JPH0256995B2 - - Google Patents
Info
- Publication number
- JPH0256995B2 JPH0256995B2 JP19407282A JP19407282A JPH0256995B2 JP H0256995 B2 JPH0256995 B2 JP H0256995B2 JP 19407282 A JP19407282 A JP 19407282A JP 19407282 A JP19407282 A JP 19407282A JP H0256995 B2 JPH0256995 B2 JP H0256995B2
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- core material
- plating
- copper
- pipe
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 claims description 51
- 239000000956 alloy Substances 0.000 claims description 51
- 238000007747 plating Methods 0.000 claims description 35
- 239000011162 core material Substances 0.000 claims description 28
- 229910018487 Ni—Cr Inorganic materials 0.000 claims description 22
- 239000010949 copper Substances 0.000 claims description 22
- 229910052802 copper Inorganic materials 0.000 claims description 20
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 19
- 239000002131 composite material Substances 0.000 claims description 17
- 238000010438 heat treatment Methods 0.000 claims description 17
- 229910052759 nickel Inorganic materials 0.000 claims description 13
- 229910052718 tin Inorganic materials 0.000 claims description 11
- 238000009792 diffusion process Methods 0.000 claims description 9
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 229910020994 Sn-Zn Inorganic materials 0.000 claims description 4
- 229910009069 Sn—Zn Inorganic materials 0.000 claims description 4
- 229910018605 Ni—Zn Inorganic materials 0.000 claims description 2
- 238000005253 cladding Methods 0.000 description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- 238000000034 method Methods 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 230000007547 defect Effects 0.000 description 6
- 229910052742 iron Inorganic materials 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 229910000599 Cr alloy Inorganic materials 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 4
- 229910000906 Bronze Inorganic materials 0.000 description 3
- DMFGNRRURHSENX-UHFFFAOYSA-N beryllium copper Chemical compound [Be].[Cu] DMFGNRRURHSENX-UHFFFAOYSA-N 0.000 description 3
- 239000010974 bronze Substances 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 229910017518 Cu Zn Inorganic materials 0.000 description 1
- 229910017752 Cu-Zn Inorganic materials 0.000 description 1
- 229910017943 Cu—Zn Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910001128 Sn alloy Inorganic materials 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 150000001879 copper Chemical class 0.000 description 1
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000005491 wire drawing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/22—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
- B23K20/233—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
- Eyeglasses (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Laminated Bodies (AREA)
Description
この発明は眼鏡フレーム部品用の複合材の製法
に関し、特にNi―Cr系合金を外被とする複合材
を製造するにあたつて、Ni―Cr系合金製パイプ
の内面にNiメツキもしくはNi―Sn2層メツキを
施した後に銅基合金芯材を挿入した後引抜加工を
施してから拡散熱処理することによりメツキ層の
Ni,Snを芯材の銅基合金中に拡散させて芯材の
バネ性、強度を向上させ、かつNi―CR系合金の
熱処理時の酸化を防止するようにしたものであ
る。
周知のようにNi―Cr系合金は耐食性が良好で
しかも白色で装飾性が良好なため、眼鏡フレーム
部品材として広く使用されている。しかしながら
Ni―Cr系合金を単独で眼鏡フレーム部品に使用
した場合、バネ性が不足し、また高価でしかも加
工に困難を伴う等の問題がある。そこで従来から
Ni―Cr系合金を外被とし、芯材としてリン青銅、
ベリリウム銅あるいはステンレス鋼等を用いたク
ラツド材を眼鏡フレーム部品に使用することが知
られている。しかしながらこの場合、リン青銅、
ベリリウム銅あるいはステンレス鋼にNi―Cr系
合金をクラツドする際に雰囲気調整が不充分であ
ればクラツド不良が発生する問題があり、また特
に芯材としてリン青銅を用いた場合にはバネ性が
不足し、しかも芯材中にリンが含有されるためク
ラツド化が不安定となる問題があり、一方芯材と
してベリリウム銅を用いた場合にはクラツド性に
は良好なものの、バネ性を与えるために熱処理を
行う必要があり、さらに芯材としてステンレス銅
を用いた場合にはクラツドに高温を要し、しかも
他の金属を用いた場合よりも加工が困難となる問
題がある。
この発明は以上の事情に鑑みてなされたもの
で、外被をNi―Cr合金とする眼鏡フレーム部品
用の複合材を製造するにあたつて、加工性を良好
にすると同時にクラツドを安定化してクラツド不
良が生じないようになし、しかもバネ性および強
度が優れた複合材が得られるようにすることを目
的とするものである。
すなわちこの発明の方法は、Ni―Cr系合金製
のパイプ内面にNiメツキおよびSnの2層メツキ
とのうちいずれか一方を施し、次いでパイプ内に
Cu―Ni―Sn―Zn合金、Cn−Zn合金、Cu―Ni―
Zn合金のうちから選ばれた銅基合金からなる芯
材を挿入し、次いで引抜加工を施し、拡散熱処理
を施して前記メツキ層の元素を芯材に拡散させる
ことを特徴とするものであり、このようにメツキ
層を設けておくことによつて熱処理時におおける
Ni―Cr系合金の酸化を防止してクラツド不良発
生を防止し、かつメツキ層のNi,Snを芯材へ拡
散させることにより芯材の銅基合金強度、バネ性
を向上させ、かつまた芯材を銅基合金とすること
により加工性も良好としたものである。
以下この発明の方法をさらに詳細に説明する。
この発明の方法においては、まず第1図Aに示
すようにNi―Cr系合金からなるパイプ1の内面
に、Niメツキ、またはNiおよびSnの2層メツキ
を施してNiもしくはNiおよびSnのメツキ層2を
形成する。ここでNi―Cr系合金としては、Crを
3〜18重量%程度含有し、残部Niからなるもの
を使用することが望ましく、またこのほか少量の
Ag等の添加元素が含有されることは妨げない。
またメツキ層2の厚みは10μm〜40μm程度とする
ことが望ましい。さらにメツキ層2として、Ni
およびSnの2層メツキを施す場合、通常はNi―
Cr系合金製パイプ1の内面に先ずNiメツキを施
してからそのNiメツキ層の上にSnメツキを施す
ことが望ましい。
上述のようにNi、もしくはNiおよびSnのメツ
キ層2をNi―Cr系合金パイプ1の内面に形成し
た後、第1図Bに示すようにその内側に銅基合金
の芯材3を挿入、嵌合させる。この銅基合金とし
ては、Cu―Ni―Sn―Zn合金、Cu―Zn合金、Cu
―Ni―Zn合金のうちから選ばれた1種のものを
用いる。これらの銅基合金はいずれも加工性が良
好であり、またバネ性および強度が良好なもので
ある。
このようにメツキ層2の内側に銅基合金芯材3
を嵌め合せた後には、通常は第1図Cに示すよう
にNi―Cr系合金パイプ1の外側に保護のための
鉄等のパイプ4を嵌め合せ、引抜加工を行つてメ
ツキ層2と銅基合金芯材3とを充分に密着させ
る。但しここでパイプ4は続く拡散熱処理後に除
去すべきものであるから、その拡散熱処理温度で
はNi―Cr系合金パイプ1と接合されないような
材質の例えば鉄等のものを用いる。
次いでメツキ層2のNiやSnを内側の芯材3の
銅基合金中へ拡散させるための熱処理を行う。こ
の熱処理によつて芯材3の銅基合金はメツキ層2
からの拡散によりNi濃度やSn濃度が高くなつて
強化され、バネ性や強度がより一層高くなると同
時に、第1図Dに示すようにメツキ層2と芯材3
とが一体化して、その間の結合強度が著しく大き
くなる。またこの拡散熱処理時においては、パイ
プ1のNi―Cr系合金の内面にメツキ層2が存在
するため、Ni―Cr系合金の内面に側に酸化が生
じることがなく、芯材との間のクラツド不良が生
じることが有効に防止される。換言すれば、熱処
理時における雰囲気置換が不充分であつても、内
部酸化によるクラツド不良が生じることが有効に
防止される。
このように拡散熱処理を行つた後には、通常は
外側の鉄等の保護用のパイプ4を適宜の手段で剥
離除去し、残つた内側のクラツド材、すなわち第
1図Eに示すようにNi―Cr系合金を外被1Aと
しNiやSnが濃化された銅基合金を芯材3Aとす
る複合材に適宜線引加工やプレス加工等を施して
眼鏡フレーム部品とする。
上述のように、最終的に得られた眼鏡フレーム
複合材部品においては、芯材部分の銅基合金の
NiやSnが濃化されているため、バネ性や強度が
著しく優れる。特に最終的な芯材の銅基合金が所
謂超弾性を示す組成となるように初期の銅基合金
の粗成およびその後の熱処理によりNiやSnの拡
散固溶量を設定しておけば、バネ性はより良好と
なる。また複合材表面は、Ni―Cr系合金となつ
ているため耐食性に優れかつロウ付け性も良好で
ある。一方製造工程上においては、Ni―Cr系合
パイプの内面にNiもしくはNiおよびSnのメツキ
層を形成してから熱処理を行うため、前述のよう
にNi―Cr系合金パイプ内面が酸化してクラツド
不良が生じるおそれが少なく、またこれに伴つて
熱処理雰囲気の設定が容易となる。さらに加工上
は銅基合金を芯材としているため、加工も容易で
生産性も高い。
以下にこの発明の実施例を基す。
実施例 1
外径45mm、肉厚1.3mm、長さ400mmのNi―10wt
%Cr合金製パイプの内面にNiメツキを20μm厚で
施し、次いでそのパイプ内部にCu―2wt%Ni―
11wt%Zn―5wt%Snの合金棒を嵌め込み、さら
にNi―Cr系合金製パイプの外側に外径49mm、内
径45mm、長さ400mmの鉄パイプを嵌め合せ、しか
る後に内径48.5mmのダイスで引抜加工を行つてNi
メツキ層と芯材としてのCu―Ni―Sn―Zn合金棒
とを密着させた。さらに水素中において700℃で
1時間拡散熱処理を行つてNiメツキ層からNiを
芯材としてのCu―Ni―Sn―Zn合金中に拡散させ
た。続いて外側の鉄パイプにフライスにより溝を
入れてその鉄パイプを内側のクラツド材から剥離
除去させた後、クラツド材を引抜加工し、さらに
焼鈍および線引加工を施して2.6mmの線材とした。
実施例 2
実施例1で用いたと同様なNi―Cr系合金パイ
プの内面にNiメツキを20μm厚で施した後、さら
にそのNiメツキ層の上にSnメツキを20μm厚で施
してNiおよびSnの2層メツキとし、次いでその
内側に実施例1と同様なCu―Ni―Zn合金棒を挿
入嵌合し、以下実施例1と同様にして2.6mmの複
合線材を得た。
比較例
実施例1で用いたと同様なNi―Cr系合金の内
面にNiメツキを施さなかつた点以外は実施例1
と同様に処理して2.6mmの複合線材を得た。
以上の各実施例および比較例において、それぞ
れにおけるクラツド歩留を調べたところ、第1表
に示す結果が得られた。ただしここでクラツド歩
留は、各例により得られた複合材から密着不良
(クラツド不良)を除いた複合材製品の重量と、
各例により得られた複合材総重量との比で示す。
また各実施例および比較例における最終加工段階
で600℃で30分間焼鈍後プレス加工して厚さ0.5
mm、幅4.5mm、長さ100mmの複合材を得、各複合板
のバネ値を調べた結果を第1表に併せて示す、。
但しこのバネ値測定においては、板の片端をチヤ
ツクし、そのチヤツク部を中心としてその反対側
の端部に荷重を加えて30゜曲げ、荷重を除去して
板が戻つた時の戻り角度θを調べ、θ/30×100
(%)の値をバネ値として表示した。
The present invention relates to a method for manufacturing a composite material for eyeglass frame parts, and in particular, when manufacturing a composite material having an outer covering made of a Ni-Cr alloy, the inner surface of a pipe made of a Ni-Cr alloy is coated with Ni plating or Ni- After applying Sn 2-layer plating, a copper-based alloy core material is inserted, drawing is performed, and then diffusion heat treatment is performed to improve the plating layer.
Ni and Sn are diffused into the copper-based alloy of the core material to improve the springiness and strength of the core material, and to prevent oxidation during heat treatment of the Ni-CR alloy. As is well known, Ni-Cr alloys have good corrosion resistance, are white, and have good decorative properties, so they are widely used as materials for eyeglass frame parts. however
When a Ni--Cr alloy is used alone for eyeglass frame parts, there are problems such as insufficient springiness, high cost, and difficulty in processing. Therefore, traditionally
The outer cover is made of Ni-Cr alloy, and the core material is phosphor bronze.
It is known to use cladding materials made of beryllium copper, stainless steel, or the like for eyeglass frame parts. However, in this case, phosphor bronze,
When cladding beryllium copper or stainless steel with Ni-Cr alloy, there is a problem of cladding failure if the atmosphere is not properly adjusted, and especially when phosphor bronze is used as the core material, the springiness is insufficient. However, since phosphorus is contained in the core material, there is a problem that cladding becomes unstable.On the other hand, when beryllium copper is used as the core material, although it has good cladding properties, it is difficult to provide spring properties. It is necessary to perform heat treatment, and furthermore, when stainless steel copper is used as the core material, the cladding requires a high temperature, and furthermore, there is a problem that processing is more difficult than when using other metals. This invention was made in view of the above-mentioned circumstances, and in manufacturing a composite material for eyeglass frame parts whose outer sheath is made of a Ni-Cr alloy, it is possible to improve workability and at the same time stabilize the cladding. The object of this invention is to prevent cladding defects from occurring and to obtain a composite material with excellent springiness and strength. In other words, the method of this invention applies either Ni plating or Sn two-layer plating to the inner surface of a Ni-Cr alloy pipe, and then coats the inside of the pipe with two layers of Ni plating or Sn plating.
Cu-Ni-Sn-Zn alloy, Cn-Zn alloy, Cu-Ni-
A core material made of a copper-based alloy selected from among Zn alloys is inserted, and then subjected to drawing processing and diffusion heat treatment to diffuse the elements of the plating layer into the core material, By providing a plating layer in this way, it is possible to prevent damage during heat treatment.
It prevents oxidation of the Ni-Cr alloy to prevent clad defects, and diffuses Ni and Sn in the plating layer into the core material to improve the strength and springiness of the copper-based alloy core material. By using a copper-based alloy as the material, workability is also improved. The method of the present invention will be explained in more detail below. In the method of the present invention, first, as shown in FIG. Form layer 2. As the Ni-Cr alloy, it is desirable to use one containing about 3 to 18% by weight of Cr, with the remainder being Ni.
The inclusion of additive elements such as Ag is not prohibited.
Further, the thickness of the plating layer 2 is preferably about 10 μm to 40 μm. Furthermore, as the plating layer 2, Ni
When applying two-layer plating of
It is desirable to first apply Ni plating to the inner surface of the Cr-based alloy pipe 1 and then apply Sn plating on the Ni plating layer. After forming the plating layer 2 of Ni or Ni and Sn on the inner surface of the Ni-Cr alloy pipe 1 as described above, a core material 3 of a copper-based alloy is inserted inside it as shown in FIG. 1B. Make it fit. This copper-based alloy includes Cu-Ni-Sn-Zn alloy, Cu-Zn alloy, Cu
- Use one type selected from Ni-Zn alloys. All of these copper-based alloys have good workability, and also have good spring properties and strength. In this way, the copper-based alloy core material 3 is placed inside the plating layer 2.
After fitting, normally, as shown in Fig. 1C, a pipe 4 made of iron or the like for protection is fitted on the outside of the Ni-Cr alloy pipe 1, and a drawing process is performed to separate the plating layer 2 and the copper. The base alloy core material 3 is brought into sufficient contact with the base alloy core material 3. However, since the pipe 4 should be removed after the subsequent diffusion heat treatment, a material such as iron is used that will not be joined to the Ni--Cr alloy pipe 1 at the diffusion heat treatment temperature. Next, heat treatment is performed to diffuse Ni and Sn of the plating layer 2 into the copper-based alloy of the inner core material 3. Through this heat treatment, the copper-based alloy of the core material 3 becomes the plating layer 2.
As a result of diffusion, the Ni and Sn concentrations increase and become stronger, resulting in even higher springiness and strength.
are integrated, and the bond strength between them increases significantly. In addition, during this diffusion heat treatment, since the plating layer 2 exists on the inner surface of the Ni-Cr alloy of the pipe 1, oxidation does not occur on the inner surface of the Ni-Cr alloy, and there is no oxidation between the inner surface of the Ni-Cr alloy and the core material. The occurrence of cladding defects is effectively prevented. In other words, even if the atmosphere replacement during heat treatment is insufficient, crud defects due to internal oxidation can be effectively prevented. After performing the diffusion heat treatment in this way, the outer protective pipe 4 made of iron or the like is usually peeled off and removed by an appropriate means, and the remaining inner cladding material, that is, the Ni- A composite material having a Cr-based alloy as the outer sheath 1A and a copper-based alloy enriched with Ni or Sn as the core material 3A is subjected to wire drawing, press working, etc. as appropriate to make an eyeglass frame part. As mentioned above, in the final eyeglass frame composite parts, the copper-based alloy of the core material is
Because it is enriched with Ni and Sn, it has significantly superior springiness and strength. In particular, if the amount of diffused solid solution of Ni and Sn is set by the initial rough formation of the copper-based alloy and subsequent heat treatment so that the final copper-based alloy of the core material has a composition that exhibits so-called superelasticity, it is possible to performance will be better. Furthermore, since the composite material surface is made of a Ni-Cr alloy, it has excellent corrosion resistance and good brazing properties. On the other hand, in the manufacturing process, heat treatment is performed after forming a plating layer of Ni or Ni and Sn on the inner surface of the Ni-Cr alloy pipe, so as mentioned above, the inner surface of the Ni-Cr alloy pipe oxidizes and cracks. There is less risk of defects occurring, and the heat treatment atmosphere can be easily set. Furthermore, since the core material is a copper-based alloy, it is easy to process and has high productivity. Examples of the present invention will be described below. Example 1 Ni-10wt with outer diameter 45mm, wall thickness 1.3mm, length 400mm
Ni plating is applied to the inner surface of the %Cr alloy pipe to a thickness of 20μm, and then Cu-2wt%Ni- is applied inside the pipe.
A 11wt%Zn-5wt%Sn alloy rod was fitted, and then an iron pipe with an outer diameter of 49mm, an inner diameter of 45mm, and a length of 400mm was fitted on the outside of the Ni-Cr alloy pipe, and then drawn using a die with an inner diameter of 48.5mm. Ni after processing
The plating layer and the Cu--Ni--Sn--Zn alloy rod as the core material were brought into close contact. Further, diffusion heat treatment was performed in hydrogen at 700°C for 1 hour to diffuse Ni from the Ni plating layer into the Cu-Ni-Sn-Zn alloy serving as the core material. Next, a groove was cut into the outer iron pipe using a milling cutter, and the iron pipe was peeled off from the inner clad material, after which the clad material was drawn and further annealed and wire-drawn to produce a 2.6 mm wire rod. . Example 2 After applying Ni plating to a thickness of 20 μm on the inner surface of a Ni-Cr alloy pipe similar to that used in Example 1, Sn plating was further applied to a thickness of 20 μm on top of the Ni plating layer to remove Ni and Sn. A two-layer plating was applied, and then a Cu--Ni--Zn alloy rod similar to that in Example 1 was inserted and fitted inside the plating, and a 2.6 mm composite wire was obtained in the same manner as in Example 1. Comparative Example Example 1 except that the inner surface of the Ni-Cr alloy used in Example 1 was not plated with Ni.
A 2.6 mm composite wire was obtained in the same manner as above. When the cladding yield in each of the above Examples and Comparative Examples was investigated, the results shown in Table 1 were obtained. However, the cladding yield here is the weight of the composite material product obtained by excluding poor adhesion (defective cladding) from the composite material obtained in each example,
It is shown as a ratio to the total weight of the composite material obtained in each example.
In addition, at the final processing stage in each example and comparative example, the material was annealed at 600°C for 30 minutes and then pressed to a thickness of 0.5
Composite materials with a width of 4.5 mm, a width of 4.5 mm, and a length of 100 mm were obtained, and the spring values of each composite plate were investigated. The results are also shown in Table 1.
However, when measuring the spring value, check one end of the board, apply a load to the opposite end around the chuck, bend it 30 degrees, and then calculate the return angle θ when the load is removed and the board returns. Check θ/30×100
(%) values are displayed as spring values.
【表】
第1表から、この発明の実施例の方法により得
られた複合材はクラツド密着性が良好でクラツド
歩留が高く、またバネ性も優れていることが明ら
かである。
以上の説明で明らかなようにこの発明の方法に
よれば、バネ性や強度が優れしかも表面耐食性が
良好な眼鏡フレーム用複合材を得ることができ、
またクラツド不良の発生が極めて少ないとともに
加工も容易となる等の種々の効果が得られる。[Table] It is clear from Table 1 that the composite material obtained by the method of the example of the present invention has good cladding adhesion, high cladding yield, and excellent springiness. As is clear from the above description, according to the method of the present invention, it is possible to obtain a composite material for eyeglass frames that has excellent spring properties and strength, and also has good surface corrosion resistance.
In addition, various effects such as extremely low occurrence of clad defects and ease of processing can be obtained.
第1図A〜Eはこの発明の方法の一例を段階的
に示す略解的な断面図である。
1…Ni―Cr系合金パイプ、2…メツキ層、3
…銅基合金芯材。
FIGS. 1A to 1E are schematic cross-sectional views showing step-by-step an example of the method of the present invention. 1... Ni-Cr alloy pipe, 2... plating layer, 3
...Copper-based alloy core material.
Claims (1)
NiおよびSnの2層メツキとのいずれか一方を施
し、 次いでパイプ内にCu―Ni―Sn―Zn合金、Cu
―Zn合金、Cu―Ni―Zn合金のうちのいずれか1
種の銅基合金からなる芯材を挿入し、 次いで引抜加工を施し、 その後拡散熱処理を施して前記メツキ層の元素
を芯材に拡散させることを特徴とする眼鏡フレー
ム用複合材の製法。[Claims] 1 Ni plating on the inner surface of the Ni-Cr alloy pipe,
Either Ni or Sn two-layer plating is applied, and then Cu-Ni-Sn-Zn alloy, Cu
-Any one of Zn alloy or Cu-Ni-Zn alloy
1. A method for producing a composite material for eyeglass frames, which comprises inserting a core material made of a copper-based alloy, then subjecting it to drawing processing, and then subjecting it to diffusion heat treatment to diffuse the elements of the plating layer into the core material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19407282A JPS5985391A (en) | 1982-11-05 | 1982-11-05 | Production of composite material for spectacle frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19407282A JPS5985391A (en) | 1982-11-05 | 1982-11-05 | Production of composite material for spectacle frame |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5985391A JPS5985391A (en) | 1984-05-17 |
| JPH0256995B2 true JPH0256995B2 (en) | 1990-12-03 |
Family
ID=16318487
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19407282A Granted JPS5985391A (en) | 1982-11-05 | 1982-11-05 | Production of composite material for spectacle frame |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5985391A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20030090994A (en) * | 2002-05-24 | 2003-12-01 | 홍유표 | METHOD FOR MANUFACTURING MULTILAYERED CLAD PALATE INCLUDING A Cu PLATE |
-
1982
- 1982-11-05 JP JP19407282A patent/JPS5985391A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5985391A (en) | 1984-05-17 |
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