Sliding member
10288118 ยท 2019-05-14
Assignee
Inventors
Cpc classification
F16C2240/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/264
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T428/12993
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T428/12917
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T428/12458
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C33/124
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C23C30/00
CHEMISTRY; METALLURGY
Y10T428/1291
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T428/263
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C2360/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/12882
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C2204/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/273
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C2223/44
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/24967
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T428/27
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C2204/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B15/015
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/265
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
C23C28/36
CHEMISTRY; METALLURGY
F16C33/121
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/12924
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B32B15/20
PERFORMING OPERATIONS; TRANSPORTING
B22D27/045
PERFORMING OPERATIONS; TRANSPORTING
F16C2202/50
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/12903
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B22D13/023
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/2495
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16C33/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16C33/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B15/01
PERFORMING OPERATIONS; TRANSPORTING
F16C33/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22D13/02
PERFORMING OPERATIONS; TRANSPORTING
C23C30/00
CHEMISTRY; METALLURGY
B32B15/20
PERFORMING OPERATIONS; TRANSPORTING
B22D27/04
PERFORMING OPERATIONS; TRANSPORTING
C23C28/00
CHEMISTRY; METALLURGY
C23C28/02
CHEMISTRY; METALLURGY
Abstract
Provided is a sliding material including a substrate; and a copper alloy layer bonded to the substrate. The copper alloy includes 2.0 to 15.0% by mass of tin. The copper alloy layer includes a sliding body part including a sliding surface, and a gradient region including a bond surface with the substrate. A tin concentration in the gradient region reduces from the sliding body part toward the bond surface. A method for producing the siding material is also provided. The method includes preparing the substrate having a first surface and a second surface opposite to the first surface; melting the copper alloy; casting the molten copper alloy on the first surface of the substrate; and solidifying the copper alloy unidirectionally by cooling the substrate from the second surface by a coolant.
Claims
1. A sliding material comprising: a substrate; and a copper alloy layer bonded to the substrate, the copper alloy comprising 2.0 to 15.0% by mass of tin, wherein the copper alloy layer comprises a gradient region including a bond surface with the substrate, and a sliding body part including a surface opposite to the bond surface, wherein a tin concentration in the gradient region reduces from the sliding body part toward the bond surface, and wherein a ratio of tin concentration in the gradient region is 0.1 to 0.8 by mass percentage.
2. The sliding material according to claim 1, wherein the ratio is 0.2 to 0.6.
3. The sliding material according to claim 1, wherein the copper alloy comprises, by mass, 2.0 to 15.0% of tin, 0 to 30.0% of Bi, not more than 5.0% in total of one or more elements selected from a group consisting of Al, Zn, Mn, Si, Ni, Fe, P, Zr, Ti and Mg, and the balance of copper and inevitable impurities.
4. The sliding material according to claim 1, wherein the copper alloy includes at least one of MoS.sub.2 or graphite, and either or both of the MoS.sub.2 and the graphite is equal to or less than 10.0% by volume.
5. The sliding material according to claim 1, further comprising an overlay on the copper alloy layer.
6. The sliding material according to claim 1, wherein the substrate has a thickness of 1.0 to 25.0 mm and the copper alloy layer has a thickness of 0.1 to 3.0 mm.
7. The sliding material according to claim 1, wherein the gradient region has a thickness of 10 to 50 m.
8. A sliding member comprising the sliding material according to claim 1.
9. A bearing device comprising the sliding member according to claim 8 and a shaft.
10. A method for producing the siding material according to claim 1, comprising: preparing the substrate having a first surface and a second surface; melting the copper alloy; casting the molten copper alloy on the first surface of the substrate; and solidifying the copper alloy unidirectionally by cooling the substrate from the second surface by a coolant.
11. The method according to claim 10, wherein further comprising a step of reducing a feeding amount of the coolant after a predetermined time period from the casting.
12. The method according to claim 10, wherein the coolant is water or oil.
13. The method according to claim 10, wherein the step of preparing the substrate comprises forming a cylindrical body from one or more substrate materials, and the step of casting comprises casting the molten copper alloy in an inner surface of the cylinder body while rotating the cylindrical body on a central axis of the cylinder.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
DETAIL DESCRIPTION OF THE INVENTION
(7)
(8) The copper alloy layer 3 can act as a sliding layer having a sliding surface 8. The copper alloy layer 3 may include tin in an amount of 2.0 to 15.0 mass % of a total mass of the copper alloy. The copper alloy may include, other than Sn, 0 to 30.0 mass % of Bi, and not more than 5.0 mass % in total of one or more elements selected from the group of Al, Zn, Mn, Si, Ni, Fe, P, Zr, Ti and Mg. The copper alloy may further include not more than 10.0 volume % of either or both of MoS.sub.2 and graphite. The copper alloy may further include dispersed particles of hard materials, such as boride, silicide, oxide, nitride or carbide of a metal element, or intermetallic compounds.
(9) Preferably, the substance of the sliding material has a thickness of 1.0 to 25.0 mm and the copper alloy layer has a thickness of 0.1 to 3.0 mm.
(10) Furthermore, the sliding material 1 according to the invention may include an overlay on the copper alloy layer 3. The overlay may be made of a known material, for example, soft metal material such as Sn or Bi, or a resin with dispersed solid lubricant. Even when the overlay is applied, the surface of the copper alloy layer 3, on which the overlay is applied, is referred to as sliding surface.
(11)
(12) Generally, a copper alloy including tin has high strength due to solid-solution strengthening of tin and/or deposition of intermetallic compounds of tin, and thus has high seizer resistance and wear resistance as well as good sliding properties, while the alloy has small toughness. On the other hand, a copper alloy including a smaller tin concentration has smaller strength but has better toughness or ductility.
(13) As the tin concentration reduces from the sliding body par 6 toward the bond surface 7 in the gradient region 5, its strength becomes smaller while toughness and ductility become greater. Accordingly, the gradient region 5 acts as a stress relaxation layer which prevents stress concentration on the bond surface 7. A load by solidification contraction and a shear stress during sliding are reduced to prevent the concentrate on the bond surface 7 and the gradient region 5 improves bonding strength. For this reason, the sliding material 1 maintains the sliding properties, seizure resistance and wear resistance of the copper alloy including tin and has improved bonding strength between the copper alloy layer 3 and the substrate 2.
(14) Since the copper alloy layer 3 and the substrate 2 are directly bonded with each other in the sliding material 1 and there is no need to use expensive copper-plated steel material, a cost of the sliding material 1 can be low.
(15) In order to function as the stress relaxation layer, a thickness of the gradient region 5 is preferably not less than 5 m. When the thickness is not less than 5 m, the load and the shear stress efficiently distribute in the layer and the bonding strength can be improved. The thickness of the gradient region 5 is more preferably not less than 10 m, and further more preferably not less than 15 m. If the thickness of the gradient region 5 is too great, a whole strength of the copper alloy layer 3 is decreased. Thus, the upper limit of the thickness is preferably 50 m. The thickness of the gradient region 5 is more preferably not more than 40 urn, and further more preferably not more than 30 m.
(16) Since an area within 50 m from the bond surface 7 in the gradient region 5 especially functions as the stress relaxation layer, a reduction rate of tin concentration within the area is important. Therefore, the tin concentration decrease within 50 m from the bond surface 7 is preferably such that a ratio of the maximum tin concentration, by mass %, to the minimum tin concentration is 0.1 to 0.8, more preferably 0.2 to 0.6. Typically, the maximum tin concentration appears at a position at an interface with the sliding body part 6 and the minimum tin concentration appear at a position in a vicinity of the bond surface 7 with the substrate. Therefore, the ratio of the tin concentration at the vicinity of the bond surface 7 with the substrate 2 in relation to the tin concentration at the interface with the sliding body 6 is preferably 0.1 to 0.8, more preferably 0.2 to 0.6. Herein, this ratio of the tin concentration in the gradient region 5 is referred to as ratio of tin concentration or the tin concentration ratio.
(17) Next, a composition of the copper alloy is explained.
(18) Sn: 2.0 to 15.0 mass %
(19) Tin (Sn) functions to strengthen the copper alloy by solid-solution-strengthening a copper matrix of the copper alloy or by forming intermetallic compounds, and thus tin improves wear resistance. Tin also improves corrosion resistance and sliding properties. When the tin content is less than 2.0 mass %, these effects are insufficient. When the tin content exceeds 15.0 mass %, the copper alloy becomes too hard to deteriorate the sliding properties and the alloy becomes brittle and loses toughness. Therefore, the tin content is determined to be 2.0 to 15.0 mass %.
(20) Bi: 0 to 30.0 mass %
(21) Bismuth (Bi) forms a soft bismuth phase dispersed in the copper alloy matrix and contributes to improve wear resistance and seize resistance. However, when the bismuth content exceeds 30.0 mass %, strength of the copper alloy tends to decrease, since bismuth itself has low strength. Preferably, the bismuth content is 8.0 to 25.0 mass %.
(22) One or more elements selected from the group of Al, Zn, Mn, Si, Ni, Fe, P, Zr, Ti and Mg: not more than 5.0 mass % in total
(23) These elements function to strengthen the copper alloy by solid-solution-strengthening a copper alloy matrix or by forming intermetallic compounds. Therefore, when the content of these elements is not more than 5.0 mass %, they contribute to strengthen the sliding material. When the content is greater, toughness of the copper tends to decrease since much intermetallic compounds precipitate. Thus, the upper limit is preferably 5.0 mass %. More preferably, the content is 0.1 to 1.1 mass %.
(24) The copper alloy may include a solid lubricant. Either or both of MoS.sub.2 and graphite may be further included up to 10.0 volume %. The solid lubricant can improve wear resistance and seize resistance of the copper alloy. When an amount of the solid lubricant exceeds 10.0 volume %, strength of the copper alloy decreases. Thus, not more than 10.0 volume % is preferable. Not more than 5.0 volume % is more preferable, and 0.5 to 2.5 volume % is further more preferable.
(25) The copper alloy may further include hard particles up to 10.0 volume %. An amount of the hard particles is preferably 0.5 to 2.5 volume %. Preferably, the hard particles may have a size of 1 to 45 m. The hard particles may be a boride, a silicide, an oxide, a nitride or a carbide of a metal, or an intermetallic compound. The hard particles can improve wear resistance. They may be dispersed in e.g. Bi phase in the copper layer to improve the wear resistance and seizure resistance
(26) Next, a method for producing the sliding material 1 according to the present invention is explained. In the present invention, a molten copper alloy having the above composition is cast on a substrate 2. The molten alloy is thus contacted directly with the substrate 2 to be solidified. Thus, the sliding material 1 is produced by bonding the copper alloy layer 3 with the substrate 2 by a casting method.
(27) First, the substrate 2 is prepared. The substrate 2 may be of a shape of a flat plate or a cylinder made of the above-explained material. However, other shape may be employed.
(28) The copper alloy having the above-explained composition is melted and cast on a surface of the substrate 2 to be bonded. It is preferable to conduct the step in an inert gas or in a reduced atmosphere or to use flux in order to prevent oxidation.
(29) The substrate 2 is cooled by a coolant from a surface of the substrate opposite to the bonded surface with the copper alloy layer 3. The coolant may be e.g. water or oil. The water or oil is collided with the substrate 2 from the surface opposite to the bonded surface to cool the substrate 2.
(30) When the copper alloy is thus cast and cooled, the molten copper alloy is solidified unidirectionally from a portion that first contacts the substrate 2. In the embodiments, cooling is not conducted from a free surface side of the copper alloy layer (a surface opposite to the bonded surface of the copper alloy layer).
(31) Since a bronze alloy has a wide temperature range of solidification, the present invention utilizes micro segregation of tin in the alloy. In the method, the solidification starts from a portion of the molten copper alloy that contacts the substrate 2 and copper (a phase) is deposited as a primary crystal in a near region with the surface of the substrate. At the time, tin, which is another component of the bronze, remains in a liquid phase and moves from the bond surface side into the liquid phase. As a result, when cooling conditions is appropriately adjusted, the formed copper alloy layer 3 has a gradient region in which a tin concentration is relatively small at the bond surface 7 between the copper alloy 3 and the substrate 2.
(32) Accordingly, since the copper alloy is unidirectionally solidified from the bond surface with the substrate 2 under a controlled cooling rate or a cooling time period, the alloy near the bond surface is rapidly cooled and solidified while the alloy near the sliding surface 8 opposite to the bonded surface is slowly cooled. In this way, the inclination of the tin concentration near the bond surface is formed.
(33) Also, since the casting method can produce a matrix by melting the whole alloy, a lining of the copper alloy by the casting method can achieve a sufficient strength as the copper alloy layer than a method of sintering a powder.
(34) In the present invention, the controlled structure can be achieved by controlling an amount of fed coolant to the surface of the substrate 2 opposite to the bond surface.
(35) As an embodiment of conducting the method, dams may be built on a base plat and a molten copper alloy may be poured in an area on the base plate and surrounded by the dams. It is preferable to conduct in an inert gas or in a reducing atmosphere, or use flux to prevent oxidation of the base and the copper alloy. The cooling by the coolant is conducted form the back side of the substrate (the base plate) as described above.
(36) In another embodiment, centrifugal casting may be applied. Needless to say, the present invention is not limited by these casting methods.
(37)
(38) Then, explained is a method of measuring the gradient region in the copper alloy layer at the bond surface with the substrate. A sectional structure of the sliding material is observed with an electron microscope (for example, at 1000 magnifications) and a distribution of tin is measured along a direction perpendicular to the sliding surface or a thickness direction in the vicinity of the bond surface of the copper alloy layer with the substrate and by a line analysis or an area analysis with EDX. Since the tin concentration of a sliding body part is substantially same as that of the whole copper alloy which forms the copper alloy layer 3, the gradient region is determined as an area in which the tin concentration decreases from the constant value in the sliding body part toward the bond surface.
EXAMPLES
(39) Examples 1 to 21 of the invention and comparison examples 1 to 5 were produced and the gradient region and the bonding strength were evaluated.
(40) Preparation of the Substrate
(41) A plate made of a steel SPCC was used as a substrate, and an upper surface of the steel plate was scraped at a central area with remaining all side to produce an open box-shape which has dams at all sides to prevent leakage of a molten alloy. A thickness for the cast was designed to be 5 mm. A thickness of an area to become the substrate of the sliding material was designed to be 6 mm. The surface of the substrate was covered by molten borax as an antioxidant, and the substrate was preheated at a temperature of 1000 to 1200 C. in a reducing H.sub.2 gas atmosphere.
(42) Casting of the Copper Alloy
(43) Pure copper, pure tin, and other component material/materials were blended according to the compositions of the copper alloys of Examples 1 to 21 and Comparative Examples 1 to 5 in tables 1 and 2, and were melted in an air. The molten alloys were kept at a temperature of 1100 to 1200 C. in an air and poured on the preheated substrate.
(44) Cooling Process
(45) After the pouring, cooling water was collided with a bottom of the substrate from water spray nozzles located below the substrate. For Comparative Examples, a small amount of cooling water was collided continuously (flow rate of the cooling water was 40 L/min, and a cooling time period was 180 seconds). On the other hand, for Examples 1 to 7 and 13 to 21, intentionally discontinuous two-stage cooling was conducted as shown in
(46) Method of Evaluating Tin Concentration Ratio
(47) EPMA device (type: JXA-8530F FIELD EMISSION ELECTRON PROBE MICROANALYZER, JEOL) was used to observe a view field of a cross section of 85 m and 116 m of each sample. An image was taken such that the bond surface becomes along the 116 m direction. A line analyze was conducted by EDS of the EPMA device and the tin distribution in the vicinity of the bond surface was measured. A ratio of tin accounts obtained by the line analyze was evaluated as the tin concentration ratio. The images were taken more than 10 areas for each sample.
(48) Measurement of Bonding Strength
(49) The bonding strength between the copper alloy layer and the substrate was evaluated by a ratio of shear strength between the copper alloy and the substrate in relation to tensile strength of the copper alloy (shear strength/tensile strength). Since the shear strength correlates to the tensile strength, the ratio between the shear strength and the tensile strength was made an index of the bonding strength, thereby materials having different compositions can be compared.
(50) A test piece for measuring the shearing strength was processed as shown in
(51) Table 1 shows the measurement results of whether the gradient region was observed or not, the thickness (m) of the gradient region if it exists, the ratio of the tin concentration in the gradient region, and the bonding strength (shear strength/tensile strength) in the columns, respectively, Presence or absence of gradient region, Thickness of gradient region (m), Ratio of tin concentration and Shear strength/Tensile strength. Please note that if the gradient region was not observed, the Ratio of tin concentration indicates a ratio of the tin concentration at the vicinity of the bond surface in relation to that at 50 m distant from the bond surface.
(52) As described above, the cooling condition for Comparative Examples 1 to 5, that for Examples 1 to 7, and that for Example 8 to 12 are different with one another. From the results in Table 1, the gradient region was not observed in the Comparative examples for which two-stage cooling condition was not applied. However, the gradient region was observed in all Examples of the invention. Between samples having same tin content, they have much different ratios of tin concentration according to the cooling conditions, and Examples 8 to 12 which were subjected to most strong cooling have the smallest ratio. Thus, adjusting of the cooling condition can achieve the ratio of tin concentration of not more than 0.8, furthermore not more than 0.6, regardless of the tin content.
(53) In the cooling condition for Comparative Examples 1 to 5, the gradient region was not observed, and reduction of the tin concentration at the vicinity of the bond surface was not observed in some samples.
(54) In the cooling condition for Examples 1 to 7, the ratio of tin concentration was almost constant between the samples regardless of their tin contents. However, in the condition for Examples 8 to 12, the ratio of tin concentration tends to reduce as the tin content increases.
(55) The shear strength of Examples 1 to 12, which have the ratio of tin concentration of not more than 0.8, have the ratio of shear strength to tensile strength of not less than 0.76. These values were much greater than those of Comparative examples 1 to 5.
(56) TABLE-US-00001 TABLE 1 Composition Presence or Thickness of (mass %) absence of gradient Ratio of tin Shear strength/ No. Cu Sn gradient region region (m) concentration Tensile strength Example 1 balance 2.2 presence 14 0.75 0.84 Example 2 balance 5.3 presence 18 0.68 0.82 Example 3 balance 5.2 presence 4 0.79 0.76 Example 4 balance 5.1 presence 57 0.73 0.81 Example 5 balance 8.4 presence 23 0.72 0.86 Example 6 balance 12.8 presence 21 0.77 0.79 Example 7 balance 15.0 presence 38 0.77 0.79 Example 8 balance 2.2 presence 20 0.48 0.91 Example 9 balance 5.3 presence 29 0.29 0.91 Example 10 balance 8.4 presence 15 0.37 0.89 Example 11 balance 12.8 presence 21 0.55 0.88 Example 12 balance 15.0 presence 22 0.22 0.88 Comparative balance 2.2 absence 1.02 0.71 Example 1 Comparative balance 5.3 absence 0.89 0.63 Example 2 Comparative balance 8.4 absence 0.95 0.67 Example 3 Comparative balance 12.8 absence 0.98 0.60 Example 4 Comparative balance 15.0 absence 1.09 0.57 Example 5
(57) Examples 13 to 21 includes other elements (Bi, Zn, Al, Fe, Ni, Mn, Si, P, Zr, Ti, Mg), or hard particles of Mo.sub.2C or solid lubricant particles of graphite (Gr) in addition to the composition (Cu about 8% tin) of Example 5. Cooling condition for Examples 13 to 21 was same as that for Example 5.
(58) Table 2 shows test results. Even though the element/particle is added, the ratio of tin concentration were in a range of 0.64% to 0.79%, which is equivalent to 0.72 of Example 5. Thus, the bonding strength (shear strength/tensile strength) was 0.76 to 0.87, which is equivalent to 0.86 of Example 5. The results show that the added element/elements or particles have only a small effect on the ratio of tin concentration and to the bonding strength.
(59) TABLE-US-00002 TABLE 2 Presence or absence Thickness Shear strength/ Composition (mass % or volume %*) of gradient of gradient Ratio of tin Tensile No. Cu Sn others region region (m) concentration strength Example 5 balance 8.4 presence 23 0.72 0.86 Example 13 balance 7.8 Bi: 24.8 presence 28 0.64 0.77 Example 14 balance 7.4 Zn: 3.1 presence 42 0.75 0.82 Example 15 balance 8.0 Al: 1.5, Fe: 1.0 presence 11 0.72 0.84 Example 16 balance 8.1 Ni: 0.9 presence 22 0.74 0.81 Example 17 balance 8.1 Mn: 1.5, Si: 0.5 presence 19 0.69 0.79 Example 18 balance 7.6 Fe: 1.0, P: 0.15 presence 24 0.67 0.76 Example 19 balance 9.0 Zr: 0.05, Ti: 0.05, presence 19 0.79 0.87 Mg: 0.05 Example 20 balance 8.0 Mo2C: 1.5 volume % presence 20 0.70 0.81 Example 21 balance 7.3 Gr: 1.0 volume % presence 31 0.65 0.76 Comparative balance 8.4 absence 0.95 0.67 Example 3 *The composition is represented by mass % except explicitly expressed as volume %.