JPH0447021B2 - - Google Patents
Info
- Publication number
- JPH0447021B2 JPH0447021B2 JP57086235A JP8623582A JPH0447021B2 JP H0447021 B2 JPH0447021 B2 JP H0447021B2 JP 57086235 A JP57086235 A JP 57086235A JP 8623582 A JP8623582 A JP 8623582A JP H0447021 B2 JPH0447021 B2 JP H0447021B2
- Authority
- JP
- Japan
- Prior art keywords
- sintered alloy
- phase
- decorative
- sintered
- alloys
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Description
本発明は、時計用外装部品、ネクタイピン、ブ
ローチ、釣り具部品の装飾品用部材に適した装飾
性と耐食性を兼ね備えた装飾用焼結合金に関す
る。
従来、装飾品用部材には、耐食性及び耐スクラ
ツチ性が要求されることから硬質合金であるWC
基、TaC基及びTiC基焼結合金が実用化されてい
る。この内、WC基及びTaC基焼結合金は、高価
である上に比重が高く携帯用装飾品としては不向
きであり、WC基及びTiC基焼結合金は、黒灰色
の単調な色彩であるため装飾効果に対する要求を
完全に満していないと云う欠点がある。この欠点
を補うものとして、TiNおよび/またはTiCを鋼
及び焼結合金に被覆した被覆合金が装飾品用部材
として使用されている。しかし被覆合金は、被覆
層の表面と内部の色調が異なつたり、被覆層の剥
離が生じたり、製造工程から生じる被覆層の膜質
及び膜厚の変化により被覆合金表面に色調むらが
起り装飾品としての価値がなくなると云う欠点が
ある。更に有色系焼結合金としてTiN系を主体
とした焼結合金が装飾品用部材として多数提案さ
れるいるが焼結性が非常に悪く、焼結性の悪い合
金を鏡面光沢の表面状態にして使用する場合、鏡
面にある欠陥が目立つために装飾品用部材には適
さないという問題がある。
本発明の装飾用焼結合金は、上述したような欠
点及び問題点を解決したものである。
本発明は、化学量論組成近傍のTiNを主原料
としたものとFe族とから成る圧粉体を焼結する
過程で、TiNがFe族に固溶してFe族固体溶体を
形成する際、Fe族中にTiとNは等モルで固溶で
きず約95%の窒素はN2ガスとして圧粉体外に排
出されるため液相出現以後は、このN2ガスが残
留して焼結性の促進を阻害する現象が起り、この
現象に基づいて脱窒防止に対する検討を行つた結
果得られた装飾用焼結合金である。
本発明の装飾用焼結合金は、Fe,Ni,Co,
Cr,Mo,Wの中から選ばれた1種以上の結合相
が2〜30重量%と金属、合金又は化合物から成る
強化相が0.1〜10重量%と残りが
(Tia,Mb)(NW,CX,OY)Zで表わされる硬
質相(但し、MはZr,Hf,V,Nb,Ta,Crの
中から選ばれた1種以上、aはTiの原子比、b
はMに相当する金属の原子比を示し、a+b=
1、1≧a≧0.4、0.6≧b≧0、Nは窒素、Cは
炭素、Oは酸素、W、X、Yは窒素、炭素、酸素
それぞれの原子比、Zは金属に対する非金属構成
元素の比を示し、W+X+Y=1、X+Y>0、
1>W≧0.4、0.5≧X≧0、0.6≧Y≧0.06、0.93
≧Z≧0.6)と不可避不純物とから成る焼結合金
である。本発明の装飾用焼結合金における強化相
がのP,Al,B,Si,Mn,Ti,Zr,Hf,V,
Nb,Ta中から選ばれた1種以上の金属又は合金
の場合は、焼結過程において結合相の液相出現温
度を低下させて焼結性の促進及び焼結合金の緻密
性を向上させるという効果と、結合相を金属間化
合物又は固溶体の状態にして焼結合金の強度、硬
さ、耐スクラツチ性及び耐食性を向上させるとい
う効果に寄与しているものである。また、強化相
がAlN,Si3N4,BN,Mo2Cの中から選ばれた1
種以上の窒化物、炭化物もしくはこれらの複化合
物の場合は、結合相と硬質相との粒界強化及び結
合強化へ作用し、その結果焼結合金の強度、耐ス
クラツチ性及び耐食性を向上させるという効果に
寄与しているものである。又、結合相中への分散
強化によつて焼結体の強度及び硬さを向上させる
効果を目的とするときには、強化相は、Al2O3、
Y2O3、ZrO2、MgO、NiO、SiO2の中から選ばれ
た1種以上の酸化物を使用することによつて焼結
体の強度、耐スクラツチ性及び耐食性の向上に寄
与することになる。更に結合相と硬質相との粒界
強化によつて硬質相と結合相との結合強化を目的
とするときには、強化相は、AlN、Si3N4、BN、
Mo2Cの中から選ばれた1種以上の窒化物、炭化
物もしくは複化合物を使用することによつて焼結
体の強度、耐スクラツチ性及び耐食性の向上に寄
与することになる。このような本発明の焼結合金
は、TiNを主体とする圧粉体を焼結する過程で
生じる脱窒が非化学量論組成であるTiNZ(0.95≧
Z≧0.6)粉末を出発原料とするために系外に排
出されていたN2ガスがTiNz粉末を逆窒化する現
象が生じ、このために脱窒が防止される。又、
Ti(NW,CX,OY)Zの如くTiNzに炭素および/ま
たは酸素が加わることによつて脱窒防止の効果が
強くなり、このために焼結性の促進が起り、緻密
な焼結体となり、焼結体の強度及び硬さが高くな
ると共に強化相の使用によつて更に焼結体の強度
及び硬さが高くなるという硬質相と強化相の相剰
効果によつて一層耐摩耗性、耐スクラツチ性及び
耐食性の優れた焼結合金となる。
本発明の装飾用焼結合金は、TiNzを主体にし
た硬質相によつて黄金色系統の色調を保持させる
ものであるがZの値が化学量論組成よりも少なく
なる程黄金色系から淡黄金色系に変化し、この色
調変化を更に黄金色を呈するTiO、ZrN、HfN、
VN、NbN、TaN、CrN、Cr2N、TaC、NbCの
1種以上を加えることによつて深みのある淡黄金
色から鮮明な黄金色までの色彩及び色調コントロ
ールが一層容易になる。
本発明の装飾用焼結合金は、真空又は非酸化性
雰囲気中で普通焼結方法により充分緻密な焼結合
金が得られるが熱間静水圧焼結方法(HIP)によ
つて処理することにより更に緻密で強度の高い焼
結合金が得られる。
次に本発明の装飾用焼結合金に於て数値限定し
た理由について述べる。
硬質相である(Tia,Mb)(NW,CX,OY)Zに
於て、Ti以外の金属Mは、硬質相の粒子成長を
抑制する効果と共に硬質相の強度及び硬さを高め
る効果もある。特に、金属Mを化合物として黄金
色を呈するCrN、ZrN、HfN、VN、NbN、
TaN、Cr2Nの中から選ばれた1種以上を添加す
る場合には、Tiの原子比aとMの原子比bとの
混合比を合金的に広く選ぶことが可能でこれを制
限する本質的な理由は無いが携帯用としての軽量
化と耐スクラツチ性を考慮する必要が有り、又、
ZrC、HfC、VC、Cr3C2等の炭化物を添加する場
合には、色彩及び色調も考慮する必要が有るため
に1≧a≧0.4、0.6≧b≧0と定めた。非金属元
素であるN、C、Oは、黄金色系統の焼結合金を
目的とするためにNを主体にし、O(酸素)は、
微量含有されることにより焼結性の促進と耐スク
ラツチ性の向上に役立ち、C(炭素)も微量含有
により同様の効果がある。O及びCの含有量が多
過ぎると焼結性が低下すると共に焼結体の硬さも
低下するので1>W≧0.4、0.5≧X≧0、0.6≧
Y0.06と定めた。尚炭素Cは、金属炭化物として
の炭素よりも遊離炭素として添加する方が焼結性
促進に対する効果が強い傾向にある。金属元素に
対する非金属元素の比を表わすZは、脱ガス防止
と焼結体の硬さ向上を目的とするために化学量論
組成よりも少なくする必要があるが逆に少な過ぎ
ると化合物が不安定になると共に焼結体の寸法精
度が低下するので0.93≧Z≧0.6と定めた。
結合相量は、硬質相量及び強化相量との関係、
更には用途によつて選定する必要があるが2重量
%未満では焼結性及び緻密性が低下し、30重量%
を越えて多くなると焼結体の硬さ低下となつて耐
スクラツチ性が悪くなるために結合相量は、2重
量%から30重量%と定めた。
強化相量は、結合相量との関係及び用途によつ
て選定する必要があるが0.1重量%未満では焼結
体の強合及び硬さの向上におよぼす効果が弱く、
10重量%を越えて多くなると焼結性が悪くなり、
焼結体も脆化するために強化相量は、0.1重量%
から10重量%と定めた。
以下に本発明の装飾用焼結合金を実施例に従つ
て具体的に説明する。
実施例 1
TiNz、TiC、TiO、Ti(Nw,Cx)z、
Ti(Nw,Oy)z、Ti(Nw,Cx,Oy)z、
(Tia,Mb)Nz、(Tia,Mb)(Nw,Cx)z、
(Tia,Mb)(Nw,Oy)z、(Tia,Mb)
(Nw,Cx,Oy)z、
各種結合相金属及び強化相、金属粉末を所定の
割合に配合し、2%のパラフインを潤滑剤として
添加した後、アセトン溶媒のボールミルにて粉砕
混合した。乾燥した混合粉末を2t/cm2の加圧力で
成形し、10-3〜10-4mmHgの真空中1400℃〜1600
℃の温度で焼結した後、必要に応じて真空中1100
℃〜1250℃の温度で3時間溶体化処理を行つた。
こうして得た焼結合金は、ダイヤモンド砥石によ
り鏡面研摩し、機械的性質、色調及び耐食性を検
討した。機械的性質は、硬度、抵抗力を測定し、
耐食性試験は、50℃の人工海水及び人工汗に7日
間各試料を浸漬した後試料鏡面部を観察すること
により行つた。各試料の配合組成、焼結条件及び
溶体化処理条件を表1に、焼結及び溶体化処理後
の各試料の硬質相の構造、結合相、抗折力、硬
さ、色調及び人工海水、人工汗による耐食性を調
査し、その結果を表2に示した。
The present invention relates to a decorative sintered alloy that has both decorative properties and corrosion resistance and is suitable for decorative parts such as watch exterior parts, tie pins, brooches, and fishing gear parts. Conventionally, materials for decorative items require corrosion resistance and scratch resistance, so WC, which is a hard alloy, has been used.
TaC-based, TaC-based, and TiC-based sintered alloys have been put into practical use. Among these, WC-based and TaC-based sintered alloys are expensive and have a high specific gravity, making them unsuitable for use as portable accessories, and WC-based and TiC-based sintered alloys have a monotonous black-gray color. The drawback is that it does not fully meet the requirements for decorative effects. To compensate for this drawback, coated alloys in which steel and sintered alloys are coated with TiN and/or TiC are used as decorative parts. However, coating alloys can be used for decorations because the color tone between the surface and inside of the coating layer may differ, the coating layer may peel off, and color tone unevenness may occur on the coating alloy surface due to changes in the quality and thickness of the coating layer that occur during the manufacturing process. The disadvantage is that it loses its value. Furthermore, many TiN-based colored sintered alloys have been proposed for decorative parts, but they have very poor sintering properties, and it is difficult to make alloys with poor sintering properties into a mirror-glossy surface. When used, there is a problem that defects on the mirror surface are noticeable, making it unsuitable for decorative parts. The decorative sintered alloy of the present invention solves the above-mentioned drawbacks and problems. In the process of sintering a compact consisting of TiN as a main raw material with a near stoichiometric composition and Fe group, when TiN dissolves in Fe group to form an Fe group solid solution, , since Ti and N cannot be dissolved in equimolar amounts in the Fe group, approximately 95% of nitrogen is discharged from the compact as N 2 gas, so after the appearance of the liquid phase, this N 2 gas remains and burns A phenomenon that inhibits the promotion of condensation occurs, and this decorative sintered alloy was obtained as a result of an investigation into preventing denitrification based on this phenomenon. The decorative sintered alloy of the present invention includes Fe, Ni, Co,
2 to 30% by weight of one or more binder phases selected from Cr, Mo, and W, 0.1 to 10% by weight of reinforcing phases consisting of metals, alloys, or compounds, and the remainder (Tia, Mb) (N W , C _
indicates the atomic ratio of the metal corresponding to M, and a+b=
1, 1≧a≧0.4, 0.6≧b≧0, N is nitrogen, C is carbon, O is oxygen, W, X, Y are the atomic ratios of nitrogen, carbon, and oxygen, and Z is the nonmetallic constituent element relative to the metal. Indicates the ratio of W+X+Y=1, X+Y>0,
1>W≧0.4, 0.5≧X≧0, 0.6≧Y≧0.06, 0.93
≧Z≧0.6) and unavoidable impurities. The reinforcing phase in the decorative sintered alloy of the present invention is P, Al, B, Si, Mn, Ti, Zr, Hf, V,
In the case of one or more metals or alloys selected from Nb and Ta, it is said that during the sintering process, the temperature at which the liquid phase appears in the binder phase is lowered, promoting sinterability and improving the compactness of the sintered alloy. This contributes to the effect of bringing the binder phase into the state of an intermetallic compound or solid solution, thereby improving the strength, hardness, scratch resistance, and corrosion resistance of the sintered alloy. In addition, the reinforcing phase is one selected from AlN, Si 3 N 4 , BN, and Mo 2 C.
In the case of more than one nitride, carbide, or a composite compound thereof, it acts to strengthen the grain boundaries and bond between the binder phase and the hard phase, thereby improving the strength, scratch resistance, and corrosion resistance of the sintered alloy. This contributes to the effectiveness. Furthermore, when the purpose is to improve the strength and hardness of the sintered body by dispersion strengthening in the binder phase, the reinforcing phase may be Al 2 O 3 , Al 2 O 3 ,
Contributing to improving the strength, scratch resistance, and corrosion resistance of the sintered body by using one or more oxides selected from Y 2 O 3 , ZrO 2 , MgO, NiO, and SiO 2 become. Furthermore, when the purpose is to strengthen the bond between the hard phase and the binder phase by strengthening the grain boundaries between the binder phase and the hard phase, the strengthening phase may be AlN, Si 3 N 4 , BN,
The use of one or more nitrides, carbides or composite compounds selected from Mo 2 C contributes to improving the strength, scratch resistance and corrosion resistance of the sintered body. In the sintered alloy of the present invention, the denitrification that occurs during the process of sintering a green compact mainly composed of TiN has a non-stoichiometric composition, TiN Z (0.95≧
Z≧0.6) Since the powder is used as a starting material, the N 2 gas discharged outside the system reversely nitrides the TiNz powder, thereby preventing denitrification. or,
The addition of carbon and/or oxygen to TiNz , such as Ti(N W , C The strength and hardness of the sintered body increases, and the use of the reinforcing phase further increases the strength and hardness of the sintered body. A sintered alloy with excellent wear resistance, scratch resistance, and corrosion resistance. The decorative sintered alloy of the present invention maintains a golden yellow color tone due to the hard phase mainly composed of TiNz, but as the Z value becomes lower than the stoichiometric composition, the color tone changes from golden yellow to pale. TiO, ZrN, HfN, which changes to a golden color, and this color change becomes even more golden
By adding one or more of VN, NbN, TaN, CrN, Cr 2 N, TaC, and NbC, it becomes easier to control the color and tone from a deep pale golden yellow to a clear golden yellow. The decorative sintered alloy of the present invention can be obtained by ordinary sintering in vacuum or in a non-oxidizing atmosphere, but it can be obtained by hot isostatic sintering (HIP). Furthermore, a denser and stronger sintered alloy can be obtained. Next, the reason for the numerical limitations in the decorative sintered alloy of the present invention will be described. In the hard phase (Tia , Mb) (N W , C It's also effective. In particular, CrN, ZrN, HfN, VN, NbN, which exhibits a golden color when metal M is compounded,
When adding one or more selected from TaN and Cr 2 N, it is possible to select a wide range of mixing ratios between the atomic ratio a of Ti and the atomic ratio b of M, and this is limited. There is no essential reason, but it is necessary to consider lightweight and scratch resistance for portable use, and
When adding carbides such as ZrC, HfC, VC, Cr3C2 , etc., it is necessary to consider color and tone, so 1≧a≧0.4 and 0.6≧b≧0 are set. The nonmetallic elements N, C, and O are mainly composed of N in order to produce a golden-colored sintered alloy, and O (oxygen) is
When contained in a small amount, it helps to promote sinterability and improve scratch resistance, and when contained in a small amount, C (carbon) has similar effects. If the content of O and C is too large, the sinterability will decrease and the hardness of the sintered body will also decrease, so 1>W≧0.4, 0.5≧X≧0, 0.6≧
Y0.06 was set. Note that carbon C tends to have a stronger effect on promoting sinterability when added as free carbon than as carbon as a metal carbide. Z, which represents the ratio of nonmetallic elements to metallic elements, needs to be less than the stoichiometric composition in order to prevent outgassing and improve the hardness of the sintered body, but if it is too small, the compound may become defective. Since the dimensional accuracy of the sintered body decreases as it becomes more stable, it is determined that 0.93≧Z≧0.6. The amount of binder phase is related to the amount of hard phase and reinforcing phase,
Furthermore, it must be selected depending on the application, but if it is less than 2% by weight, the sinterability and density will decrease, and if it is less than 30% by weight,
The amount of the binder phase was determined to be from 2% by weight to 30% by weight, since if the amount exceeds 20% by weight, the hardness of the sintered body decreases and the scratch resistance deteriorates. The amount of reinforcing phase must be selected depending on the relationship with the amount of binder phase and the application, but if it is less than 0.1% by weight, it will have a weak effect on strengthening and improving the hardness of the sintered body.
If the amount exceeds 10% by weight, sinterability will deteriorate,
Since the sintered body also becomes brittle, the amount of reinforcing phase is 0.1% by weight.
10% by weight. The decorative sintered alloy of the present invention will be specifically described below based on examples. Example 1 TiNz, TiC, TiO, Ti(Nw, Cx)z, Ti(Nw, Oy)z, Ti(Nw, Cx, Oy)z, (Tia, Mb) Nz, (Tia, Mb) (Nw, Cx)z, (Tia, Mb) (Nw, Oy)z, (Tia, Mb)
(Nw, Cx, Oy)z, Various binder phase metals, reinforcing phases, and metal powder were blended in predetermined proportions, 2% paraffin was added as a lubricant, and then pulverized and mixed in a ball mill using an acetone solvent. The dried mixed powder was molded under a pressure of 2t/cm 2 and heated at 1400°C to 1600°C in a vacuum of 10 -3 to 10 -4 mmHg.
After sintering at a temperature of 1100 °C in vacuum if necessary
Solution treatment was carried out at a temperature of 1250°C for 3 hours.
The sintered alloy thus obtained was mirror-polished using a diamond grindstone, and its mechanical properties, color tone, and corrosion resistance were examined. Mechanical properties measure hardness, resistance,
The corrosion resistance test was conducted by immersing each sample in artificial seawater and artificial sweat at 50°C for 7 days and then observing the mirror surface of the sample. The composition, sintering conditions and solution treatment conditions of each sample are shown in Table 1, and the hard phase structure, binder phase, transverse rupture strength, hardness, color tone and artificial seawater of each sample after sintering and solution treatment Corrosion resistance due to artificial sweat was investigated, and the results are shown in Table 2.
【表】【table】
【表】【table】
【表】
実施例 2
Al2O3、Y2O3、ZrO2、MgO、NiO、SiO2の各
粉末及び実施例1で使用した各原料粉末によつて
所定の割合に配合し、実施例1と同様な製造方法
で焼結し、得られた各試料の機械的性質、色調及
び耐食性試験を行つた。各試料の配合組成、焼結
条件、及び溶体化処理条件を表3に、焼結及び溶
体化処理後の各試料の硬質相の構造、結合相、強
化相、抗折力、硬さ、色調及び人工海水、人工汗
による耐食性を調査し、その結果を表4に示し
た。[Table] Example 2 Each powder of Al 2 O 3 , Y 2 O 3 , ZrO 2 , MgO, NiO, SiO 2 and each raw material powder used in Example 1 were mixed in a predetermined ratio, and the Each sample was sintered using the same manufacturing method as in Example 1 and tested for mechanical properties, color tone, and corrosion resistance. The composition, sintering conditions, and solution treatment conditions of each sample are shown in Table 3, and the structure, bonding phase, reinforcing phase, transverse rupture strength, hardness, and color tone of the hard phase of each sample after sintering and solution treatment. The corrosion resistance caused by artificial seawater and artificial sweat was also investigated, and the results are shown in Table 4.
【表】【table】
【表】
実施例 3
AlN、Si3N4、BN、Mo2Cの各粉末及び実施例
1で使用した各原料粉末によつて所定の割合に配
合し、実施例1と同様な製造方法で焼結し、得ら
れた各試料の機械的性質、色調及び耐食性試験を
行つた。各試料の配合組成、焼結条件及び溶体化
処理条件を表5に、焼結及び溶体化処理後の各試
料の硬質相の構造、結合相、強化相、抗折力、硬
さ、色調及び人工海水、人工汗による耐食性を調
査し、その結果を表6に示した。[Table] Example 3 Each powder of AlN, Si 3 N 4 , BN, Mo 2 C and each raw material powder used in Example 1 were mixed in a predetermined ratio, and the same manufacturing method as in Example 1 was used. After sintering, the mechanical properties, color tone, and corrosion resistance of each sample were tested. Table 5 shows the composition, sintering conditions, and solution treatment conditions of each sample. Corrosion resistance due to artificial seawater and artificial sweat was investigated, and the results are shown in Table 6.
【表】【table】
【表】【table】
【表】
実施例 4
実施例1で焼結した試料No.1、7、12と実施例
2で焼結した試料No.14、17と実施例3で焼結した
試料No.19、21、26の各試料を1500bar−1350℃の
条件でHIP処理した後機械的性質、色調及び耐食
性試験を行つた。これらの試験結果を表7に示し
た。[Table] Example 4 Samples No. 1, 7, and 12 sintered in Example 1, Samples No. 14, 17 sintered in Example 2, and Samples No. 19, 21, and sintered in Example 3. After HIPing each of the 26 samples at 1500bar-1350℃, mechanical properties, color tone and corrosion resistance tests were conducted. The results of these tests are shown in Table 7.
【表】【table】
Claims (1)
た1種以上の結合相が2〜30重量%とP,Al,
B,Si,Mn,Ti,Zr,Hf,V,Nb,Taの1種
以上の金属、合金又はAl,Y,Zr,Mg,Ni,Si
の酸化物、Al,Si,Bの窒化物、Moの炭化物も
しくはこれらの相互固溶体の1種以上の化合物か
ら成る強化相が0.1〜10重量%と残りが次式(A)で
表わされる硬質相と不可避不純物とから成ること
を特徴とする装飾用焼結合金。 (Tia,Mb)(NW,CX,OY)Z …(A) 但し、M:Zr,Hf,V,Nb,Ta,Crの中か
ら選ばれた1種以上 a+b=1,1≧a≧0.4,0.6≧b≧0 W+X+Y=1,X+Y>0,1>W≧0.4 0.5≧X≧0,0.6≧Y≧0.06,0.93≧Z≧0.6 2 上記強化相がP,Al,B,Si,Mn,Ti,
Zr,Hf,V,Nb,Taの中から選ばれた1種以
上の単体金属又は合金であることを特徴とする特
許請求の範囲第1項記載の装飾用焼結合金。 3 上記強化相がAl2O3,Y2O3,ZrO2,MgO,
NiO,SiO2の中から選ばれた1種以上の酸化物
であることを特徴とする特許請求の範囲第1項又
は第2項記載の装飾用焼結合金。 4 上記強化相がAlN,Si3N4,BN,Mo2Cの中
から選ばれた1種以上の窒化物、炭化物もしくは
複化合物であることを特徴とする特許請求の範囲
第1項又は第2項記載の装飾用焼結合金。[Claims] 1. 2 to 30% by weight of one or more binder phases selected from Fe, Ni, Co, Cr, Mo, and W, and P, Al,
One or more metals or alloys of B, Si, Mn, Ti, Zr, Hf, V, Nb, Ta or Al, Y, Zr, Mg, Ni, Si
0.1 to 10% by weight of a reinforcing phase consisting of oxides of Al, Si, B nitrides, carbides of Mo, or compounds of one or more of these mutual solid solutions, and the remainder is a hard phase represented by the following formula (A). A decorative sintered alloy characterized by comprising: and inevitable impurities. (Tia , Mb ) (N W , C a≧0.4, 0.6≧b≧0 W + X + Y = 1, X + Y > 0, 1 > W ≧ 0.4 0.5 ≧ Si, Mn, Ti,
The decorative sintered alloy according to claim 1, characterized in that it is one or more single metals or alloys selected from Zr, Hf, V, Nb, and Ta. 3 The above reinforcing phase is Al 2 O 3 , Y 2 O 3 , ZrO 2 , MgO,
The decorative sintered alloy according to claim 1 or 2, characterized in that it is one or more oxides selected from NiO and SiO 2 . 4. Claim 1 or 4, wherein the reinforcing phase is one or more nitrides, carbides, or composites selected from AlN, Si 3 N 4 , BN, Mo 2 C. Decorative sintered alloy according to item 2.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8623582A JPS58204150A (en) | 1982-05-21 | 1982-05-21 | Sintered alloy for decoration |
US06/474,813 US4702769A (en) | 1982-05-21 | 1983-03-10 | Sintered alloy for decoration |
CH2755/83A CH656146A5 (en) | 1982-05-21 | 1983-05-19 | SINDERED ALLOY FOR DECORATIONAL PURPOSES. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8623582A JPS58204150A (en) | 1982-05-21 | 1982-05-21 | Sintered alloy for decoration |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS58204150A JPS58204150A (en) | 1983-11-28 |
JPH0447021B2 true JPH0447021B2 (en) | 1992-07-31 |
Family
ID=13881129
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8623582A Granted JPS58204150A (en) | 1982-05-21 | 1982-05-21 | Sintered alloy for decoration |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58204150A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012121023A1 (en) | 2011-03-07 | 2012-09-13 | 住友電工ハードメタル株式会社 | Material for decorative part |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5342740B2 (en) * | 2005-09-27 | 2013-11-13 | 京セラ株式会社 | Ceramics for decorative parts and decorative parts for watches using the same |
JP5342742B2 (en) * | 2006-09-27 | 2013-11-13 | 京セラ株式会社 | Ceramics for decorative parts and decorative parts for watches using the same |
KR20100061848A (en) | 2007-11-28 | 2010-06-09 | 쿄세라 코포레이션 | Ceramic for decorative parts and decorative parts made by using the ceramic |
WO2009145146A1 (en) | 2008-05-28 | 2009-12-03 | 京セラ株式会社 | Ceramic for decorative part and decorative part comprising the same |
CN102405299A (en) | 2009-04-24 | 2012-04-04 | 京瓷株式会社 | Ceramics for decorative component and decorative component using same |
JP5279659B2 (en) * | 2009-08-27 | 2013-09-04 | 京セラ株式会社 | Ceramics for decorative parts and decorative parts for fishing line guides |
CN104228182B (en) * | 2013-06-21 | 2017-09-29 | 深圳富泰宏精密工业有限公司 | Housing and preparation method thereof |
CN103757513A (en) * | 2013-12-30 | 2014-04-30 | 沈阳理工大学 | A Al2O3/Ti (C, N) nanocomposite cermet mold material and its prepn |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS52104406A (en) * | 1976-02-28 | 1977-09-01 | Mitsubishi Metal Corp | Super hard alloy for decorative part |
JPS5337113A (en) * | 1976-09-18 | 1978-04-06 | Nippon Shinkinzoku Kk | Titaniummnitrideebased highhstrength sintered alloy |
JPS5391007A (en) * | 1977-01-24 | 1978-08-10 | Nippon Shinkinzoku Kk | High strength sintered alloy belonging to titanium nitride |
JPS5952224B2 (en) * | 1979-02-15 | 1984-12-18 | 三菱マテリアル株式会社 | Sintered hard alloy parts with nitrided surface layer |
JPS5948948B2 (en) * | 1979-06-22 | 1984-11-29 | 三菱マテリアル株式会社 | Sintered hard alloy with excellent corrosion resistance |
JPS5949297B2 (en) * | 1979-07-04 | 1984-12-01 | 三菱マテリアル株式会社 | Hard sintered alloy for decorative parts |
JPS5658944A (en) * | 1979-10-15 | 1981-05-22 | Seiko Instr & Electronics Ltd | Wrist watch case |
JPS604259B2 (en) * | 1980-12-19 | 1985-02-02 | セイコーエプソン株式会社 | Exterior parts for hard watches |
JPS57134535A (en) * | 1981-02-16 | 1982-08-19 | Daijietsuto Kogyo Kk | Hard sintered nitride alloy for decoration |
JPS57140851A (en) * | 1981-02-23 | 1982-08-31 | Daijietsuto Kogyo Kk | Hard sintered alloy for decoration |
JPS5933660B2 (en) * | 1981-10-09 | 1984-08-17 | 日本タングステン株式会社 | Decorative golden sintered alloy |
JPS58133342A (en) * | 1982-01-30 | 1983-08-09 | Toshiba Tungaloy Co Ltd | Decorative sintered alloy |
-
1982
- 1982-05-21 JP JP8623582A patent/JPS58204150A/en active Granted
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012121023A1 (en) | 2011-03-07 | 2012-09-13 | 住友電工ハードメタル株式会社 | Material for decorative part |
US8992657B2 (en) | 2011-03-07 | 2015-03-31 | Sumitomo Electric Hardmetal Corp. | Material for decorative parts |
Also Published As
Publication number | Publication date |
---|---|
JPS58204150A (en) | 1983-11-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR960010815B1 (en) | Surface-coated small-alloy, its manufacturing method, and coated surface-coated small-alloy coated with a hard film on the alloy | |
US4589917A (en) | Decorative golden sintered alloy | |
JPH0447021B2 (en) | ||
US4606767A (en) | Decorative silver-colored sintered alloy | |
JPH0447020B2 (en) | ||
JP2001303233A (en) | Member for molten metal excellent in erosion resistance to molten metal and producing method thereof | |
KR100385208B1 (en) | Silver Sintered Product and Manufacturing Method Thereof | |
US4702769A (en) | Sintered alloy for decoration | |
JP2003514747A (en) | High strength molybdenum silicide material | |
JP3266200B2 (en) | Silicon nitride based sintered body | |
JPS5916945A (en) | Exterior parts for watches | |
JPS5949297B2 (en) | Hard sintered alloy for decorative parts | |
JP3231873B2 (en) | Silver sintered alloy and method for producing the same | |
JPH0598383A (en) | Hard alloy | |
JPS5913045A (en) | External decorative parts for timepiece | |
JP2002045957A (en) | Member for molten metal excellent in erosion resistance to molten metal and its producing method | |
JP2002105577A (en) | Decorative member and method of manufacturing the same | |
JPH0258335B2 (en) | ||
JPH07172924A (en) | Highly tough sintered compact for tool and its production | |
JPS5948948B2 (en) | Sintered hard alloy with excellent corrosion resistance | |
JPH0368739A (en) | Titanium carbide-base silver-colored sintered alloy | |
JPH05214479A (en) | High corrosion resistant and high strength hard sintered alloy | |
JPS6248408A (en) | Cermet-make cutting tool having excellent wear and abrasion resistance and toughness | |
JPS597341B2 (en) | Hard sintered alloy with excellent corrosion resistance | |
JP2717925B2 (en) | Cemented carbide and its manufacturing method |