CN1216164C - Titanium alloy coated mould material for photographic trade and manufacturing method thereof - Google Patents
Titanium alloy coated mould material for photographic trade and manufacturing method thereof Download PDFInfo
- Publication number
- CN1216164C CN1216164C CN02156614.3A CN02156614A CN1216164C CN 1216164 C CN1216164 C CN 1216164C CN 02156614 A CN02156614 A CN 02156614A CN 1216164 C CN1216164 C CN 1216164C
- Authority
- CN
- China
- Prior art keywords
- titanium alloy
- coating mold
- deformation
- mold material
- photographic industry
- 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 - Fee Related
Links
Landscapes
- Metal Rolling (AREA)
Abstract
本发明涉及一种钛合金材料,特别涉及一种照相行业应用钛合金涂布模具材料及其制造方法,该钛合金涂布模具材料化学成份(重量百分比)是Ti基;Al:5.0%~7.0%;Fe:1.3%~2.2%;C:0~0.05%;N:0~0.035%;H:0~0.0125%;O:0~0.15%,该合金经熔炼锻造及固熔处理:850℃~950℃/30min~90min/WQ,成为便于机加工的软态材料,其硬度HRC≤37.2;加工成坯料部件后经时效热处理:450℃~550℃/6h~12h/AC,其硬度HRC≥40,本发明钛合金涂布模具材料不仅在多种介质特别是在高氯化银乳剂中耐腐蚀强,而且不影响照相性能,适用于生产照相相业的涂布模具和各种贮存设备等,本发明提供的钛合金材料不含稀贵金属,具有市场竞争力。The invention relates to a titanium alloy material, in particular to a titanium alloy coating mold material used in the photographic industry and a manufacturing method thereof. The chemical composition (weight percentage) of the titanium alloy coating mold material is Ti-based; Al: 5.0% to 7.0 %; Fe: 1.3% to 2.2%; C: 0 to 0.05%; N: 0 to 0.035%; H: 0 to 0.0125%; O: 0 to 0.15%. ~950℃/30min~90min/WQ, become a soft material that is easy to machine, its hardness HRC≤37.2; after processing into blank parts, aging heat treatment: 450℃~550℃/6h~12h/AC, its hardness HRC≥ 40. The titanium alloy coating mold material of the present invention not only has strong corrosion resistance in various media, especially high silver chloride emulsion, but also does not affect the photographic performance, and is suitable for the production of coating molds and various storage equipment in the photographic industry, etc. , the titanium alloy material provided by the invention does not contain rare and precious metals and has market competitiveness.
Description
技术领域:Technical field:
本发明涉及一种钛合金材料,特别涉及一种照相行业应用钛合金涂布模具材料及其制造方法。The invention relates to a titanium alloy material, in particular to a titanium alloy coating mold material used in the photographic industry and a manufacturing method thereof.
技术背景:technical background:
照相工业中的涂布模具是感光乳剂涂布过程的核心部件。近年来国内先后使用过多种不锈钢制作的涂布模具,但实际应用时均不理想,这是因为感光乳剂含有腐蚀性强的卤化物,实验已证实,把0Cr14NiMn3Al置于感光乳剂溶液内浸泡24小时,就会出现树叶状的腐蚀痕迹,这种腐蚀不仅改变了涂布模具的几何形状、影响涂布效果以及减少涂布模具使用寿命,而且腐蚀物被带入感光涂料层中影响照相性能。目前,国外制作涂布模具所使用的SUS317号不锈钢(日本标准),硬度较低(HB146),对物料工艺过程控制要求高,使用易划伤,加工制做困难,另外,涂布系统的清洗液大多数是强氧化剂,例如NaClO,涂布模具容易被氧化。采用纯钛制作涂布模具,虽然耐蚀性令人满意,但由于纯钛硬度较低,加工精度不易控制,表面容易被划伤,进而导致涂布弊病,因此也不能满足使用要求。中国专利CN1170767A公开了一种钛合金材料,虽然该材料的耐蚀性优良,但其含有Cu元素,不宜制作照相乳剂设备。因而需要研制一种能够满足照相行业用的新的涂布模具材料。Coating dies in the photographic industry are a central component of the emulsion coating process. In recent years, a variety of coating molds made of stainless steel have been used in China, but they are not ideal in practical applications. This is because the photosensitive emulsion contains highly corrosive halides. Experiments have confirmed that 0Cr14NiMn3Al is placed in the photosensitive emulsion solution. After hours, there will be leaf-shaped corrosion marks, which not only change the geometry of the coating mold, affect the coating effect and reduce the service life of the coating mold, but also corrode products are brought into the photosensitive coating layer to affect the photographic performance. At present, the SUS317 stainless steel (Japanese standard) used in the production of coating molds abroad has low hardness (HB146), high requirements for material process control, easy to scratch when used, and difficult to process and manufacture. In addition, the cleaning of the coating system Most of the liquid is a strong oxidizing agent, such as NaClO, and the coating mold is easily oxidized. Although the corrosion resistance of pure titanium is satisfactory, due to the low hardness of pure titanium, the processing accuracy is not easy to control, and the surface is easily scratched, which will lead to coating problems, so it cannot meet the use requirements. Chinese patent CN1170767A discloses a titanium alloy material. Although the material has excellent corrosion resistance, it contains Cu element, which is not suitable for making photographic emulsion equipment. Thereby it is necessary to develop a new coating mold material that can satisfy the photographic industry.
发明内容:Invention content:
本发明的目的是:提供一种照相行业涂布模具用的钛合金材料及该材料的制造方法,使用该材料制作的照相行业涂布模具,既有令人满意的耐蚀性,不影响感光乳剂的性能,又有高硬度的特点,能满足制作照相乳剂涂布模具和供料系统中各种贮存设备的特殊要求。The object of the present invention is to provide a titanium alloy material for coating molds in the photographic industry and a manufacturing method of the material. The coating molds for the photographic industry made of this material have satisfactory corrosion resistance and do not affect photosensitivity. The performance of the emulsion and the characteristics of high hardness can meet the special requirements of various storage equipment in the production of photographic emulsion coating molds and feeding systems.
本发明的技术方案是:Technical scheme of the present invention is:
一种照相行业用钛合金涂布模具材料,其特征在于:该材料的化学成份(重量百分比)是Ti基;Al:5.0%~7.0%;Fe:1.3%~2.2%;C:0~0.05%;N:0~0.035%;H:0~0.0125%;O:0~0.15%;其中不含Cu、Zn、Sn、Pb等对照相乳剂有影响元素。A titanium alloy coating mold material for the photographic industry, characterized in that: the chemical composition (weight percentage) of the material is Ti-based; Al: 5.0% to 7.0%; Fe: 1.3% to 2.2%; C: 0 to 0.05% %; N: 0-0.035%; H: 0-0.0125%; O: 0-0.15%; which does not contain Cu, Zn, Sn, Pb and other elements that affect the photographic emulsion.
一种照相行业用钛合金涂布模具材料的生产方法,包括:A method for producing a titanium alloy coating mold material for the photographic industry, comprising:
a.采用零级海绵钛,工业纯铁,工业纯铝箔、铝条原料,按合金的化学成份进行配料,并压制电极;a. Use zero-grade sponge titanium, industrial pure iron, industrial pure aluminum foil, and aluminum strips as raw materials, make ingredients according to the chemical composition of the alloy, and press the electrodes;
b.将压制成的电极经在真空或氩气保护下氩弧焊接,在真空自耗电弧炉中进行两次熔炼后铸成合金锭;b. The pressed electrode is argon-arc welded under vacuum or argon protection, and then melted twice in a vacuum consumable electric arc furnace and cast into an alloy ingot;
c.将合金锭放在电炉中加热后进行锻造开坯,锻造开坯温度控制在1050℃~1150℃之间;c. Heat the alloy ingot in an electric furnace and then forge the billet. The temperature of the forging billet is controlled between 1050°C and 1150°C;
d.对锻造开坯过的半成品放在电炉中加热后进行热加工,热加工温度控制在850℃~950℃之间,对半成品热加工的头次变形量应大于60%,热加工制成棒材或型材成品的其余火次变形量不小于40%。期间还进行α+β/β相变以上温区变形,变形量不小于30%,此循环不少于两次;若生产板材,每火次变形量不小于50%,最后一火次变形量不小于60%;d. Heat the semi-finished product that has been forged and opened in an electric furnace for thermal processing. The thermal processing temperature is controlled between 850°C and 950°C. The first deformation of the semi-finished product should be greater than 60%. The remaining fire deformation of the finished bar or profile is not less than 40%. During the period, deformation in the temperature zone above the α+β/β phase transition is carried out, the deformation amount is not less than 30%, and this cycle is not less than two times; if the plate is produced, the deformation amount of each fire is not less than 50%, and the deformation amount of the last fire Not less than 60%;
其特征在于:对热加工制成的棒材或型材在固熔处理状态下加工成型,材料硬度HRC≤37.2,固熔热处理制度是:850℃~950℃/30min~90min/WQ,加工成型后,再经时效处理后使用,材料硬度HRC≥40,其时效热处理制度是:480℃~530℃/6h~12h/AC。It is characterized in that: the rod or profile made by thermal processing is processed and formed in the state of solid solution treatment, the material hardness HRC≤37.2, the solid solution heat treatment system is: 850℃~950℃/30min~90min/WQ, after processing and forming , and then used after aging treatment, material hardness HRC ≥ 40, the aging heat treatment system is: 480 ℃ ~ 530 ℃ / 6h ~ 12h / AC.
采用上述技术方案,本发明充分满足了照相行业中多种介质环境特别是在高氯化银乳剂的高腐蚀的环境中的应用,同时材料硬度大。可用于生产照相行业的涂布模具、供料装置和多种贮存设备。By adopting the above-mentioned technical scheme, the present invention fully satisfies the application in various media environments in the photographic industry, especially in high-corrosion environments of high-silver chloride emulsion, and the material has high hardness. It can be used to produce coating molds, feeding devices and various storage equipment for the photographic industry.
具体实施方式Detailed ways
下面通过具体实施例对本发明作进一步的说明。The present invention will be further described below by specific examples.
实施例1:Example 1:
一种照相行业用钛合金涂布模具材料的生产方法,包括:采用零级海绵钛,工业纯铁,工业纯铝箔、铝条,按(重量百分比)Al:5.7%,Fe:1.9%,同时将氧含量及其他杂质含量控制在要求范围,并压制电极;将压制成的电极经在真空或氩气保护下氩弧焊接,在真空自耗电弧炉中进行两次熔炼后铸成合金锭;将合金锭放在电炉中加热后进行开坯锻造,开坯锻造温度控制在1150℃;对锻造开坯过的半成品放在电炉中加热后进行热加工,热加工温度控制在900℃;对半成品热加工的头次变形量为70%,其余火次变形量为45%,期间还进行α+β/β相变以上温区变形,变形量为35%,此循环进行三次,最后制成棒材;对热加工制成的棒材进行热处理,其固熔热处理制度是:850℃/30min/WQ,此时材料的硬度HRC值为34.5;加工成型后,再经时效处理后使用,其时效热处理制度是:480℃/8h/AC,此时材料的硬度HRC值为42,得到样品1,对样品进行成份分析,结果见表1。A production method for coating mold materials with titanium alloys in the photographic industry, comprising: adopting zero-grade sponge titanium, industrial pure iron, industrial pure aluminum foil, aluminum strips, according to (weight percentage) Al: 5.7%, Fe: 1.9%, at the same time Control the oxygen content and other impurity content within the required range, and press the electrode; the pressed electrode is argon-arc welded under vacuum or argon protection, and it is melted twice in a vacuum consumable electric arc furnace and cast into an alloy ingot ;Heat the alloy ingot in an electric furnace and then carry out billet forging, and the temperature of the billet forging is controlled at 1150°C; put the semi-finished product that has been forged and billeted in an electric furnace and then heat it, and then carry out thermal processing, and the thermal processing temperature is controlled at 900°C; The first deformation of the semi-finished product thermal processing is 70%, and the remaining heat deformation is 45%. During this period, the temperature zone above the α+β/β phase transformation is deformed, and the deformation is 35%. This cycle is carried out three times, and finally it is made Bars; for heat treatment of bars made by thermal processing, the solid solution heat treatment system is: 850°C/30min/WQ, at this time the hardness HRC value of the material is 34.5; after processing and forming, it is used after aging treatment, and its The aging heat treatment system is: 480°C/8h/AC. At this time, the hardness HRC value of the material is 42. Sample 1 is obtained. The composition of the sample is analyzed, and the results are shown in Table 1.
实施例2:Example 2:
采用零级海绵钛,工业纯铁,工业纯铝箔、铝条,按(重量百分比)Al:7.0%,Fe:1.3%,同时将氧含量及其他杂质含量控制在要求范围,并压制电极;将压制成的电极经在真空或氩气保护下氩弧焊接,在真空自耗电弧炉中进行两次熔炼后铸成合金锭;将合金锭放在电炉中加热后进行开坯锻造,开坯锻造温度控制在1050℃;对锻造开坯过的半成品放在电炉中加热后进行热加工,热加工温度控制在950℃;对半成品热加工的头次变形量65%,其余火次变形量为40%,期间还进行α+β/β相变以上温区变形,变形量为30%,此循环进行二次,最后制成棒材;对热加工制成的棒材进行热处理,其固熔热处理制度是:950℃/50min/WQ,此时材料的硬度HRC值为37.2;加工成型后,再经时效处理后使用,其时效热处理制度是:530℃/6h/AC,此时材料的硬度HRC值为42.5,得到样品2,对样品进行成份分析,结果见表1。Use zero-grade sponge titanium, industrial pure iron, industrial pure aluminum foil, aluminum strip, according to (weight percentage) Al: 7.0%, Fe: 1.3%, at the same time control the content of oxygen and other impurities within the required range, and press the electrode; The pressed electrodes are welded by argon arc under vacuum or argon protection, and cast into alloy ingots after being smelted twice in a vacuum consumable electric arc furnace; The forging temperature is controlled at 1050°C; the semi-finished product that has been forged and opened is heated in an electric furnace for thermal processing, and the thermal processing temperature is controlled at 950°C; the first deformation of the semi-finished product is 65%, and the remaining heat deformation is 40%, during which the temperature zone above the α+β/β phase transformation is deformed, and the deformation amount is 30%. This cycle is carried out twice, and finally made into bars; The heat treatment system is: 950℃/50min/WQ, at this time the hardness HRC value of the material is 37.2; after processing and molding, it is used after aging treatment, and the aging heat treatment system is: 530℃/6h/AC, the hardness of the material at this time HRC value is 42.5, obtains sample 2, carries out component analysis to sample, and the results are shown in Table 1.
实施例3:Example 3:
采用零级海绵钛,工业纯铁,工业纯铝箔、铝条,按(重量百分比)Al:5.0%,Fe:2.2%,同时将氧含量及其他杂质含量控制在要求范围,并压制电极;将压制成的电极经在真空或氩气保护下氩弧焊接,在真空自耗电弧炉中进行两次熔炼后铸成合金锭;将合金锭放在电炉中加热后进行开坯锻造,开坯锻造温度控制在1100℃;将板坯放在电阻炉,加热温度控制在850℃,用200吨真空轧机两火轧制,第一火次变形量为65%,最后一火次变形量为80%,最后获得板材。对热加工制成的板材进行热处理,其固熔热处理制度是:910℃/90min/WQ,此时材料的硬度HRC值为36.7;加工成型后,再经时效处理后使用,其时效热处理制度是:520℃/12h/AC,此时材料的硬度HRC值为42.8,得到样品3,对样品进行成份分析,结果见表1。Use zero-grade sponge titanium, industrial pure iron, industrial pure aluminum foil, aluminum strip, according to (weight percentage) Al: 5.0%, Fe: 2.2%, at the same time control the content of oxygen and other impurities within the required range, and press the electrode; The pressed electrodes are welded by argon arc under vacuum or argon protection, and cast into alloy ingots after being smelted twice in a vacuum consumable electric arc furnace; The forging temperature is controlled at 1100°C; the slab is placed in a resistance furnace, the heating temperature is controlled at 850°C, and it is rolled with two fires in a 200-ton vacuum rolling mill. The deformation in the first fire is 65%, and the deformation in the last fire is 80%. %, finally get the sheet. For heat treatment of the plate made by thermal processing, the solid solution heat treatment system is: 910°C/90min/WQ, at this time, the hardness HRC value of the material is 36.7; after processing and forming, it is used after aging treatment, and the aging heat treatment system is : 520°C/12h/AC. At this time, the hardness HRC value of the material is 42.8. Sample 3 is obtained. The composition of the sample is analyzed, and the results are shown in Table 1.
耐蚀实施例1:取上述样品1一样片,用砂纸磨光各面,用去离子水、酒精清洗干净,在100℃下烘干2小时,冷却,分别在青乳剂全浸泡和半浸泡两样品,浸泡时间分别为144小时、316小时和544小时。洗净腐蚀(HF∶HNO3∶H2O=1∶3∶7)后样品,进行金相观察(OLYMPUS)、扫描电镜(JSM-5800)和能谱仪(LINK ISIS)分析。发现合金腐蚀缓慢,约为0.000mm/a-0.0107mm/a属极耐腐蚀材料,均匀耐蚀率见附表4。Corrosion resistance example 1: Take the same piece of the above sample 1, polish each surface with sandpaper, clean it with deionized water and alcohol, dry it at 100°C for 2 hours, cool it, and soak it in green emulsion fully and half soaked respectively. For the samples, the immersion times were 144 hours, 316 hours and 544 hours, respectively. After cleaning the corroded samples (HF:HNO 3 :H 2 O=1:3:7), the samples were analyzed by metallographic observation (OLYMPUS), scanning electron microscope (JSM-5800) and energy spectrometer (LINK ISIS). It is found that the alloy corrodes slowly, about 0.000mm/a-0.0107mm/a is an extremely corrosion-resistant material, and the uniform corrosion resistance rate is shown in Attached Table 4.
耐蚀实施例2:感光乳剂中黄乳剂是腐蚀性最强,且半浸泡比全浸泡腐蚀性强,本实施例采取半浸泡腐蚀实验。用研磨膏研磨上述样品2一样片各面,用去离子水、酒精清洗干净,在100℃下烘干2小时,冷却,在黄乳剂浸泡该样片,浸泡时间为144小时,用蛋白酶溶液在室温下浸泡1小时后取出,洗净腐蚀后样品,进行金相观察、扫描电镜和能谱分析。发现合金腐蚀缓慢,约为0.03mm/a-0.04mm/a属极耐腐蚀材料,均匀耐蚀率见附表4。Corrosion resistance example 2: Yellow emulsion is the most corrosive among photosensitive emulsions, and half immersion is more corrosive than full immersion. This embodiment adopts half immersion corrosion experiment. Grind each side of the above-mentioned sample 2 with abrasive paste, clean with deionized water and alcohol, dry at 100°C for 2 hours, cool, soak the sample in yellow emulsion for 144 hours, and use protease solution at room temperature Take it out after submerging for 1 hour, clean the corroded sample, and carry out metallographic observation, scanning electron microscope and energy spectrum analysis. It is found that the alloy corrodes slowly, about 0.03mm/a-0.04mm/a is an extremely corrosion-resistant material, and the uniform corrosion resistance rate is shown in Attached Table 4.
耐蚀实施例3:取上述样品3一样片,使之洁净干燥后称重,另取大小相当重量相同双相钢样品,分别全浸泡和半浸泡于NaClO(0.8%W)溶液和NaOH(0.4%W)溶液中,控制温度40.2℃,分别浸泡6小时、8小时和12小时,取出洗净干燥称重,观察表面腐蚀情况。试验结果如附表4。Corrosion resistance example 3: Take the same piece of the above sample 3, make it clean and dry, weigh it, and take another dual-phase steel sample of the same size and weight, and soak it fully and half in NaClO (0.8% W) solution and NaOH (0.4% W) respectively. %W) solution, control the temperature at 40.2°C, soak for 6 hours, 8 hours and 12 hours respectively, take out, wash, dry and weigh, and observe the surface corrosion. The test results are shown in attached table 4.
缝隙耐蚀实施例4:取上述样品1一样片,试样经热处理后,先用磨掉样品氧化皮,然后在样品中间钻一个Φ100mm的孔,用砂纸磨光样片各面,用去离子水、酒精清洗干净,烘干冷却,将两片试样用纯钛螺栓拧紧,试样之间用两片δ0.2mm×1mm×15mm的钛片隔离开来,作出0.2mm的缝隙,将样品投入黄乳剂,浸泡144、480、984小时后取出,进行表面扫描电镜和能谱分析,发现浸泡144小时后没有发生明显腐蚀现象,能谱分析各元素含量如附表4。Example 4 of crevice corrosion resistance: Take the same piece of the above sample 1. After the sample is heat-treated, first grind off the scale of the sample, then drill a Φ100mm hole in the middle of the sample, use sandpaper to polish all sides of the sample, and use deionized water , alcohol cleaning, drying and cooling, tighten the two samples with pure titanium bolts, separate the samples with two titanium sheets of δ0.2mm×1mm×15mm, make a gap of 0.2mm, and put the samples into The yellow emulsion was taken out after soaking for 144, 480, and 984 hours, and the surface scanning electron microscope and energy spectrum analysis were carried out. It was found that no obvious corrosion occurred after soaking for 144 hours.
电化学耐蚀实施例5:取上述样品1一样片,在乳剂中的电化学腐蚀见附表4所示。Electrochemical Corrosion Resistance Example 5: Take a sample of the above-mentioned sample 1, and the electrochemical corrosion in the emulsion is shown in attached table 4.
照相性能试验实施例:取样品1尺寸为20mm×20mm×2mm样片精研,浸泡到SA-2彩纸黄乳剂中,在42℃下分别浸泡0小时、3小时、6小时和9小时,涂布片环观测其灰雾变化,发现材料对照相性能影响极小。试验数据如附表3。Photographic performance test example: Take sample 1 with a size of 20mm×20mm×2mm and grind it, soak it in SA-2 colored paper yellow emulsion, soak it at 42°C for 0 hour, 3 hours, 6 hours and 9 hours respectively, and coat Observing the change of the fog in the film ring, it is found that the influence of the material on the photographic performance is minimal. The test data are shown in attached table 3.
附表1:本发明钛合金材料成份分析数据
附表2:本发明钛合金硬度实验数据
附表3:照相性能实验数据Attached Table 3: Photographic Performance Experimental Data
附表4:本发明钛合金材料在各种介质中耐蚀性实验数据
从表中数据可以看出,本发明的钛合金材料的硬度和耐腐蚀性能不仅在多种介质特别是在高氯化银乳剂中满足照相业的特殊要求,而且不影响照相性能。It can be seen from the data in the table that the hardness and corrosion resistance of the titanium alloy material of the present invention not only meet the special requirements of the photographic industry in various media, especially in high silver chloride emulsions, but also do not affect the photographic performance.
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN02156614.3A CN1216164C (en) | 2002-12-17 | 2002-12-17 | Titanium alloy coated mould material for photographic trade and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN02156614.3A CN1216164C (en) | 2002-12-17 | 2002-12-17 | Titanium alloy coated mould material for photographic trade and manufacturing method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1508272A CN1508272A (en) | 2004-06-30 |
| CN1216164C true CN1216164C (en) | 2005-08-24 |
Family
ID=34236312
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN02156614.3A Expired - Fee Related CN1216164C (en) | 2002-12-17 | 2002-12-17 | Titanium alloy coated mould material for photographic trade and manufacturing method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1216164C (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101899590A (en) * | 2010-07-29 | 2010-12-01 | 江苏佳哲钛合金材料科技有限公司 | Titanium-aluminum-iron alloy |
| CN103667788B (en) * | 2012-09-14 | 2016-12-21 | 北京工业大学 | A kind of titanium alloy and Technology for Heating Processing |
| CN107479328B (en) * | 2017-08-07 | 2021-07-06 | 上海利正卫星应用技术有限公司 | Production method and production device of precoated photoresist magnesium plate |
-
2002
- 2002-12-17 CN CN02156614.3A patent/CN1216164C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN1508272A (en) | 2004-06-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5141566A (en) | Process for manufacturing corrosion-resistant seamless titanium alloy tubes and pipes | |
| CN101825200B (en) | Titanium alloy TC4 hot-rolled tube and production method thereof | |
| CN104152744A (en) | Low-cost medium-high-strength corrosion-resistant titanium alloy and processing method thereof | |
| CN108165822B (en) | Preparation method of TA2 cold-rolled titanium strip for low-strength and easy-to-form welded pipe | |
| CN107805741A (en) | A kind of preparation method of ti-ni shape memory alloy thin plate | |
| TWI261947B (en) | Titanium system material for fuel cell separator, and manufacturing method therefor | |
| CN109642273B (en) | Titanium alloy plate for electrode | |
| CN114405995B (en) | A method for preparing wide-width pure titanium foil tape | |
| CN1216164C (en) | Titanium alloy coated mould material for photographic trade and manufacturing method thereof | |
| CN116005049B (en) | Corrosion-resistant aluminum alloy profile and preparation method thereof | |
| JP3228134B2 (en) | Method for producing pure titanium plate excellent in formability and seizure resistance | |
| CN117344176B (en) | (Alpha+beta) titanium alloy for oil well pipe and preparation method thereof | |
| CN114774725B (en) | Preparation method of Gr4 strip for 3C electronic product | |
| CN120035685A (en) | Titanium materials, chemical device parts and chemical devices | |
| CN112481522B (en) | Zirconium alloy, preparation method of zirconium alloy and zirconium alloy section | |
| CN109825749A (en) | One kind can punching press aluminium alloy extrusions heat-and corrosion-resistant heat treatment method and aluminium alloy extrusions | |
| CN112458337B (en) | Zirconium alloy and preparation method of zirconium alloy profile | |
| CN112538571A (en) | Method for rolling ingot casting melted by residual titanium waste into plate | |
| CN112458338B (en) | Zirconium alloy, preparation method of zirconium alloy and zirconium alloy section | |
| JP2000248324A (en) | CORROSION RESISTANT Ti ALLOY | |
| JP3360535B2 (en) | Manufacturing method of decorative stainless steel sheet | |
| JPS6318673B2 (en) | ||
| CN120945251A (en) | A nickel-based NS600R alloy resistant to sulfuric acid corrosion and its preparation method | |
| CN119614940A (en) | Heat dissipation copper alloy foil for motor equipment and manufacturing process thereof | |
| CN115896540A (en) | A kind of Ti-Mo-Ni-Al-Zr corrosion-resistant titanium alloy and preparation method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20050824 Termination date: 20131217 |