This application claims priority from Japanese Patent Application No. 2016-174243 filed on Sep. 7, 2016, the entire contents of which are incorporated herein by reference.
Field of the Invention
The present invention relates to a shielded wire and a wire harness.
Description of Related Art
Conventionally, a shield braid configured by braiding metal coated fibers in each of which a metal film is formed on the outer circumference of a refractory fiber, copper members made of copper or a copper alloy being placed between a plurality of metal coated fibers constituting the braid, at a constant thickness has been proposed (see Patent Literature 1: JP-A-2013-110053). According to the shield braid, while high bendability is realized by the metal coated fibers, the grounding process is enabled by the copper members to be easily performed, and, when the thickness of the copper members is made adequate, the bendability can be prevented from being lowered by an excessive thickness of the copper members.
[Patent Literature 1] JP-A-2013-110053
According to a related art, in a shield braid, no consideration is given to a sheath which is disposed on an outer circumference of the shield braid, and, even when the shield braid itself has a high bendability, there is a possibility that the bendability may be lowered by the influence of the sheath. In the case where the shield braid is bent, for example, the degree of freedom is lost because of the contractile force of the sheath, and therefore there is a possibility that the wires may be broken at an early stage. In such a case, the shielding performance is lowered, and the bending resistance of the whole of the shielded wire including the sheath cannot be improved.
One or more embodiments provide a shielded wire and a wire harness in which bending resistance can be improved.
In accordance with one or more embodiments, a shielded wire includes an electrical wire including a conductor portion and a covering portion, a shield braid in which electrically conductive wire members are braided, and which covers an outer circumference of the electrical wire, and a tubular sheath disposed on an outer circumference of the shield braid and made of an insulating resin,
wherein D1 is an inner diameter of the sheath in a state where the sheath is disposed on the outer circumference of the shield braid,
wherein t is a thickness of the sheath in the state where the sheath is disposed on the outer circumference of the shield braid,
wherein E is a modulus of elasticity of the sheath,
wherein μA is a coefficient of static friction between the shield braid and the electrical wire,
wherein μB is a coefficient of static friction between the shield braid and the sheath,
wherein Fmax is a value of a load which, in a fatigue test where a load is repeatedly applied to the shield braid in an axial direction of the braid, is obtained when an electrical resistance value of the shield braid is increased by 10% with respect to an initial value at a timing when the load is repeatedly applied 5 million times,
wherein D2 is an inner diameter of the sheath in a free state, and
wherein D2 satisfies following relational expression (1).
According to one or more embodiments, the inner diameter D2 of the sheath in the free state satisfies the above-described relational expression, and therefore it is possible to reduce the possibility that the constriction of the shield braid is excessively enhanced by contraction of the sheath, and the electrically conductive wire member is broken before 5 million endurance cycles. Therefore, the bending resistance of the whole shielded wire can be improved.
In the wire harness of one or more embodiments, the wire harness may include the above mentioned shielded wire.
The wire harness includes the shielded wire in which the bending resistance is improved, and therefore also the bending resistance of the whole wire harness can be improved.
According to one or more embodiments, it is possible to provide a shielded wire and wire harness in which the bending resistance can be improved.
Exemplary embodiments are described with reference to the drawings. This invention is not limited to the below-described embodiment. The embodiment can be adequately changed without departing from the spirit of the invention. Although, in the below-described embodiment, illustrations and descriptions of partial configurations are omitted, it is matter of course that, with respect to the details of the omitted techniques, known or well-known techniques are applied within the range where no inconsistency occurs with the contents of the following description.
Each of the metal strands has a diameter of 0.05 mm to 0.12 mm. Since the strand diameter is 0.05 mm or larger, the strands are not excessively thin, and the possibility that the wire is broken as a result of repeated bending can be reduced. Since the strand diameter is 0.12 mm or smaller, moreover, the flexibility can be ensured (distortion due to bending can be reduced), and the possibility that the wire is broken as a result of repeated bending can be reduced. That is, also the above-described range of the diameter of each of the metal strands enables the electrical wire 10 to have a structure of high bendability.
The shield braid 20 is configured by knitting 48 plated fiber bundles (an example of the electrically conductive wire member) in which metal plating is performed on tensile strength fibers, and covers the outer circumference of the electrical wire 10. Here, the tensile strength fibers are fibers in which the fibrous material is produced by chemical synthesis from raw materials such as petroleum, the tensile strength at break is 1 GPa or higher, and the elongation rate at break is 1% or larger and 10% or smaller. Examples of such fibers are aramid fibers, polyarylate fibers, and PBO fibers. The metal plating is configured by a metal such as copper or tin.
Specifically, for example, the tensile strength fibers are polyarylate fibers (φ is 0.022 mm, and the number of filaments is 300), and the metal plating is configured by stacking copper and tin layers in this sequence starting from the lower layer, and has a thickness of 2.4 μm, on each fiber.
The sheath 30 is a tubular member made of an insulating resin which is disposed on the outer circumference of the shield braid 20, and has a certain degree of stretchability. The sheath 30 is configured by polyethylene, ethylene-propylene rubber (hereinafter referred to as EPDM rubber), or the like. In the state (the inner diameter is D1) where the sheath is disposed on the outer circumference of the shield braid 20, the inner diameter is increased as compared with that in the free state (the inner diameter is D2 (D2<D1)). That is, the sheath 30 is caused by the own contractile force to be in close contact with the shield braid 20.
In the embodiment, here, the inner diameter D2 of the sheath 30 in the free state satisfies following Relational expression (1):
In the above expression, D1 is the inner diameter of the sheath 30 in the state where the sheath is disposed on the outer circumference of the shield braid 20, t is the thickness of the sheath 30 in the state where the sheath is disposed on the outer circumference of the shield braid 20, E is the modulus of elasticity of the sheath 30, μA is the coefficient of static friction between the shield braid 20 and the electrical wire 10, and μB is the coefficient of static friction between the shield braid 20 and the sheath 30. Moreover, Fmax is a value of a constant load which, in a fatigue test where a load is repeatedly applied to the shield braid 20 in the axial direction of the braid, is obtained when the resistance of the shield braid 20 is increased by 10% with respect to the initial value at timing when the load is repeatedly applied 5 million times.
When the inner diameter D2 of the sheath 30 in the free state is set to have a value in the range which is obtained from the above expression, it is possible to reduce the possibility that the constriction of the shield braid 20 is excessively enhanced by contraction of the sheath 30, and the plated fibers are broken before 5 million endurance cycles, and therefore the bending resistance of the whole shielded wire 1 can be improved. Hereinafter, this will be described in detail.
In the fatigue test, firstly, a constant load F was repeatedly applied until the resistance of the plated fiber bundle was increased by 10% with respect to the initial value. Namely, a cycle in which the constant load F is applied and then the load is reduced to 0 N was repeatedly performed. The applied load can be expressed as a sinusoidal wave, and the test was performed at a frequency of 10 Hz.
As shown in
Moreover, in the case where the applied constant load F was about 103 N, when the load was repeatedly applied about 20,000 times, the resistance of the plated fiber bundle was increased by 10% with respect to the initial value, and, in the case where the applied constant load F was about 70 N, when the load was repeatedly applied about 100,000 times, the resistance of the plated fiber bundle was increased by 10% with respect to the initial value. In the case where the applied constant load F was 35 N, when the load was repeatedly applied thirty-five million times, the resistance of the plated fiber bundle was increased by 10% with respect to the initial value. When the above measurement results are linearly approximated, it is possible to express the relationship of the applied constant load and the number of cycles which were performed until the resistance was increased by 10% with respect to the initial value.
In the plated fiber bundle used in the example of
As shown in
The pulling mechanism 130 pulls one end of the plated fiber bundle S. The pulling mechanism 130 gradually increases the tensile load, and measures the force (static friction force) at a timing when the plated fiber bundle S is moved.
As described with reference to
In the shielded wire 1 in which the same shield braid 20 as in the example of
As described with reference to
In the shielded wire 1 in which the same shield braid 20 as in the example of
As described with reference to
In the shielded wire 1 in which the same shield braid 20 as in the example of
When an internal pressure p is applied to a cylinder (the Young's modulus is E) in which the radius is R (=D1/2), and the thickness is t, the radius increase ΔR (=(D1−D2)/2) is given by the following expression:
Based on Expression (2) above and the maximum allowable value of the sheath internal pressure which has been described with reference to
The above is summarized in that the allowable inner diameter D2max of the sheath 30 functioning as a stand-alone tube can be expressed by following Expression (3):
Since, in addition to Expression (3) above, the sheath 30 is disposed on the shield braid 20, D2≥D1 never occurs, because, if D2≥D1 occurs, a clearance exists between the shield braid 20 and the sheath 30, and this causes the sheath 30 to wrinkle or crack. Therefore, Relational expression (1) above indicating the range of D2 is derived.
Next, an example and a comparative example will be described. Table 1 below shows shielded wires of the example and the comparative example, and results of 5 million-cycle fatigue tests. In the fatigue tests of Table 1, a bending test apparatus shown in
In the shielded wire of the example, polyehylene was used in the covering portion of the wire, and the sheath. The coefficient (μA, μB) of static friction of polyehylene is 0.4, and the modulus of elasticity E of the sheath is 40 MPa. The thickness t of the sheath is 1 mm, and the inner diameter D1 of the sheath which covers the shield braid is 13.1 mm. The shield braid is identical with that of the embodiment shown in
In the shielded wire of the comparative example, polyehylene was used in the covering portion of the wire, and EPDM rubber was used in the sheath. The coefficient (μA) of static friction of polyehylene is 0.4, the coefficient (μB) of static friction of EPDM rubber is 0.65, and the modulus of elasticity E of the sheath is 10 MPa. The thickness t of the sheath is 2.8 mm, and the inner diameter D1 of the sheath which covers the sheath braid is 13.1 mm. The shield braid is identical with that of the embodiment shown in
In the shielded wire of the example, the inner diameter D2 of the sheath in the free state is 12.8 mm, and therefore larger than 12.3 mm which is D2max. Consequently, the sheath internal pressure is not excessively raised, and the possibility of wire breakage can be reduced without causing the degree of freedom of the shield braid in the case where the shield braid is bent, to be lowered by the contractile force of the sheath. As a result, it is possible to obtain a shielded wire having a bending resistance of 5 million times.
In the shielded wire of the comparative example, by contrast, the inner diameter D2 of the sheath in the free state is 11 mm, and therefore smaller than 12.3 mm which is D2max. Consequently, the sheath internal pressure is excessively raised, and the degree of freedom of the shield braid in the case where the shield braid is bent is lowered by the contractile force of the sheath, thereby increasing the possibility of wire breakage. As a result, a shielded wire which does not have a bending resistance of 5 million times is obtained.
In the shielded wire 1 of the embodiment, as described above, the inner diameter D2 of the sheath 30 in the free state satisfies Relational expression (1) above, and therefore the possibility that the constriction of the shield braid 20 is excessively increased by contraction of the sheath 30, and plated wires are broken before 5 million endurance cycles can be reduced. Therefore, the bending resistance of the whole shielded wire 1 can be improved.
When the wire harness WH includes the shielded wire 1 having the improved bending resistance, moreover, also the bending resistance of the whole wire harness can be improved.
Although the invention has been described with reference to the embodiment, the invention is not limited to the embodiment. Changes may be made to the embodiment without departing from the spirit of the invention, or the embodiment may be combined with other techniques (including well-known and known techniques).
In the case of such a twisted wire in which a plurality of electrical wires 10 are twisted, the inner diameter D1 of the sheath 30 disposed on the shield braid 20 is equal to a value which is obtained by adding the thickness of the shield braid to the twist diameter of the twisted wire.
Although the number of the electrical wires 10 shown in
Number | Date | Country | Kind |
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2016-174243 | Sep 2016 | JP | national |
Number | Name | Date | Kind |
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4970352 | Satoh | Nov 1990 | A |
20090126993 | Nishimura | May 2009 | A1 |
20110036613 | Hayashishita | Feb 2011 | A1 |
20150083458 | Tanaka | Mar 2015 | A1 |
Number | Date | Country |
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2013-110053 | Jun 2013 | JP |
Number | Date | Country | |
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20180068763 A1 | Mar 2018 | US |