Patent Publication Number: US-11049629-B2

Title: Non-halogen flame-retardant insulated electric wire and non-halogen flame-retardant cable

Description:
The present application is a Continuation Application of U.S. patent application Ser. No. 15/170,727, filed on Jun. 1, 2016, which is based on and claims priority from Japanese Patent Application No. 2015-118481, filed on Jun. 11, 2015, the entire contents of which are incorporated herein by reference. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention relates to a non-halogen flame-retardant insulated electric wire and a non-halogen flame-retardant cable. 
     2. Description of the Related Art 
     Electric wires and cables used in rolling stock, automobiles, devices, etc., desirably have high abrasion resistance, flame retardancy, good low-temperature characteristics, and other properties as occasion demands. 
     Polyvinyl chloride (PVC), which is inexpensive and highly flame retardant, has been widely used as the electric wire coating material. However, PVC contains halogen and releases halogen gas when burned, raising environmental issues. Thus, non-halogen electric wire coating materials have been sought after. 
     One approach to obtaining a non-halogen flame retardant electric wire known in the art is to load the coating material with a metal hydroxide, such as magnesium hydroxide or aluminum hydroxide, that acts as a flame retardant. In order to load the coating material with such a flame retardant, a soft polyolefin, such as an ethylene-vinyl acetate copolymer (EVA) or an ethylene-acrylic acid ester copolymer, is used as a base polymer of a coating material (refer to Japanese Unexamined Patent Application Publication No. 2006-8873). 
     However, soft polyolefins such as EVA have low strength, deform easily, are susceptible to abrasion, and are easily damaged. 
     Moreover, in stripping an electric wire terminal by using a wire stripper or the like, the coating material may become stretched and a clean cut may not be obtained, thereby leaving some part of the coating material on a conductor in some instances. When this happens, sparks occur during resistance welding and render the process difficult to perform. 
     Moreover, electric wires may fuse to each other or deform in a high-temperature environment involving a temperature higher than the melting point of the coating material. This makes inspection of wiring and replacement operation difficult. 
     SUMMARY OF THE INVENTION 
     In view of the foregoing and other exemplary problems, drawbacks, and disadvantages of the conventional methods and structures, an exemplary feature of the present invention is to provide non-halogen flame-retardant insulated electric wire and non-halogen flame-retardant cable. 
     It is desirable to provide a non-halogen flame-retardant insulated electric wire and a non-halogen flame-retardant cable that have excellent abrasion resistance, terminal processability, and high handling ease in a high-temperature environment. 
     The present invention provides the following non-halogen flame-retardant insulated electric wire and non-halogen flame-retardant cable. 
     [1] A non-halogen flame-retardant insulated electric wire comprising a conductor and a crosslinked single-layer or multilayer insulating layer on an outer periphery of the conductor, in which the insulating layer has a tensile elastic modulus of 500 MPa or more and an elongation at break of 120% or less in a tensile test performed at a displacement rate of 200 mm/min, and has a storage elastic modulus at 125° C. of 3×10 6  Pa or more in a dynamic viscoelasticity test. 
     [2] The non-halogen flame-retardant insulated electric wire described in [1], in which the insulating layer has an outermost layer formed of a coating material that contains magnesium hydroxide and/or aluminum hydroxide and has a specific gravity of 1.4 or more. 
     [3] The non-halogen flame-retardant insulated electric wire described in [1] or [2], in which the insulating layer has an outermost layer formed of a coating material that includes a melting point peak of 120° C. or higher in differential scanning calorimetry. 
     [4] The non-halogen flame-retardant insulated electric wire described in [2] or [3], in which the coating material contains, as a base polymer, a polyolefin having a melting point of 120° C. or higher. 
     [5] The non-halogen flame-retardant insulated electric wire described in [4], in which the coating material also contains, as the base polymer, a polyolefin having a melting point lower than 120° C. 
     [6] A non-halogen flame-retardant cable comprising a crosslinked sheath in an outermost layer, the crosslinked sheath having a tensile elastic modulus of 500 MPa or more and an elongation at break of 120% or less in a tensile test performed at a displacement rate of 200 mm/min, and having a storage elastic modulus at 125° C. of 3×10 6  Pa or more in a dynamic viscoelasticity test. 
     [7] The non-halogen flame-retardant cable described in [6], in which the sheath is formed of a coating material that contains magnesium hydroxide and/or aluminum hydroxide and has a specific gravity of 1.4 or more. 
     [8] The non-halogen flame-retardant cable described in [6] or [7], in which the sheath is formed of a coating material that includes a melting point peak of 120° C. or higher in differential scanning calorimetry. 
     The present invention thus provides a non-halogen flame-retardant insulated electric wire and a non-halogen flame-retardant cable that have excellent abrasion resistance, terminal processability, and high handling ease in a high-temperature environment. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       The foregoing and other exemplary purposes, aspects and advantages will be better understood from the following detailed description of the invention with reference to the drawings, in which: 
         FIG. 1  is a cross-sectional view of an embodiment (single-layer insulating layer) of an insulated electric wire according to the present invention; 
         FIG. 2  is a cross-sectional view of an embodiment (double-layer insulating layer) of an insulated electric wire according to the present invention; and 
         FIG. 3  is a cross-sectional view of an embodiment of a cable according to the present invention. 
     
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     Referring now to the drawings, and more particularly to  FIGS. 1-3 , there are shown exemplary embodiments of the structures according to the present invention. 
     Non-Halogen Flame-Retardant Insulated Electric Wire 
     A non-halogen flame-retardant insulated electric wire according to one embodiment of the present invention includes a crosslinked single-layer or multilayer insulating layer on the outer periphery of a conductor. The insulating layer has a tensile elastic modulus of 500 MPa or more and an elongation at break of 120% or less in a tensile test performed at a displacement rate of 200 mm/min, and has a storage elastic modulus at 125° C. of 3×10 6  Pa or more in a dynamic viscoelasticity test. 
       FIGS. 1 and 2  are cross-sectional views showing embodiments of the insulated electric wire according to the present invention.  FIG. 1  shows an embodiment in which the insulating layer is a single layer.  FIG. 2  shows an embodiment in which the insulating layer is constituted by two layers. Embodiments of the present invention will now be described with reference to the drawings. 
     According to embodiments of the present invention, the insulating layer may be constituted by one layer as shown in FIG.  1  or may have a multilayer structure constituted by two or more layers (in  FIG. 2 , an example of a double-layer insulating layer is shown). 
     An insulated electric wire  10  of an embodiment shown in  FIG. 1  includes a conductor  11  and an insulating layer  12  directly covering the conductor  11 . The insulating layer  12  can be formed by extrusion molding. 
     An insulated electric wire  20  according to an embodiment shown in  FIG. 2  includes a conductor  11 , an inner insulating layer  21  directly covering the conductor  11 , and an outer insulating layer  22  covering the inner insulating layer  21 . The insulating layers  21  and  22  can be formed simultaneously by co-extrusion. 
     Conductor 
     The conductor  11  may be a conductor obtained by stranding tin-coated annealed copper wires, but is not particularly limited. The conductor outer diameter may be any and may be, for example, about 0.15 to 7 mm. The number of conductors that serve as the conductor  11  may be 1 as illustrated in  FIG. 1 , or more than 1. 
     Insulating Layer 
     The single-layer insulating layer  12  illustrated in  FIG. 1  has a tensile elastic modulus of 500 MPa or more and an elongation at break of 120% or less in a tensile test performed at a displacement rate of 200 mm/min, and a storage elastic modulus at 125° C. of 3×10 6  Pa or more in a dynamic viscoelasticity test. 
     If the tensile elastic modulus is less than 500 MPa, abrasion resistance is not obtained. The tensile elastic modulus is preferably 600 MPa or more. A tensile elastic modulus of 700 MPa or more is more preferable, since fracture does not easily occur even when the insulating layer is pressed against a sharp edge or the like. 
     If the elongation at break is higher than 120%, the coating material deforms during electric wire terminal stripping and is likely to remain on the conductor, resulting in insufficient terminal processability. The elongation at break may be any value equal to or less than 120%, but is preferably 110% or less and more preferably 100% or less. 
     When the storage elastic modulus at 125° C. is 3×10 6  Pa or more, fusion and deformation of the electric wires can be reduced in the 125° C. environment. The storage elastic modulus at 125° C. is preferably 3.5×10 6  Pa or more and more preferably 4×10 6  Pa or more. 
     For a multilayer insulating layer, the above-described properties are to be satisfied by the multilayer insulating layer as a whole. For example, in the case of two layers illustrated in  FIG. 2 , the inner insulating layer  21  and the outer insulating layer  22  as a whole are to satisfy the properties. An insulating layer that has the above-described properties as a whole is formed as an outermost layer of an insulated electric wire. 
     The outermost layer (the insulating layer  12  in  FIG. 1  and the outer insulating layer  22  in  FIG. 2 ) of the insulating layer is preferably formed of a coating material having a specific gravity of 1.4 or more in order to enhance flame retardancy. 
     The outermost layer of the insulating layer is preferably formed of a coating material that contains a melting point peak of 120° C. or higher in a differential scanning calorimetry (DSC). This is because the above-described properties are easily obtained. 
     The coating material constituting the outermost layer of the insulating layer contains any non-halogen polyolefin as a base polymer without limitation. However, a polyolefin having a melting point of 120° C. or higher is preferably contained since excellent terminal processability is easily obtained, for example. Examples of the polyolefin having a melting point of 120° C. or higher include straight-chain low-density polyethylene, high-density polyethylene, and polypropylene. These can be used alone or in combination. 
     In 100 parts by mass of the base polymer, preferably 25 to 55 parts by mass, more preferably 30 to 50 parts by mass, and yet more preferably 35 to 45 parts by mass of the polyolefin having a melting point of 120° C. or higher is contained. 
     Engineering plastics such as polybutylene terephthalate are also available as the polymer having a melting point of 120° C. or higher, but are preferably not used since it is difficult to load these plastics with a non-halogen flame retardant. 
     The coating material preferably contains, as a base polymer, a polyolefin having a melting point lower than 120° C. as well as the polyolefin having a melting point of 120° C. or higher in order to enhance the flame retardant loadability. Examples of the polyolefin having a melting point lower than 120° C. include low-density polyethylene, ultralow-density polyethylene, ethylene-acrylic acid ester copolymers, ethylene-vinyl acetate copolymers, ethylene-propylene copolymers, ethylene-octene copolymers, ethylene-butene copolymers, and butadiene-styrene copolymers. These materials may be modified with an acid such as maleic acid. These materials may be used alone or in combination. One of the above-described materials modified with an acid such as maleic acid may be used in combination with one of the above-described materials unmodified. 
     In 100 parts by mass of the base polymer, preferably 45 to 75 parts by mass, more preferably 50 to 70 parts by mass, and yet more preferably 55 to 65 parts by mass of the polyolefin having a melting point lower than 120° C. is contained. 
     The flame retardant used in the coating material constituting the outermost layer of the insulating layer may be any non-halogen flame retardant. Magnesium hydroxide and aluminum hydroxide, which are metal hydroxides, are particularly preferable. These may be used alone or in combination. Magnesium hydroxide is more preferable since the main dehydration reaction is at 350° C., which is high, and exhibits excellent flame retardancy. Phosphorus flame retardants such as red phosphor and triazine flame retardants such melamine cyanurate are also available as the non-halogen flame retardants. However, they release phosphine gas and cyan gas harmful to human body and thus are not preferable. 
     Other specific examples of the non-halogen flame retardants that can be used include clay, silica, zinc stannate, zinc borate, calcium borate, dolomite hydroxide, and silicone. 
     In view of dispersibility, the flame retardant may be surface-treated with a silane coupling agent, a titanate coupling agent, or a fatty acid such as stearic acid. 
     The amount of the flame retardant added is not particularly limited but when the polyolefin is highly loaded with magnesium hydroxide or aluminum hydroxide and the specific gravity of the coating material is adjusted to 1.4 or more, high flame retardancy can be obtained. For example, 110 to 190 parts by mass of magnesium hydroxide or aluminum hydroxide is added to 100 parts by mass of the base polymer. 
     To the coating material (resin composition) constituting the outermost layer of the insulating layer, various additives can be added as needed. Examples of the additives include a crosslinking agent, a crosslinking aid, a flame retardant, a flame retarding aid, an ultraviolet absorber, a photostabilizer, a softener, a lubricant, a coloring agent, a reinforcing agent, a surfactant, an inorganic filler, an antioxidant, a plasticizer, a metal chelating agent, a blower, a compatibilizer, a processing aid, and a stabilizer. 
     A layer other than the outermost layer of the insulating layer (such a layer is absent in  FIG. 1  and is the inner insulating layer  21  in  FIG. 2 ) may be formed of any material as long as the above-described properties are exhibited as the whole insulating layer. For example, any non-halogen resin composition may be used. The base polymer may be any. Examples of the base polymer include polyolefins such as high-density polyethylene, medium-density polyethylene, low-density polyethylene, ultralow-density polyethylene, and ethylene-acrylic acid ester copolymers. These polyolefins may be used alone or as a blend of two or more. If needed, the above-described various additives such as a crosslinking agent may be added to the coating material (resin composition) that constitutes the layer other than the outermost layer of the insulating layer. 
     The insulating layer  12 , the inner insulating layer  21 , and the outer insulating layer  22  are each formed by performing crosslinking after molding. Examples of the crosslinking method include chemical crosslinking that uses an organic peroxide, a sulfur compound, silane, or the like, irradiation crosslinking that uses an electron beam, a radiation, or the like, and crosslinking that involves other chemical reactions. Any of these crosslinking methods may be employed. 
     The insulated electric wires  10  and  20  may each be equipped with a braided line or the like, if needed. 
     Non-Halogen Flame-Retardant Cable 
     A non-halogen flame-retardant cable according to an embodiment of the present invention includes a crosslinked sheath that constitutes an outermost layer, the crosslinked sheath having a tensile elastic modulus of 500 MPa or more and an elongation at break of 120% or less in a tensile test performed at a displacement rate of 200 mm/min, and a storage elastic modulus at 125° C. of 3×10 6  Pa or more in a dynamic viscoelasticity test. 
       FIG. 3  is a cross-sectional view of an embodiment of a cable according to the present invention. Embodiments of the present invention are described below with reference to the drawings. 
     A cable  30  according to this embodiment includes a three-core wire prepared by bundling, together with a filler  13  such as paper, three single-layer insulated electric wires  10  of the above-described embodiment each including a conductor  11  and an insulating layer  12  covering the conductor  11 , a binding tape  14  wound around the outer periphery of the three-core wire, and a sheath  15  extruded onto the outer periphery of the binding tape  14 . The wire is not limited to a three-core wire, and may alternatively be one electric wire (single core) or a multicore wire including 2 or 4 or more cores. The binding tape  14  may be omitted or replaced by a braid. 
     The sheath  15  having the above-described properties is preferably formed of the coating material (resin composition) that constitutes the insulating layer  12  and the outer insulating layer  22 . In this embodiment, the insulating layer  12  also has the above-described properties and is formed of the coating material (resin composition) described above. However, the insulating layer  12  is not limited to this and may be formed of a different resin composition for forming an insulating layer (preferably a non-halogen flame retardant resin composition). The sheath  15  is subjected to a crosslinking process through electron beam irradiation or the like after molding. 
     In this embodiment, the sheath has a single layer structure as illustrated in  FIG. 3 . Alternatively, the sheath may have a multilayer structure. In this case, at least the outermost layer is to have the properties described above and be formed of the coating material (resin composition) described above. Although the single-layer insulated electric wire  10  illustrated in  FIG. 1  is used, the double-layer insulated electric wire  20  illustrated in  FIG. 2  can be used instead in this embodiment. 
     The cable  30  may be equipped with a braided line or the like, if needed. 
     EXAMPLES 
     The present invention will now be described in further detail through Examples. The present invention is in no way limited by the examples described below. 
     A single-layer insulated electric wire  10  illustrated in FIG.  1  and a double-layer insulated electric wire  20  illustrated in  FIG. 2  were fabricated as follows. 
     (1) A 37 strands/0.18 mm tin-coated conductor was used as the conductor  11 . 
     (2) Components in Tables 1 and 2 were blended and kneaded with a 14-inch open roll to prepare a resin composition. The resin compositions were pelletized with a pelletizer to obtain an outer-layer material and an inner-layer material. 
     (3) In fabricating a single-layer insulated electric wire  10  illustrated in  FIG. 1 , the obtained outer-layer material was extruded onto the conductor  11  by using a 40 mm extruder so as to form an insulating layer  12  having a thickness of 0.26 mm on the conductor  11 .
 
(4) In fabricating a double-layer insulated electric wire  20  illustrated in  FIG. 2 , the obtained outer-layer material and inner-layer material were co-extruded with a 40 mm extruder so that an inner insulating layer  21  having a thickness of 0.1 mm and an outer insulating layer  22  having a thickness of 0.16 mm are formed on the conductor  11 .
 
(5) The obtained insulated electric wire was irradiated with an electron beam to conduct crosslinking (irradiation dose: 15 Mrad in Examples and Comparative Example 1, 10 Mrad in Comparative Example 2, 20 Mrad in Comparative Example 3, and 2 Mrad in Comparative Example 5). No crosslinking was performed in Comparative Example 4.
 
     The specific gravity of the insulating layer  12  of the single-layer insulated electric wire  10  and the outer insulating layer  22  of the double-layer insulated electric wire  20  was measured in accordance with JIS-Z8807. The obtained crosslinked insulated electric wire was subjected to tests described below. The results are shown in Table 1. 
     (1) Tensile Test 
     The insulating layer after removal of the conductor  11  was subjected to a tensile test in accordance with JIS C3005 at a tensile rate of 200 mm/min. Samples with a tensile elastic modulus of 500 MPa or more and an elongation at break of 120% or less were rated pass (A). 
     (2) Dynamic Viscoelasticity Test 
     The insulating layer after removal of the conductor  11  was subjected to a dynamic viscoelasticity test in accordance with JIS K7244-4 at a frequency of 10 Hz, a strain of 0.08%, and a temperature elevation rate of 10° C./min. Samples having a storage elastic modulus at 125° C. of 3×10 6  Pa or more were rated pass (A). 
     (3) Abrasion Test 
     The insulated electric wire was evaluated in accordance with EN50305.5.2. Samples withstanding 150 or more abrasion cycles were rated pass (A) and samples withstanding less than 150 cycles were rated fail (F). 
     (4) Terminal Processability Test 
     Ten insulated electric wire terminals were each stripped 10 mm with a wire stripper. Samples with which all ten wires could be processed without stretching the insulating layers were rated pass (A) and other samples were rated fail (F). 
     (5) Fusion Deformation Test (Handling Ease of Electric Wire in High-Temperature Environment) 
     Ten insulated electric wires were bundled and put in a 125° C. constant-temperature oven. Samples in which the number of electric wires that fused to each other or deformed was less than 5 were rated pass (A), and samples in which the number was 5 or more were rated fail (F). 
     (6) Flame Retardancy Test 
     An insulated electric wire having a length of 600 mm was kept upright, and flame of a Bunsen burner was applied to the insulated electric wire for 60 seconds. After the flame was removed, the char length was measured. Samples with a char length less than 300 mm were rated excellent (AA), samples with a char length less than 400 mm were rated good (A), samples with a char length less than 450 mm were rated fair (B), and samples with a char length equal to or more than 450 mm were rated poor (F). Samples rated AA to B were pass, and samples rated F were fail. 
     (7) Comprehensive Evaluation 
     For comprehensive evaluation, samples rated AA or A in all of the tests (3) to (6) above were rated pass (AA), samples that included the B rating were also rated pass (A), and samples that included the F rating were rated fail (F). 
     The materials used indicated in Table 1 were as follows: 
     1) High-density polyethylene (HDPE) (produced by Prime Polymer Co., Ltd., tradename: HI-ZEX 5305E) (melting point: 131° C.) 
     2) Linear low-density polyethylene (LLDPE) (produced by Japan Polyethylene Corporation, tradename: NOVATEC UF420) (melting point: 123° C.) 
     3) Low-density polyethylene (LDPE) (produced by Sumitomo Chemical Co., Ltd., tradename: SUMIKATHENE F208-O) (melting point: 112° C.) 
     4) Ethylene-ethyl acrylate-maleic anhydride ternary copolymer (M-EEA) (produced by Arkema K.K., tradename: BONDINE LX4110) (melting point: 107° C.) 
     5) Ethylene-vinyl acetate copolymer (EVA) (produced by Du Pont-Mitsui Polychemicals Co., Ltd., tradename: Evaflex EV170) (melting point: 62° C.) 
     6) Ethylene-ethyl acrylate copolymer (EEA) (produced by Japan Polyethylene Corporation, tradename: REXPEARL A1150) (melting point: 100° C.) 
     7) Magnesium hydroxide (produced by Kyowa Chemical Industry Co., Ltd., tradename: KISUMA 5L) 
     8) Aluminum hydroxide (produced by Nippon Light Metal Co., Ltd., tradename: BF013STV) 
     
       
         
           
               
               
               
             
               
                   
                 TABLE 1 
               
             
            
               
                   
                   
               
               
                   
                 Examples 
                 Comparative Examples 
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Example Items 
                 1 
                 2 
                 3 
                 4 
                 5 
                 1 
                 2 
                 3 
                 4 
                 5 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Outer 
                 HDPE 1)   
                  40 
                 — 
                 — 
                  40 
                 — 
                 — 
                 — 
                 — 
                 — 
                 — 
               
               
                 layer* 
                 LLDPE 2)   
                 — 
                  40 
                 40 
                 — 
                  40 
                 — 
                 — 
                 — 
                 — 
                  40 
               
               
                   
                 LDPE 3)   
                 — 
                 — 
                 — 
                 — 
                 — 
                  40 
                 — 
                 — 
                 — 
                 — 
               
               
                   
                 M-EEA 4)   
                  30 
                  30 
                 30 
                  30 
                  30 
                  30 
                 — 
                 — 
                 — 
                  30 
               
               
                   
                 EVA 5)   
                  30 
                 — 
                 — 
                 — 
                 — 
                 — 
                 100 
                 100 
                 100 
                 — 
               
               
                   
                 EEA 6)   
                 — 
                  30 
                 30 
                  30 
                  30 
                  30 
                 — 
                 — 
                 — 
                  30 
               
               
                   
                 Magnesium 
                 150 
                 150 
                 180  
                 120 
                 — 
                 100 
                 200 
                 200 
                 200 
                 150 
               
               
                   
                 hydroxide 7 ) 
               
               
                   
                 Aluminum 
                 — 
                 — 
                 — 
                 — 
                 150 
                 — 
                 — 
                 — 
                 — 
                 — 
               
               
                   
                 hydroxide 8)   
               
               
                   
                 Other 1 (Table 2) 
                  7 
                  7 
                  7 
                  7 
                  7 
                  7 
                  7 
                  7 
                  7 
                  7 
               
               
                 Inner 
                 LLDPE 2)   
                 — 
                 100 
                 100  
                 — 
                 100 
                 100 
                 100 
                 100 
                 100 
                 100 
               
               
                 layer* 
                 Other 2 (Table 2) 
                 — 
                  12 
                 12 
                 — 
                  12 
                  12 
                  12 
                  12 
                  12 
                  12 
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Outer layer specific gravity 
                    1.44 
                    1.44 
                    1.48 
                    1.41 
                    1.44 
                    1.39 
                    1.50 
                    1.50 
                    1.50 
                    1.44 
               
               
                 Irradiation dose (Mrad) 
                  15 
                  15 
                 15 
                  15 
                  15 
                  15 
                  10 
                  20 
                  0 
                  2 
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Evaluation 
                 Tensile elastic 
                 710 
                 530 
                 600  
                 750 
                 510 
                 500 
                 150 
                 170 
                  95 
                 250 
               
               
                   
                 modulus (MPa), 
                 A 
                 A 
                 A 
                 A 
                 A 
                 A 
                 F 
                 F 
                 F 
                 F 
               
               
                   
                 500 MPa or more 
               
               
                   
                 Elongation at 
                 110 
                 120 
                 90 
                 100 
                 105 
                 130 
                 200 
                 100 
                 400 
                 170 
               
               
                   
                 break (%), 120% 
                 A 
                 A 
                 A 
                 A 
                 A 
                 F 
                 F 
                 A 
                 F 
                 F 
               
               
                   
                 or less 
               
               
                   
                 Storage elastic 
                 4 × 10 6   
                 3.3 × 10 6   
                 3.7 × 10 6   
                 4 × 10 6   
                 3.2 × 10 6   
                 3.2 × 10 6   
                 2.8 × 10 6   
                 3.0 × 10 6   
                  0 
                 2.0 × 10 5   
               
               
                   
                 modulus (Pa), 
                 A 
                 A 
                 A 
                 A 
                 A 
                 A 
                 F 
                 A 
                 F 
                 F 
               
               
                   
                 3 × 10 6  Pa or 
               
               
                   
                 more 
               
               
                   
                 Abrasion cycle 
                 400 
                 180 
                 410  
                 320 
                 165 
                 160 
                  10 
                  11 
                  2 
                  3 
               
               
                   
                 rating 
                 A 
                 A 
                 A 
                 A 
                 A 
                 A 
                 F 
                 F 
                 F 
                 F 
               
               
                   
                 Terminal 
                 A 
                 A 
                 A 
                 A 
                 A 
                 F 
                 F 
                 A 
                 F 
                 F 
               
               
                   
                 processability 
               
               
                   
                 Fusion 
                 A 
                 A 
                 A 
                 A 
                 A 
                 A 
                 F 
                 A 
                 F 
                 F 
               
               
                   
                 deformation 
               
               
                   
                 evaluation 
               
               
                   
                 Flame retardancy 
                 100 
                 200 
                 150  
                 250 
                 400 
                 300 
                  80 
                  80 
                 110 
                 250 
               
               
                   
                 test, char length 
                 AA 
                 AA 
                 AA 
                 AA 
                 B 
                 A 
                 AA 
                 AA 
                 AA 
                 AA 
               
               
                   
                 (mm) rating 
               
               
                   
                 Comprehensive 
                 AA 
                 AA 
                 AA 
                 AA 
                 A 
                 F 
                 F 
                 F 
                 F 
                 F 
               
               
                   
                 evaluation 
               
               
                   
               
            
           
         
       
     
     The unit of the contents of the components is parts by mass. 
     
       
         
           
               
               
               
               
             
               
                   
                 TABLE 2 
               
               
                   
                   
               
               
                   
                   
                   
                 Amount 
               
               
                   
                   
                   
                 added 
               
               
                   
                   
                   
                 (parts 
               
               
                   
                   
                   
                 by 
               
               
                   
                 Other additives 
                 Manufacturer 
                 mass) 
               
               
                   
                   
               
             
            
               
                   
               
            
           
           
               
               
               
               
            
               
                 Other 1 
                 IRGANOX 1010 (pentaerythritol 
                 BASF 
                 2 
               
               
                   
                 tetrakis[3-(3,5-di-tert-butyl-4- 
               
               
                   
                 hydroxyphenyl)propionate]) 
               
               
                   
                 TMPT (trimethylol propane 
                 Shin Nakamura 
                 4 
               
               
                   
                 trimethacrylate) 
                 Chemical 
               
               
                   
                 SZ-P (zinc stearate) 
                 Sakai Chemical 
                 1 
               
               
                   
                 Total 
                   
                 7 
               
               
                 Other 2 
                 IRGANOX 1010 (pentaerythritol 
                 BASF 
                 2 
               
               
                   
                 tetrakis[3-(3,5-di-tert-butyl-4- 
               
               
                   
                 hydroxyphenyl)propionate]) 
               
               
                   
                 AO-412S (2,2-bis[[3-(dodecylthio)- 
                 ADEKA 
                 1 
               
               
                   
                 1-oxopropyloxy]methyl]- 
               
               
                   
                 1,3-propanediyl bis[3- 
               
               
                   
                 (dodecylthio)propionate] 
               
               
                   
                 CDA-6 (decamethylenedicarboxylic 
                 ADEKA 
                 4 
               
               
                   
                 acid disalicyloylhydrazide) 
               
               
                   
                 TMPT (trimethylol propane 
                 Shin Nakamura 
                 4 
               
               
                   
                 trimethacrylate) 
                 Chemical 
               
               
                   
                 SZ-P (zinc stearate) 
                 Sakai Chemical 
                 1 
               
               
                   
                 Total 
                   
                 12 
               
               
                   
               
            
           
         
       
     
     Table 1 shows that samples of Example 1 to 4 were rated AA or A in all tests and thus were rated pass (AA) in the comprehensive evaluation. Samples of Example 5 were rated B in flame retardancy test and A in all other tests, and thus were rated pass (A) in the comprehensive evaluation. 
     The results of Comparative Examples 1 to 5 described in Table 1 were as follows. 
     In Comparative Example 1, the elongation at break exceeded 120%, and thus the terminal processability was rated fail (F). Thus, the comprehensive evaluation was fail (F). 
     In Comparative Example 2, the tensile elastic modulus was less than 500 MPa, the elongation at break exceeded 120%, and the storage elastic modulus at 125° C. was less than 3×10 6  Pa. Thus, all the ratings except for the rating in the flame retardancy test were fail (F). Thus, the comprehensive evaluation was fail (F). 
     In Comparative Example 3, the tensile elastic modulus was less than 500 MPa and thus the abrasion cycle was rated fail (F). Thus, the comprehensive evaluation was fail (F). 
     In Comparative Example 4, the insulating layer was not crosslinked, the tensile elastic modulus was less than 500 MPa, the elongation at break exceeded 120%, and the storage elastic modulus at 125° C. was less than 3×10 6  Pa. Thus, the ratings were all fail except for the flame retardancy test. The comprehensive evaluation was fail (F). 
     In Comparative Example 5, the tensile elastic modulus was less than 500 MPa, the elongation at break exceeded 120%, and the storage elastic modulus at 125° C. was less than 3×10 6  Pa. Thus, the ratings were all fail (F) except for the flame retardancy test. The comprehensive evaluation was fail (F). 
     Although the invention has been described with respect to specific exemplary embodiments for complete and clear disclosure, the appended claims are not to be thus limited but are to be construed as embodying all modifications and alternative constructions that may occur to one skilled in the art which fairly fall within the basic teaching herein set forth. 
     Further, it is noted than Applicant&#39;s intent is to encompass equivalents of all claim elements, even if amended later during prosecution.