
                   
                 Tensile Strength @ Break (psi) 
               
             
          
           
               
                   
                 Time in Chamber 
                 Example 4 
                 Example 5 
               
               
                   
               
               
                   
                  24 hr 
                 41 
                 70 
               
               
                   
                  48 hr 
                 38 
                 80 
               
               
                   
                 120 hr  
                 37 
                 70 
               
               
                   
                 168 hr  
                 33 
                 71 
               
               
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 9 
               
               
                   
               
               
                   
                   
                 Example 4 
                 Example 5 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Specific Gravity, g/cm 3   
                 1.19 
                 1.17 
               
               
                   
                 Tensile Strength, psi 
                 931 
                 846 
               
               
                   
                 Elongation, % 
                 663 
                 181 
               
               
                   
                 Secant Modulus, psi 
                 1895 
                 4846 
               
               
                   
                 Limiting Oxygen Index, % 
                 27.6 
                 27 
               
               
                   
                 Low Temperature 
                 −45 
                 −20 
               
               
                   
                 Brittleness, ° C. 
                   
                   
               
               
                   
                 Hot Deformation (1 hour 
                 27 
                 8 
               
               
                   
                 @ 121° C.), % 
               
               
                   
               
             
          
         
       
     
       Example 6 
       [0067]    The chlorinated polyethylene resin of Example 1 (75 parts by weight), a linear low density polyethylene resin (25 parts by weight), and a processing aid (5 parts by weight) were mixed in a high speed mixer with the slow addition of a grafting solution comprised of vinyltriethoxysilane, a free radical initiator comprising 1,1-di(tert-butylperoxy)-3,3,5-trimethylcyclohexane, and antioxidant. The grafting solution accounted for 5.7 weight percent of the total mixture and the silane, peroxide and antioxidant contents of the total mixture were about 0.2, 0.08 and 0.5 weight percent, respectively. The total mixing time was 2 minutes. The mixture was then grafted on a single screw extruder at a melt temperature of 300-365° F. (149-185° C.). The composition of the grafted resin mixture is shown in Table 10. 
         [0068]    After grafting, the grafted resin mixture (95 weight percent) was mixed in a laboratory Brabender mixer at 160° C. with a catalyst masterbatch (5.00 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst. The composition of this sample is shown in Table 11. 
         [0069]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring after about 48 hours in the humidity cabinet. The addition of the flame-retardant masterbatch raised the low temperature brittle point from −40° C. to −25° C., but the oxygen index improved from 21% to 26.5%. The properties of this sample are shown in Tables 12 and 13. 
       Example 7 
       [0070]    The chlorinated polyethylene resin of Example 1 (75 parts by weight), the linear low density polyethylene resin of Example 6 (25 parts by weight) and a processing aid (5 parts by weight) were mixed in a high speed mixer with the slow addition of a grafting solution comprised of vinyltriethoxysilane, a free radical initiator comprising 1,1-di(tert-butylperoxy)-3,3,5-trimethylcyclohexane, and antioxidant. The grafting solution accounted for 5.7 weight percent of the total mixture and the silane, peroxide and antioxidant contents of the total mixture were about 0.2, 0.08 and 0.5 weight percent, respectively. The total mixing time was 2 minutes. The mixture was then grafted on a single screw extruder at a melt temperature of 300-365° F. (149-185° C.). The composition of the grafted resin mixture is shown in Table 10. 
         [0071]    After grafting, the grafted resin mixture (95 parts by weight) was mixed in a laboratory Brabender mixer at 160° C. with a catalyst masterbatch (5 parts by weight) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst and a flame-retardant masterbatch (25 parts by weight). The flame-retardant masterbatch contained 30.1% EVA, 48.8% decabromobiphenyl oxide, 16.3% antimony trioxide, 3.61% antioxidant stabilizer and 1.19% polyethylene wax as a processing aid. The composition of this sample is shown in Table 11. 
         [0072]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring after about 48 hours in the humidity cabinet. The addition of the flame-retardant masterbatch raised the low temperature brittle point from −40° C. to −25° C., but the oxygen index improved from 21% to 26.5% compared with Example 6. The lower hot deformation resistance is primarily due to the low softening point EVA binder used in the flame-retardant masterbatch. The properties of this sample are shown in Tables 12 and 13. 
       Example 8 
       [0073]    For the purpose of comparison, the chlorinated polyethylene resin of Example 1 (100 parts by weight) and a processing aid (5 parts by weight) were mixed in a high speed mixer with the slow addition of the grafting solution of Examples 6 and 7. The total mixing time was 2 minutes. The mixture was then grafted on a single screw extruder at a melt temperature of 300-365° F. (149-185° C.). 
         [0074]    After grafting, the grafted resin mixture (95 weight percent) was mixed in a laboratory Brabender mixer at 160° C. with a catalyst masterbatch (5.00 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst. The composition of this sample is shown in Table 11. 
         [0000]    
       
         
               
             
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 10 
               
             
             
               
                   
               
               
                 Grafted Resin Formulations 
               
             
          
           
               
                   
                 Example 6 
                 Example 7 
                 Example 8 
               
               
                   
               
             
          
           
               
                 Chlorinated Polyethylene Resin 
                 75 
                 75 
                 100 
               
               
                 Linear Low Density 
                 25 
                 25 
                 — 
               
               
                 Polyethylene* 
                   
                   
                   
               
               
                 Process Aid 
                 5 
                 5 
                 5 
               
               
                 Total 
                 105 
                 105 
                 105 
               
               
                   
               
               
                 Quantities are expressed in parts by weight. 
               
               
                 *Specific Gravity, 0.92 g/cm 3 ; Melt Index, 6.0 g/10 min. 
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 11 
               
               
                   
               
               
                   
                 Example 6 
                 Example 7 
                 Example 8 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 Grafted Resin (Table 10) 
                 95 
                 95 
                 95 
               
               
                 Flame Retardant Masterbatch 
                   
                 25 
                   
               
               
                 Catalyst Masterbatch 
                 5 
                 5 
                 5 
               
               
                 Total 
                 100 
                 125 
                 100 
               
               
                   
               
               
                 Quantities are expressed in parts by weight. 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
             
               
               
               
               
             
           
               
                 TABLE 12 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. 
               
             
          
           
               
                   
                 Tensile Strength @ Break (psi) 
               
             
          
           
               
                 Time in Chamber 
                 Example 6 
                 Example 7 
                 Example 8 
               
               
                   
               
               
                  24 hr 
                 63 
                 55 
                 60 
               
               
                  48 hr 
                 79 
                 70 
                 — 
               
               
                 120 hr 
                 81 
                 72 
                 69 
               
               
                 168 hr 
                 76 
                 68 
                 70 
               
               
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
               
             
               
               
               
               
             
           
               
                 TABLE 13 
               
               
                   
               
               
                   
                 Example 6 
                 Example 7 
                 Example 8 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 Specific Gravity, g/cm 3   
                 1.09 
                 1.19 
                 1.15 
               
               
                 Tensile Strength, psi  
                 1284 
                 1392 
                 1199 
               
               
                 Elongation, % 
                 591 
                 576 
                 749 
               
               
                 Secant Modulus, psi 
                 4076 
                 3953 
                 849 
               
               
                 Limiting Oxygen Index, % 
                 21 
                 26.5 
                 22.6 
               
               
                 Low Temperature 
                 −40 
                 −25 
                 −60 
               
               
                 Brittleness, ° C. 
                   
                   
                   
               
               
                 Hot Deformation (1 
                 9 
                 30 
                 53 
               
               
                 hour @ 121° C.), % 
               
               
                   
               
             
          
         
       
     
         [0075]    By comparing the data for Examples 6 and 8, it can be concluded that silanating a blend of a chlorinated polyolefin resin and a non-chlorinated polyethylene provides an article having better hot deformation properties than that produced by silanating the chlorinated polyolefin resin alone. The hot deformation data for Example 8 does not meet the industry standards mentioned above, which require deformation of 30% or less. It is believed that the improvement in hot deformation resistance provided by the compositions of the present invention is at least partly due to an increased level of grafting between the silane and the non-chlorinated polyethylene, which results in a denser crosslinked network. 
       Example 9 
       [0076]    The commercially available, pre-compounded thermoplastic chlorinated polyethylene compound (89.48 weight percent) of Example 3 was blended with the silane-grafted EVA (10.00 weight percent) of Example 2 and a catalyst masterbatch (0.52 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 14. 
         [0077]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 15 and 16. 
         [0000]    
       
         
               
               
             
               
               
               
             
           
               
                   
                 TABLE 14 
               
               
                   
                   
               
               
                   
                 Example 9 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated Polyethylene 
                 89.48 
               
               
                   
                 Compound* 
               
               
                   
                 Silane-Grafted EVA 
                 10.00 
               
               
                   
                 Catalyst Masterbatch 
                 0.52 
               
               
                   
                 Total 
                 100 
               
               
                   
                   
               
               
                   
                 Quantities are expressed in percent by weight. 
               
               
                   
                 *Specific Gravity, 1.28 g/cm 3   
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
               
               
               
             
           
               
                 TABLE 15 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. 
               
             
          
           
               
                   
                   
                 Tensile Strength (psi) 
               
               
                   
                 Time in Chamber 
                 @ Break 
               
               
                   
                   
               
             
          
           
               
                   
                  24 hr 
                 22 
               
               
                   
                  48 hr 
                 25 
               
               
                   
                 120 hr 
                 23 
               
               
                   
                 168 hr 
                 24 
               
               
                   
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
             
           
               
                   
                 TABLE 16 
               
               
                   
                   
               
             
             
               
                   
                 Specific Gravity, g/cm 3   
                 1.24 
               
               
                   
                 Tensile Strength, psi 
                 2782 
               
               
                   
                 Elongation, % 
                 264 
               
               
                   
                 Secant Modulus, psi 
                 23939 
               
               
                   
                 Limiting Oxygen Index, % 
                 27.6 
               
               
                   
                 Low Temperature 
                 −35 
               
               
                   
                 Brittleness, ° C. 
               
               
                   
                 Hot Deformation (1 hour 
                 4 
               
               
                   
                 @ 121° C.), % 
               
               
                   
                   
               
             
          
         
       
     
       Example 10 
       [0078]    The commercially available, pre-compounded thermoplastic chlorinated polyethylene compound (73.70 weight percent) of Example 3 was blended with a silane-grafted polyethylene resin (25.00 weight percent) and a catalyst masterbatch (1.30 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 17. 
         [0079]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 18 and 19. 
         [0000]    
       
         
               
               
             
               
               
               
             
           
               
                   
                 TABLE 17 
               
               
                   
                   
               
               
                   
                 Example 10 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated Polyethylene 
                 73.70 
               
               
                   
                 Compound* 
               
               
                   
                 Silane-Grafted EVA 
                 25.00 
               
               
                   
                 Catalyst Masterbatch 
                 1.30 
               
               
                   
                 Total 
                 100 
               
               
                   
                   
               
               
                   
                 Quantities are expressed in percent by weight. 
               
               
                   
                 *Specific Gravity, 1.28 g/cm 3   
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
               
               
               
             
           
               
                 TABLE 18 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. 
               
             
          
           
               
                   
                   
                 Tensile Strength (psi) 
               
               
                   
                 Time in Chamber 
                 @ Break 
               
               
                   
                   
               
             
          
           
               
                   
                  24 hr 
                 73 
               
               
                   
                  48 hr 
                 69 
               
               
                   
                 120 hr 
                 56 
               
               
                   
                 168 hr 
                 70 
               
               
                   
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
             
           
               
                   
                 TABLE 19 
               
               
                   
                   
               
             
             
               
                   
                 Specific Gravity, g/cm 3   
                 1.16 
               
               
                   
                 Tensile Strength, psi 
                 4110 
               
               
                   
                 Elongation, % 
                 151 
               
               
                   
                 Secant Modulus, psi 
                 29004 
               
               
                   
                 Limiting Oxygen Index, % 
                 26 
               
               
                   
                 Low Temperature 
                 −35 
               
               
                   
                 Brittleness, ° C. 
               
               
                   
                 Hot Deformation (1 hour 
                 1 
               
               
                   
                 @ 121° C.), % 
               
               
                   
                   
               
             
          
         
       
     
       Example 11 
       [0080]    The chlorinated polyethylene resin of Example 1 (94.74 weight percent) was blended with the silane-grafted EVA of Example 2 (5.00 weight percent) and a catalyst masterbatch (0.26 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 20. 
         [0081]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 21 and 22. 
       Example 12 
       [0082]    The chlorinated polyethylene resin of Example 1 (89.48 weight percent) was blended with the silane-grafted polyethylene resin of Example 10 (10.00 weight percent) and a catalyst masterbatch (0.52 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 20. 
         [0083]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 21 and 22. 
       Example 13 
       [0084]    A chlorinated polyethylene resin (73.70 weight percent) was blended with the silane-grafted EVA of Example 2 (25.00 weight percent) and a catalyst masterbatch (1.30 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 20. 
         [0085]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 21 and 22. 
       Example 14 
       [0086]    The chlorinated polyethylene resin of Example 13 (94.74 weight percent) was blended with the silane-grafted polyethylene resin of Example 10 (5.00 weight percent) and a catalyst masterbatch (0.26 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 20. 
         [0087]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 21 and 22. 
         [0000]    
       
         
               
               
               
               
               
             
           
               
                 TABLE 20 
               
               
                   
               
               
                 Examples 
                 11 
                 12 
                 13 
                 14 
               
               
                   
               
             
             
               
                 Chlorinated 
                 94.74  
                 89.48 
                 73.70* 
                 94.74* 
               
               
                 Polyethylene Resin 
               
               
                 Silane-Grafted EVA 
                 5.00 
                 — 
                 25.00  
                 — 
               
               
                 Silane-Grafted PE 
                 — 
                 10.00 
                 — 
                 5.00 
               
               
                 Resin 
               
               
                 Catalyst Masterbatch 
                 0.26 
                  0.52 
                 1.30 
                 0.26 
               
               
                   
               
               
                 *Specific Gravity, 1.16 g/cm 3 ; Chlorine Content, 36%; Mooney Viscosity (1 + 4) @ 121° C., 80. 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
               
               
               
               
               
             
               
               
               
               
               
             
           
               
                 TABLE 21 
               
             
             
               
                   
               
               
                 Hot Tensile Strength at 140° C. 
               
             
          
           
               
                   
                 Tensile Strength at Break (psi) 
                   
               
             
          
           
               
                 Time in Chamber 
                 11 
                 12 
                 13 
                 14 
               
               
                   
               
             
          
           
               
                  24 hr 
                 10 
                 10 
                 44 
                 11 
               
               
                  48 hr 
                 10 
                 10 
                 31 
                 12 
               
               
                 120 hr 
                 7 
                 — 
                 41 
                 11 
               
               
                 168 hr 
                 10 
                 14 
                 41 
                 14 
               
               
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
               
               
               
             
               
               
               
               
               
             
           
               
                 TABLE 22 
               
               
                   
               
               
                 Examples 
                 11 
                 12 
                 13 
                 14 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 Specific Gravity, g/cm 3   
                 1.18 
                 1.14 
                 1.12 
                 1.17 
               
               
                 Tensile Strength, psi 
                 2658 
                 1526 
                 2812 
                 2305 
               
               
                 Elongation, % 
                 800 
                 657 
                 752 
                 800 
               
               
                 Secant Modulus, psi 
                 669 
                 990 
                 1890 
                 818 
               
               
                 Limiting Oxygen Index, % 
                 22.7 
                 23.2 
                 21.5 
                 23.2 
               
               
                 Low Temperature 
                 &lt;−60 
                 −50 
                 −60 
                 &lt;−60 
               
               
                 Brittleness, ° C. 
               
               
                 Hot Deformation (1 hour 
                 88 
                 50 
                 53 
                 69 
               
               
                 @ 121° C.), % 
               
               
                   
               
             
          
         
       
     
       Example 15 
       [0088]    The chlorinated polyethylene resin of Example 1 (46.20 weight percent) was blended with the silane-grafted EVA of Example 2 (25.05 weight percent), a catalyst masterbatch (3.70 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst, and a flame retardant masterbatch (25.05 weight percent) in a laboratory Brabender mixer at 160° C. The composition of this sample is shown in Table 23. 
         [0089]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Hot tensile measurements were taken after 24, 48, 120 and 168 hours. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are shown in Tables 24 and 25. 
         [0000]    
       
         
               
               
             
               
               
               
             
           
               
                   
                 TABLE 23 
               
               
                   
                   
               
               
                   
                 Example 15 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated Polyethylene 
                 46.20 
               
               
                   
                 Resin 
               
               
                   
                 Silane Grafted EVA 
                 25.05 
               
               
                   
                 PE-Silane Copolymer 
                 — 
               
               
                   
                 Catalyst Materbatch 
                 3.70 
               
               
                   
                 Flame-Retardant 
                 25.05 
               
               
                   
                 Masterbatch 
                   
               
               
                   
                 Total 
                 100.00 
               
               
                   
                   
               
               
                   
                 Quantities are expressed in percent by weight. 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
           
               
                 TABLE 24 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. 
               
             
          
           
               
                   
                 Time in Chamber 
                 Tensile Strength @ Break (psi) 
               
               
                   
                   
               
               
                   
                  24 hr 
                 26 
               
               
                   
                  48 hr 
                 49 
               
               
                   
                 120 hr 
                 34 
               
               
                   
                 168 hr 
                 22 
               
               
                   
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
             
               
               
               
             
           
               
                   
                 TABLE 25 
               
               
                   
                   
               
               
                   
                 Example 15 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Specific Gravity, g/cm 3   
                 1.19 
               
               
                   
                 Tensile Strength, psi 
                 1336 
               
               
                   
                 Elongation, % 
                 674 
               
               
                   
                 Secant Modulus, psi 
                 2381 
               
               
                   
                 Limiting Oxygen Index, % 
                 27.6 
               
               
                   
                 Low Temperature 
                 — 
               
               
                   
                 Brittleness, ° C. 
               
               
                   
                 Hot Deformation (1 hour 
                 33 
               
               
                   
                 @ 121° C.), % 
               
               
                   
                   
               
             
          
         
       
     
       Example 16 
       [0090]    The chlorinated polyethylene compound (82.84 weight percent) of Example 1 was blended with a silane-grafted polyethylene resin (12.16 weight percent) and a catalyst masterbatch (5.00 weight percent) containing about 2 weight percent dibutyltin dilaurate silanol condensation catalyst in a laboratory Brabender at 160° C. The weight ratio of chlorinated polyethylene resin to grafted EVA in this blend was about 3:1. The composition of the blend is shown in Table 26. 
         [0091]    Plaque samples comprising this mixture were cured in a humidity cabinet at 85° C. and 95% relative humidity. Mechanical properties together with flame-resistance and low temperature properties were measured after curing for 168 hours. The hot tensile tests show that crosslinking was achieved, with maximum cure occurring between about 24 and 48 hours conditioning in the humidity cabinet. The properties of this sample are set out in Tables 27 and 28. 
         [0000]    
       
         
               
               
             
               
               
               
             
           
               
                   
                 TABLE 26 
               
               
                   
                   
               
               
                   
                 Example 16 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Chlorinated 
                 36.49 
               
               
                   
                 Polyethylene Resin* 
               
               
                   
                 Clay 
                 8.76 
               
               
                   
                 Mica 
                 13.14 
               
               
                   
                 Silica 
                 9.24 
               
               
                   
                 Crosslink Promoter 
                 2.35 
               
               
                   
                 Antioxidant 
                 2.15 
               
               
                   
                 Magnesium Oxide 
                 1.95 
               
               
                   
                 Antimony Trioxide 
                 2.92 
               
               
                   
                 Process Aid 
                 0.97 
               
               
                   
                 Diundecyl 
                 4.87 
               
               
                   
                 Phthalate 
               
               
                   
                 Silane-Grafted PE 
                 — 
               
               
                   
                 Resin** 
               
               
                   
                 Catalyst 
                 5.00 
               
               
                   
                 Masterbatch 
               
               
                   
                 Total 
                 100.00 
               
               
                   
                   
               
               
                   
                 Quantities are expressed in percent by weight. 
               
               
                   
                 *Specific Gravity, 1.16 g/cm 3 ; Chlorine Content, 36%; Mooney Viscosity (1 + 4) @ 121° C., 80. 
               
               
                   
                 **Specific Gravity, 0.922 g/cm 3 ; Melt Index, 1.0 g/10 min.; Vinylsilane Graft Content, 2%. 
               
             
          
         
       
     
         [0000]    
       
         
               
             
               
               
               
             
               
               
               
             
           
               
                 TABLE 27 
               
             
             
               
                   
               
               
                 Hot Tensile Strength @ 140° C. and 40% Elongation 
               
             
          
           
               
                   
                 Time in Chamber 
                 Tensile Strength (psi) 
               
               
                   
                   
               
             
          
           
               
                   
                  24 hr 
                 11 
               
               
                   
                  48 hr 
                 9 
               
               
                   
                 120 hr 
                 12 
               
               
                   
                 168 hr 
                 9 
               
               
                   
                   
               
             
          
         
       
     
         [0000]    
       
         
               
               
             
               
               
               
             
           
               
                   
                 TABLE 28 
               
               
                   
                   
               
               
                   
                 Example 16 
               
               
                   
                   
               
             
             
               
                   
               
             
          
           
               
                   
                 Specific Gravity, g/cm 3   
                 1.34 
               
               
                   
                 Tensile Strength, psi 
                 782 
               
               
                   
                 Elongation, % 
                 325 
               
               
                   
                 Secant Modulus, psi 
                 6100 
               
               
                   
                 Limiting Oxygen Index, % 
                 27.6 
               
               
                   
                 Low Temperature 
                 −15 
               
               
                   
                 Brittleness, ° C. 
               
               
                   
                   
               
             
          
         
       
     
         [0092]    Although the invention has been described in relation to certain preferred embodiments, it will be appreciated that it is not intended to be limited thereto. Rather, the invention is intended to encompass all embodiments which fall within the scope of the following claims.