JP2008240061A - Ornament - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide an ornament having high hardness, high resistance to scratches, and high corrosion resistance, prevented from being scratched and corroded by impact, and having a gold color tone. <P>SOLUTION: On the surface of the ornament composed of a soft base material, as an initial layer, a metal layer composed of one or more kinds of metals selected from Hf, Ti and Zr and a first alloy layer are formed, next, as a first layer with a modulated structure, a second alloy layer composed of one or more kinds of metals selected from Hf, Ti and Zr and different from the first alloy layer and a third alloy layer composed of one or more kinds of metals selected from Hf, Ti and Zr and different from the second alloy layer are alternately stacked thereon, and further, as a second layer with a modulated structure, an Au alloy layer and a fourth alloy layer composed of one or more kinds selected from Hf, Ti and Zr are alternately stacked thereon, and a hardened layer with a multilayer stacked structure where the outermost surface layer is the Au alloy layer is formed, thus the ornament having high hardness, high resistance to scratches, and high corrosion resistance, prevented from being scratched and corroded by impact, and having a gold color tone is attained. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  The present invention relates to a decorative part having a gold-colored hardened layer containing gold on the surface.

  For watch exterior parts such as watch bands, watch cases, bezels, back covers, braces, buckles and crowns, and decorative parts such as earrings, earrings, rings, glasses frames, pendants, brooches, necklaces and bracelets, Stainless steel, Ti, Ti alloy, and the like, which are soft base materials that can be easily processed, are widely used. However, it has been pointed out that a deterioration in the appearance quality due to the generation of scratches during use of decorative parts made from these soft substrates is a major problem. This is mainly due to the fact that the surface hardness of the soft substrate itself is a Vickers hardness and a low hardness of about Hv = 200, and various surface hardening treatments have been attempted with the aim of solving the problem.

  In addition, watch exterior parts such as the above watch band, watch case, bezel, back cover, bracelet, buckle and crown, and decorative parts such as earrings, earrings, rings, glasses frames, pendants, brooches, necklaces and bracelets Is required to have high decorative performance and appearance quality, and various surface hardening treatment techniques have been attempted to ensure a particularly high-quality golden color tone.

  As a method for curing a soft substrate, there are a method of forming a film on the surface of the soft substrate and a method of curing the soft substrate itself.

  Examples of the method for forming a golden film on the surface of the soft substrate include wet plating and ion plating. In particular, Au plating, Au—Ni plating, Au—Pd plating, and the like are widely used for decorative parts, but any of the plating films is soft and has not yet been solved. In ion plating, a method of coating a titanium nitride film or the like can be mentioned, but the titanium nitride film has high internal stress, so there is a drawback that adhesion is difficult and peeling easily occurs, both of which are problems with film peeling. On the other hand, it has not yet been fully resolved. Further, when peeling occurs, the soft material itself is exposed, and corrosion occurs at this portion, making it impossible to use as a part.

  As methods for curing decorative parts made of materials such as stainless steel, Ti and Ti alloys, ion implantation, ion nitriding, gas nitriding, etc. are known, but in any case, the curing time is long and productivity is difficult. In addition, since the processing temperature is high, the crystal grains of the decorative part are coarsened to cause surface roughness, and the appearance quality is greatly deteriorated. In particular, the problem of surface roughness is serious, and when a decorative part subjected to mirror polishing is subjected to gas nitriding treatment or carburizing treatment, crystal grains on the surface of the decorative part after the treatment are coarsened and the surface roughness is 200 to 300 μm. The generated mirror surface disappears, and even if post-polishing is performed, the mirror surface state before the carburizing process cannot be recovered, and the appearance quality is significantly lowered and deteriorated.

  Further, as a golden decorative part, 94.0 to 98.5 wt% Au, 1.0 to 3.0 wt% Fe, 0.5 to 3.3 on a nitride composed of at least one element of Ti, Zr, Hf, and Ta. An Au alloy finishing layer composed of three elements of 0 wt% Pd has been proposed (see, for example, Patent Document 1 or Patent Document 2), but this achieves a gold decorative part that does not cause metal allergy and ensures an Au color tone. For the purpose, Fe and Pd are added, and no mention is made of hardness and strength. When the authors conducted a follow-up test, only a low-hardness film having a Hv of 250 or less could be obtained.

Japanese Patent No. 3244952 (Claim 1) JP 2001-294955 A (Claim 1)

  The object of the present invention is a decorative part made of a soft base material such as stainless steel, Ti and Ti alloy, and has a high hardness, high scratch resistance and no corrosion, and no corrosion occurs during use. Is to provide.

  As a result of examining various surface treatments in order to solve the above-mentioned problems in the present invention, by having a hardened layer containing Au on the surface of a decorative part made of a soft base material such as stainless steel, Ti and Ti alloy, A high-hardness, scratch-resistant, corrosion-resistant, and gold-colored decorative part that does not cause scratches is achieved.

  As a result of various studies on the structure of the hardened layer, it was found that a hardened layer having a golden color tone can be effectively formed by adopting the structure described below.

  It is to form a hardened layer having a multilayer laminated structure composed of an initial layer, a first modulation structure layer and a second modulation structure layer on the surface of a decorative part made of a soft base material such as stainless steel, Ti and Ti alloy. Specifically, the initial layer is a metal layer made of one or more kinds of metals selected from Hf, Ti, and Zr, and a nitride layer or carbonitride layer of the same metal as the metal constituting the metal layer. The first alloy layer is formed, and then the first modulation structure layer is made of a nitride layer or carbonitride layer made of one or more metals selected from Hf, Ti, and Zr and different from the first alloy layer. The second alloy layer and a third alloy layer made of a metal nitride layer or a carbonitride layer made of one or more metals selected from Hf, Ti, and Zr and different from the second alloy layer are alternately arranged. After the lamination, an Au alloy layer as a second modulation structure layer, and a nitride layer or carbonitride layer that is made of one or more metals from Hf, Ti, and Zr and is different from the third alloy layer. The fourth alloy layer is alternately laminated, and the outermost layer is an Au alloy layer It is to make it the hardened layer of the multilayer laminated structure which is. Further, in order to obtain a hardened layer having higher hardness and scratch resistance, the Au alloy layer should be an alloy containing Au—Ni alloy, Au—Pd alloy, Au—Pt alloy, Au—Cu alloy as a main component. preferable. The decorative parts are preferably watch exterior parts, earrings, earrings, rings, glasses frames, pendants, necklaces, bracelets and brooches.

(Function)
There are various types of hardened layers mainly composed of gold alloys, all of which are characterized by no mechanical corrosion even when immersed for a long time in acid or alkali, and higher mechanical strength than pure Au. In addition, adhesion between multilayer films in which nitride layers such as HfN, TiN, and ZrN and Au alloy layers are alternately and repeatedly stacked is good, and peeling does not occur. The present invention solves the above problems by utilizing these characteristics. That is, as the initial layer, a metal layer made of one or more kinds of metals from Hf, Ti, and Zr, and a first alloy layer that is a nitride layer or carbonitride layer of the same metal as the metal constituting the metal layer And then, as the first modulation structure layer, a second alloy layer made of a nitride layer or a carbonitride layer made of one or more metals selected from Hf, Ti, and Zr and different from the first alloy layer And a third alloy layer made of a metal nitride layer or a carbonitride layer made of one or more metals selected from Hf, Ti, and Zr and different from the second alloy layer. Further, an Au alloy layer and a fourth alloy layer made of one or more kinds of metal nitride layers or carbonitride layers of Hf, Ti, and Zr are alternately stacked as the second modulation structure layer. Forms a hardened layer with a multi-layer structure with the outermost layer being an Au alloy layer In Rukoto, is even more high hardness, high scratch resistance of the cured layer is formed, high hardness, high scratch resistance which scratches due to the impact is not generated, it is the high corrosion resistance of the decorative part is achieved.

  As described above, according to the present invention, on the surface of a decorative part made of a soft base material such as stainless steel, Ti and Ti alloy, a metal made of one or more kinds of metals among Hf, Ti and Zr as an initial layer. And a first alloy layer which is a nitride layer or carbonitride layer of the same metal as the metal constituting the metal layer, and then, as a first modulation structure layer, one of Hf, Ti and Zr A second alloy layer comprising a nitride layer or carbonitride layer different from the first alloy layer and comprising at least one kind of metal; and a second alloy comprising at least one kind of metal selected from Hf, Ti and Zr. After alternately laminating a third alloy layer made of a metal nitride layer or carbonitride layer different from the layer, an Au alloy layer as a second modulation structure layer, and Hf, Ti, Zr From one or more metal nitride layers or carbonitride High hardness that does not cause scratches due to impact and does not cause corrosion by forming a hardened layer with a multilayer laminated structure in which the outermost layer is an Au alloy layer by alternately stacking fourth alloy layers made of physical layers High-scratch-resistant and high-corrosion-resistant decorative parts with gold color tone are achieved, and there is a special effect as a surface hardening method for decorative parts.

  In addition, the present invention is characterized in that an initial layer, a first modulation structure layer, a second modulation structure layer, and a hardened layer having a multilayer laminated structure are formed on the surface of the decorative part. Compared to a multi-layered structure in which nitride layers or carbonitride layers and Au alloy layers are alternately laminated repeatedly, and the outermost layer is terminated with an Au alloy layer, since only two or three layers are laminated in the structure layer. Since the thickness of the layer is small, it is possible to greatly reduce the amount of Au used, and to make the decorative part manufacturing cost cheaper.

  After processing a base material made of materials such as stainless steel, Ti and Ti alloy into a base material having various decorative part shapes, a metal layer of Hf, Ti or Zr in an arbitrary inert gas plasma as an initial layer; Forming a first alloy layer which is a nitride layer or carbonitride layer of the same metal as the metal constituting the metal layer in a gas plasma atmosphere in which a nitrogen component or a carbon component is contained in an arbitrary inert gas; Next, the first modulation structure layer is made of one or more metals out of Hf, Ti, and Zr in a gas plasma atmosphere in which an arbitrary inert gas contains a nitrogen component or a carbon component, and is different from the first alloy layer. A second alloy layer made of nitride or carbonitride and a nitride layer or carbonitride layer made of a metal different from the second alloy layer made of one or more kinds of metals from Hf, Ti, and Zr Third After alternately laminating the alloy layers, an Au alloy layer as a second modulation structure layer in a gas plasma atmosphere in which a nitrogen component or a carbon component is further contained in an arbitrary inert gas, and Hf, Ti, Zr A step of forming a hardened layer having a multilayer laminated structure in which an outermost layer is an Au alloy layer by alternately laminating a fourth alloy layer made of one or more kinds of metal nitride layers or carbonitride layers from among them. By adopting this method, a high hardness and corrosion resistant decorative part that does not cause corrosion due to impact and does not occur can be achieved. Details of the invention are illustrated in the following examples.

(First embodiment)
In the present embodiment, a metal layer as an initial layer and a first alloy layer are formed in a mixed gas plasma atmosphere of Ar and nitrogen in an Ar gas plasma atmosphere, and then in a mixed gas plasma atmosphere of Ar and nitrogen. The first modulation structure layer having a structure in which the second alloy layer and the third alloy layer are laminated, and the structure in which the Au alloy layer and the fourth alloy layer are laminated, and the outermost layer is an Au alloy layer. A method of forming a hardened layer having a multilayer laminated structure including a certain second modulation structure layer was adopted.

Example 1
A first embodiment of the present invention will be described with reference to the drawings. FIG. 1 is a schematic cross-sectional view showing a hardened layer structure of a decorative part 2 made of an arbitrary base material. Arbitrary substrate 2 is placed in a vacuum device, and after evacuating the vacuum device, Ar is introduced to generate Ar gas plasma, and Ti is used in a plasma atmosphere in which the pressure is maintained at 0.2 Pa. A Ti layer is formed as a metal layer 4 constituting the initial layer 8 on the surface of an arbitrary substrate 2 by DC sputtering, and then a first alloy layer is introduced in a mixed gas plasma of Ar and nitrogen by introducing nitrogen gas. No. 6, a TiN layer was formed. Next, an HfN layer as the second alloy layer 10 and a TiN layer as the third alloy layer 12 constituting the first modulation structure layer 14 were alternately laminated by DC sputtering in the same gas plasma atmosphere at the same pressure. Further, an Au—Ni alloy layer and an HfN layer as the fourth alloy layer 18 are alternately laminated as the Au alloy layer 16 constituting the second modulation structure layer 20, and the outermost layer is the Au alloy layer 16. A cured layer was formed. The total thickness of the initial layer 8 composed of the Ti layer that is the metal layer 4 and the TiN layer that is the first alloy layer 6 is 0.8 μm, and the HfN layer that is the second alloy layer 10 is 0. Five layers of 0.02 μm (20 nm) and four layers of TiN layers 0.02 μm (20 nm) as the third alloy layer 12 are alternately stacked, and the total of the first modulation structure layers is 0.18 μm, and further, an Au alloy Three Au-Ni alloy layers as the layer 16 were stacked at 0.01 μm (10 nm) and two HfN layers as the fourth alloy layer 18 were alternately stacked at 0.01 μm (10 nm). However, since the film thickness of the Au—Ni alloy layer which is the outermost Au alloy layer 16 is 0.02 μm (20 nm), the total of the second modulation structure layers is 0.06 μm, and the total set film thickness is 1 The film formation time was adjusted so as to be 0.04 μm. A watch case made of Ti was used as an arbitrary base material 2. An Au—Ni alloy having an arbitrary composition was used for the Au alloy layer 16.

(Example 2-18)
In the same manner as in Example 1, after evacuating the vacuum apparatus, Ar was introduced to generate Ar gas plasma, and Ti was used in a plasma atmosphere in which the pressure was maintained at 0.20 Pa. A Ti layer was formed on the surface of the substrate 2 as a metal layer constituting the initial layer, and then a nitrogen gas was introduced to form a TiN layer as a first alloy layer in a mixed gas plasma of Ar and nitrogen. Next, an HfN layer or a ZrN layer as the second alloy layer constituting the first modulation structure layer and a TiN layer as the third alloy layer were alternately laminated by DC sputtering in the same gas plasma atmosphere at the same pressure. Further, an Au—Ni alloy layer as an Au alloy layer constituting the second modulation structure layer and an HfN layer or a ZrN layer, which is the same nitride layer as the second alloy layer, are alternately laminated as a fourth alloy layer. A hardened layer having a multilayer laminated structure in which the surface layer was an Au alloy layer was formed. The total thickness of the initial layer composed of the Ti layer as the metal layer and the TiN layer as the first alloy layer was set to 0.80 μm. The number of layers of the second alloy layer and the third alloy layer is appropriately adjusted to an arbitrary value between 2 and 5, and the total thickness of the first modulation structure layers is 0.10 μm to 0.18 μm. Adjusted. Further, the number of Au alloy layers and the fourth alloy layer is appropriately adjusted to an arbitrary value between 1 and 3, and the thickness of the outermost Au alloy layer is set to 0.02 μm. The total film thickness of the two modulation structure layers is adjusted to 0.03 μm to 0.06 μm, and the film formation time is set so that the total set film thickness is an arbitrary value between 0.93 μm and 1.04 μm. Was adjusted to form a film. For the decorative parts, watch exterior parts such as a watch case, a watch band, a watch bezel and a back cover were used. Ti, Ti alloy, SUS316L and SUS317L were used as the base material of the watch exterior part. An Au-Ni alloy having an arbitrary composition was adopted for the Au alloy layer.

(Comparative Example 1-16)
As Comparative Example 1-16 of the embodiment of the present invention, a watch case made of Ti, Ti alloy, SUS316L and SUS317L, a watch band, a watch bezel, an Au—Ni film and an Au—Pd film on the surface of the back cover by a wet plating method. Formed.

  Tables 1 to 3 show the results of the hardness test, the wear resistance test, the corrosion resistance test, and the overall evaluation results of the watch exterior parts obtained in Example 1-18 and Comparative Example 1-16 of the first embodiment. .

The composition of the first alloy layer, the second alloy layer, the third alloy layer, the fourth alloy layer and the Au alloy layer, which are nitride layers, was specified by performing an EPMA (X-ray microanalysis) analysis. The hardness was measured with a micro Vickers hardness meter at a load of 5 mN, and Vickers hardness Hv = 1500 or more was regarded as acceptable. In the abrasion resistance test, a wear test was performed with a wear tester NUS-ISO-2 manufactured by Suga Abrasion Test Co., Ltd., and the test surface after the test was analyzed with EPMA, and the base substrate surface that was not exposed was accepted. . In the corrosion resistance test, the sample was dipped in a CASS test solution for 48 hours, and no corrosion occurred at all. Those that passed all these three items were regarded as acceptable in the comprehensive evaluation results.

A specific wear test method using a wear tester NUS-ISO-2 manufactured by Suga Abrasion Test Co., Ltd. is a test piece with a hardened layer surface facing downward on a flat test piece made of the same base material as the decorative part. It fixes to the opening part of a test piece mounting base with a holding plate and a test piece holding screw. The abrasive paper is then attached to the wear wheel. An upward load that presses the abrasive paper against the test piece is applied to the wear wheel by a balance mechanism. Thereafter, the specimen mounting base is reciprocated by a mechanism that converts the rotational movement of the motor into a reciprocating movement, and the wear wheel is rotated by an angle of 0.9 ° for each reciprocation of the specimen mounting base. This rotation always makes contact with a new, unworn area of the abrasive paper with the test piece attached to the wear wheel. The number of reciprocations of the test mounting table can be automatically set, and the wear tester stops at the set number of reciprocations. A lapping film (# 1200 with alumina particles having a particle diameter of about 12 μm on the film surface) was used as the abrasive paper attached to the wear ring. The contact load between the test piece and the abrasive paper was 100 gf, and the number of reciprocating motions of the test piece mounting base was 50 times.

As shown in Tables 1 and 2, on the surface of the watch exterior part made of Ti, Ti alloy, and stainless steel (SUS316L, SUS317L), the initial layer made of the metal layer and the first alloy layer, the second alloy layer and the third A first modulation structure layer having a structure in which the alloy layers are stacked; a second modulation structure layer having a structure in which the Au alloy layer and the fourth alloy layer are stacked; and the outermost layer being an Au alloy layer; A cured layer having a multilayer laminated structure consisting of All of these Examples 1-18 passed the hardness test when the Vickers hardness was Hv = 1690 or more, passed the wear resistance test without passing through the base substrate surface after the wear test, and passed the CASS even in the corrosion resistance test. Corrosion did not occur after the test and the test was successful. Therefore, in the comprehensive evaluation, all of Examples 1-18 passed.

  On the other hand, when the Au-Ni plating film is formed on the surface of the watch exterior part made of Ti, Ti alloy, stainless steel (SUS316L, SUS317L) of Comparative Example 1-8 by the wet plating method, the corrosion does not occur after the CASS test. Although it did not occur and passed, in the abrasion resistance test, the substrate surface was exposed after the wear test and was rejected. In the hardness test, the Vickers hardness was Hv = 680 or less and was rejected. Further, in the corrosion resistance test, corrosion does not occur after the CASS test in which the Au-Pd plating film is formed on the surface of the watch exterior part made of Ti alloy and stainless steel (SUS316L, SUS317L) of Comparative Example 9-16. Although it was acceptable, the abrasion resistance test was rejected because the underlying substrate surface was exposed after the abrasion test, and the hardness test was also rejected because the Vickers hardness was as low as Hv = 540 or less. Therefore, the overall evaluation was that all the comparative examples failed.

(Second Embodiment)
Similarly to the first embodiment, the present embodiment also continues after the metal layer as the initial layer and the first alloy layer are formed in the mixed gas plasma atmosphere of He and nitrogen in the He gas plasma atmosphere. A first modulation structure layer having a structure in which a second alloy layer and a third alloy layer are laminated in a mixed gas plasma atmosphere of He and nitrogen, and a structure in which an Au alloy layer and a fourth alloy layer are laminated. A method of forming a hardened layer having a multi-layered structure composed of a second modulation structure layer, the outermost layer of which is an Au alloy layer, and a multilayer structure is adopted.

(Examples 19-36)
As in the first embodiment, after the inside of the vacuum apparatus is evacuated, He is introduced to generate He gas plasma, and the surface of the decorative part is subjected to DC sputtering in a plasma atmosphere maintained at a pressure of 0.15 Pa. After forming a metal layer consisting of an Hf layer, Ti layer or Zr layer as an initial layer, nitrogen gas is introduced and the same metal as the metal constituting the metal layer in a mixed gas plasma atmosphere of He and nitrogen at the same pressure After forming a first alloy layer such as an HfN layer, a TiN layer, or a ZrN layer, the first modulation structure layer is a nitride layer different from the first alloy layer, such as an HfN layer, a TiN layer, or a ZrN layer. A second alloy layer such as a layer and a third alloy layer such as an HfN layer, a TiN layer, or a ZrN layer different from the second alloy layer were alternately stacked. Furthermore, as the second modulation structure layer, an Au alloy layer and a fourth alloy layer such as an HfN layer, a TiN layer, and a ZrN layer are alternately laminated to form a hardened layer having a multilayer laminated structure in which the outermost layer is an Au alloy layer. I let you. The film thickness was a set value, and the total of the initial layer composed of the metal layer and the first alloy layer was 0.80 μm. The number of layers of the second alloy layer and the third alloy layer is appropriately adjusted to an arbitrary value between 2 and 5, and the total thickness of the first modulation structure layers is 0.10 μm to 0.18 μm. Adjusted. Further, the number of Au alloy layers and the fourth alloy layer is appropriately adjusted to an arbitrary value between 1 and 3, and the thickness of the outermost Au alloy layer is set to 0.02 μm. The total film thickness of the two modulation structure layers is adjusted to 0.03 μm to 0.06 μm, and the film formation time is set so that the total set film thickness is an arbitrary value between 0.93 μm and 1.04 μm. Was adjusted to form a film. For the decorative parts, watch exterior parts such as a watch case, a watch band, a watch bezel and a back cover were used. Ti, Ti alloy, SUS316L and SUS317L were used as the base material of the watch exterior part. In addition, an Au—Pd alloy, Au—Pt alloy, or Au—Cu alloy having an arbitrary composition was adopted for the Au alloy layer.

  Tables 4 and 5 show the results of the hardness test, the wear resistance test, the corrosion resistance test, and the comprehensive evaluation results of the watch exterior parts obtained in Examples 19-36 of the second embodiment. The first alloy layer, the second alloy layer, the third alloy layer, the composition of the fourth alloy layer and the Au alloy layer, the hardness test, the adhesion test, the corrosion resistance test, and the comprehensive evaluation results are all the first implementation. The same evaluation criteria as the evaluation criteria evaluated in the form were adopted.

As shown in Tables 4 and 5, on the surface of the watch exterior part made of Ti, Ti alloy, and stainless steel (SUS316L, SUS317L), the initial layer made of the metal layer and the first alloy layer, the second alloy layer, and the third A first modulation structure layer having a structure in which the alloy layers are stacked; a second modulation structure layer having a structure in which the Au alloy layer and the fourth alloy layer are stacked; and the outermost layer being an Au alloy layer; A cured layer having a multilayer laminated structure consisting of All of these Examples 19-36 passed in the hardness test when the Vickers hardness was Hv = 1695 or more, passed in the wear resistance test without passing through the base material surface after the wear test, and passed in the corrosion resistance test. Corrosion did not occur after the test and the test was successful. Therefore, in the comprehensive evaluation, all of Examples 19 to 36 passed.

(Third embodiment)
Similarly to the first embodiment, in the present embodiment, the metal layer as the initial layer and the first alloy layer in the mixed gas plasma atmosphere of Ar and nitrogen or carbon are formed in an Ar gas plasma atmosphere. Subsequently, a first modulation structure layer having a structure in which a second alloy layer and a third alloy layer are laminated in a mixed gas plasma atmosphere of Ar and nitrogen or carbon, an Au alloy layer, and a fourth alloy layer are provided. A method of forming a hardened layer having a multilayer laminated structure comprising a second modulation structure layer having a laminated structure and an outermost layer being an Au alloy layer was employed.

(Examples 37-56)
As in the first embodiment, after the vacuum apparatus is evacuated, Ar is introduced to generate Ar gas plasma, and the surface of the decorative part is subjected to DC sputtering in a plasma atmosphere maintained at a pressure of 0.20 Pa. After forming a metal layer composed of an Hf layer, Ti layer or Zr layer as an initial layer, nitrogen gas or methane gas is introduced to form a metal layer in a mixed gas plasma atmosphere of Ar and nitrogen or methane gas at the same pressure After forming a first alloy layer such as a HfN layer, a ZrN layer, or a TiCN layer made of the same metal as TiN layer, TiCN, which is an alloy layer different from the first alloy layer as the first modulation structure layer A second alloy layer such as a layer and a third alloy layer such as an HfN layer, a ZrN layer, or a TiCN layer different from the second alloy layer were alternately stacked. Further, an Au alloy layer as the second modulation structure layer and a TiCN layer as the fourth alloy layer were alternately laminated to form a hardened layer having a multilayer structure in which the outermost layer was an Au alloy layer. The film thickness was a set value, and the total of the initial layer composed of the metal layer and the first alloy layer was 0.90 μm. The number of layers of the second alloy layer and the third alloy layer is appropriately adjusted to an arbitrary value between 2 and 5, and the total thickness of the first modulation structure layer is 0.05 μm to 0.14 μm. Adjusted. Further, the number of Au alloy layers and the fourth alloy layer is appropriately adjusted to an arbitrary value between 1 and 3, and the thickness of the outermost Au alloy layer is set to 0.02 μm. The total film thickness of the two modulation structure layers is adjusted to 0.03 μm to 0.06 μm, and the total film thickness is set to an arbitrary value between 0.98 μm and 1.10 μm. Was adjusted to form a film. For the decorative parts, watch exterior parts such as a watch case, a watch band, a watch bezel and a back cover were used. Ti, Ti alloy, SUS316L and SUS317L were used as the base material of the watch exterior part. In addition, an Au—Ni alloy, Au—Pd alloy, Au—Pt alloy, or Au—Cu alloy having an arbitrary composition was adopted for the Au alloy layer.

  Tables 6 and 7 show the results of the hardness test, the wear resistance test, the corrosion resistance test, and the overall evaluation results of the watch exterior parts obtained in Examples 37-56 of the third embodiment. The first alloy layer, the second alloy layer, the third alloy layer, the composition of the fourth alloy layer and the Au alloy layer, the hardness test, the adhesion test, the corrosion resistance test, and the comprehensive evaluation results are all the first implementation. The same evaluation criteria as the evaluation criteria evaluated in the form were adopted.

As shown in Tables 6 and 7, on the surface of the watch exterior part made of Ti, Ti alloy, stainless steel (SUS316L, SUS317L), an initial layer composed of a metal layer and a first alloy layer, a second alloy layer and a third A first modulation structure layer having a structure in which the alloy layers are stacked; a second modulation structure layer having a structure in which the Au alloy layer and the fourth alloy layer are stacked; and the outermost layer being an Au alloy layer; A cured layer having a multilayer laminated structure consisting of All of these Examples 37-56 passed in the hardness test when the Vickers hardness was Hv = 1765 or more, passed in the wear resistance test without passing through the base substrate surface after the wear test, and passed in the corrosion resistance test. Corrosion did not occur after the test and it passed, and therefore, the overall evaluation was that all of Examples 37 to 56 passed.

(Fourth embodiment)
Similarly to the first embodiment, in the present embodiment, the metal layer as the initial layer and the first alloy layer in the mixed gas plasma atmosphere of Ar and nitrogen or carbon are formed in an Ar gas plasma atmosphere. Subsequently, a first modulation structure layer having a structure in which a second alloy layer and a third alloy layer are laminated in a mixed gas plasma atmosphere of Ar and nitrogen or carbon, an Au alloy layer, and a fourth alloy layer are provided. A method of forming a hardened layer having a multilayer laminated structure comprising a second modulation structure layer having a laminated structure and an outermost layer being an Au alloy layer was employed.

(Examples 37-56)
As in the first embodiment, after the vacuum apparatus is evacuated, Ar is introduced to generate Ar gas plasma, and the surface of the decorative part is subjected to DC sputtering in a plasma atmosphere in which the pressure is kept at 0.27 Pa. After forming a Ti layer as a metal layer as an initial layer, a first alloy such as a TiN layer or a TiCN layer is introduced in a mixed gas plasma atmosphere of Ar and nitrogen or methane gas at the same pressure by introducing nitrogen gas or methane gas After forming the layer, the second alloy layer, such as a TiCN layer, an HfCN layer, a ZrCN layer, or the like, which is an alloy layer different from the first alloy layer as the first modulation structure layer, Third alloy layers such as different TiN layers and TiCN layers were alternately stacked. Further, an Au alloy layer as the second modulation structure layer and an HfCN layer, a ZrCN layer, and a TiCN layer as the fourth alloy layer are alternately laminated to form a hardened layer having a multilayer structure in which the outermost layer is an Au alloy layer. The total thickness of the initial layer composed of the metal layer and the first alloy layer was set to 0.90 μm. The number of layers of the second alloy layer and the third alloy layer is appropriately adjusted to an arbitrary value between 2 and 5, and the total thickness of the first modulation structure layer is 0.05 μm to 0.14 μm. Adjusted. Further, the number of Au alloy layers and the fourth alloy layer is appropriately adjusted to an arbitrary value between 1 and 3, and the thickness of the outermost Au alloy layer is set to 0.02 μm. The total film thickness of the two modulation structure layers is adjusted to 0.03 μm to 0.06 μm, and the total film thickness is set to an arbitrary value between 0.98 μm and 1.10 μm. Was adjusted to form a film. For the decorative parts, watch exterior parts such as a watch case, a watch band, a watch bezel and a back cover were used. Ti, Ti alloy, SUS316L and SUS317L were used as the base material of the watch exterior part. In addition, an Au—Ni alloy, Au—Pt alloy, or Au—Cu alloy having an arbitrary composition was adopted for the Au alloy layer.

  Tables 6 and 7 show the results of the hardness test, the wear resistance test, the corrosion resistance test, and the overall evaluation results of the watch exterior parts obtained in Examples 57 to 76 of the fourth embodiment. The first alloy layer, the second alloy layer, the third alloy layer, the composition of the fourth alloy layer and the Au alloy layer, the hardness test, the adhesion test, the corrosion resistance test, and the comprehensive evaluation results are all the first implementation. The same evaluation criteria as the evaluation criteria evaluated in the form were adopted.

As shown in Table 8 and Table 9, on the surface of the watch exterior part made of Ti, Ti alloy, stainless steel (SUS316L, SUS317L), the initial layer made of the metal layer and the first alloy layer, the second alloy layer and the third A first modulation structure layer having a structure in which the alloy layers are stacked; a second modulation structure layer having a structure in which the Au alloy layer and the fourth alloy layer are stacked; and the outermost layer being an Au alloy layer; A cured layer having a multilayer laminated structure consisting of All of these Examples 57-76 passed in the hardness test when the Vickers hardness was Hv = 1770 or more, passed in the wear resistance test without exposure of the underlying substrate surface after the wear test, and also in the corrosion resistance test CASS Corrosion did not occur after the test and the test was successful. Therefore, the overall evaluation was that of Examples 57-76.

  Although Ti, Ti alloy, SUS316L, and SUS317L are used as the base material in each embodiment, the base material is not limited to these and can be applied to materials made of various stainless steels, various Ti alloys, and the like.

  The DC sputtering method was adopted as a means for evaporating the metal and the Au alloy, but this was adopted because the alloy composition can be easily controlled, and it is not necessary to limit to the DC sputtering method. The DC magnetron sputtering method, RF Any sputtering method such as magnetron sputtering, RF sputtering, or DC sputtering may be used. In addition to the sputtering method, other PVD methods such as an ion plating method and an ion beam deposition method may be adopted as long as the process is a dry process. Similarly, the plasma generation means may employ either the RF method or the DC method.

  As the pressure condition of the gas plasma for forming the hardened layer, the pressure is 0.20 Pa in the first embodiment and the third embodiment, the pressure is 0.15 Pa in the second embodiment, and the pressure is 0 in the fourth embodiment. However, the pressure of the gas plasma need not be limited to the same condition, and the pressure may be any numerical value as long as the gas plasma can be generated.

  In the first embodiment, the third embodiment, and the fourth embodiment, Ar is used as the inert gas, and He is used as the inert gas in the second embodiment, but the inert gas generates plasma. Therefore, it is not limited to Ar and He, and may be replaced with another inert gas such as Xe or Kr.

It is a cross-sectional schematic diagram which shows the hardening layer structure of the decorative component which is one Embodiment of the decorative component of this invention.

Explanation of symbols

2 decorative parts 4 metal layer 6 first alloy layer 8 initial layer 10 second alloy layer 12 third alloy layer 14 first modulation structure layer 16 Au alloy layer 18 fourth alloy layer 20 second modulation structure layer

Claims (3)

A decorative part having a hardened layer on a surface, wherein the hardened layer has an initial layer, a first modulation structure layer, and a second modulation structure layer, and the initial layer is one of Hf, Ti, and Zr. A metal layer having the above metal, and a first alloy layer made of the same metal nitride layer or carbonitride layer as the metal constituting the metal layer on the metal layer; The modulation structure layer is composed of a nitride layer or carbonitride layer of one or more metals from Hf, Ti, or Zr, a second alloy layer that is different from the first alloy layer, and Hf, Ti, or Zr. The second alloy layer is composed of one or more kinds of metals and a third alloy layer made of a metal nitride layer or carbonitride layer different from the second alloy layer, and the second alloy layer The modulation structure layer is composed of an Au alloy layer and one of Hf, Ti, or Zr. The fourth alloy layer are laminated alternately decorative component outermost layer is Au alloy layer made of a nitride layer or carbonitride layer above the metal kind. The first alloy layer, the second alloy layer, the third alloy layer, or the fourth alloy layer is HfN, TiN, ZrN, HfCN, TiCN, or ZrCN. Decorative parts. The decorative part according to claim 1 or 2, wherein the Au alloy layer is mainly composed of an Au-Ni alloy, an Au-Pd alloy, an Au-Pt alloy, or an Au-Cu alloy.

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