会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明授权
    • Method of manufacturing high-temperature shape memory alloys
    • 制造高温形状记忆合金的方法
    • US5641364A
    • 1997-06-24
    • US549319
    • 1995-10-27
    • Dmitrii Victorovich GolbergKazuhiro OtsukaTatsuhiko UekiHiroshi HorikawaKengo Mitose
    • Dmitrii Victorovich GolbergKazuhiro OtsukaTatsuhiko UekiHiroshi HorikawaKengo Mitose
    • C22F1/00C22C1/02C22F1/16
    • C22F1/006
    • A method of manufacturing a high-temperature shape memory alloy includes the steps of cold-working a high-temperature shape memory alloy, in which a reverse martensite transformation start temperature (As) in a first heating after cold working reaches 350.degree. C. or above. Thereafter, the cold-worked alloy undergoes a first heat treatment for a period of time within the incubation time required for recrystallization or less, and at a temperature higher than a reverse martensite transformation finish temperature (Af). Finally, the resultant alloy is annealed with a second heat treatment, at a temperature which is not less than the plastic strain recovery temperature and not more than the recrystallization temperature. Specifically, the first heat treatment is performed for a period of three minutes or less at a temperature which exceeds 500.degree. C. and which is lower than the melting point of the alloy. The composition of the high-temperature shape memory alloy is Ti.sub.50 Ni.sub.50-x Pd.sub.x (x being 35 to 50 at %), Ti.sub.50-x Ni.sub.50 Zr.sub.x (x being 22 to 30 at %), Ti.sub.50-x Ni.sub.50 Hf.sub.x (x being 20 to 30 at %) or the like.
    • 制造高温形状记忆合金的方法包括冷加工高温形状记忆合金的步骤,其中冷加工后第一加热中的反向马氏体转变开始温度(As)达到350℃,或 以上。 此后,冷加工合金在再结晶所需的温育时间以下,以及高于反马氏体转变终止温度(Af)的温度下进行一段时间的第一次热处理。 最后,在不低于塑性应变恢复温度且不大于再结晶温度的温度下,将所得合金进行第二次热处理退火。 具体而言,在超过500℃,低于合金的熔点的温度下进行第1次热处理3分钟以下。 高温形状记忆合金的组成为Ti50Ni50-xPdx(x为35〜50原子%),Ti50-xNi50Zrx(x为22〜30原子%),Ti50-xNi50Hfx(x为20〜30原子%)或 类似。
    • 2. 发明授权
    • Ni-Ti-Pd superelastic alloy material, its manufacturing method, and
orthodontic archwire made of this alloy material
    • Ni-Ti-Pd超弹性合金材料,其制造方法和由该合金材料制成的正畸弓丝
    • US5951793A
    • 1999-09-14
    • US677299
    • 1996-07-09
    • Kengo MitoseTatsuhiko Ueki
    • Kengo MitoseTatsuhiko Ueki
    • A61C7/20C22C14/00C22F1/00C22F1/10
    • C22C14/00C22F1/006A61C2201/007A61C7/20
    • The present invention provides a Ni--Ti--Pd superelastic alloy material of a composition consisting of, by atomic percent, 34 to 49% nickel, 48 to 52% titanium and 3 to 14% palladium. Optionally, in a part of nickel and/or titanium of this alloy is replaced with one or more elements selected from a group of Cr, Fe, Co, V, Mn, B, Cu, Al, Nb, W and Zr such that these elements to be replaced amount to 2% or less in total (by atomic percent), wherein a stress hysteresis between the loading and unloading stresses in the stress-strain curve at temperatures between Af and Af+5.degree. is as small as 50 to 150 MPa. Since the Ni--Ti--Pd superelastic alloy material having the above composition is excellent in hot workability, it can be hot-worked into a wire having a diameter up to the range from 1 to 5 mm and manufactured at a low cost. Then, a final heat-treatment is given to the hot-worked material at a temperature in the range from 300 to 700.degree. C. through a step of final cold-drawing at a reduction ratio in a cross section area of not less than 20%, whereby an excellent superelastic material is obtained, with a stress hysteresis in the range from 50 to 150 MPa, and a residual strain of 0% or close to 0% after unloading, and which can be suitably used for an orthodontic archwire.
    • 本发明提供一种Ni-Ti-Pd超弹性合金材料,其组成为原子百分比为34-49%的镍,48-52%的钛和3-14%的钯。 任选地,在该合金的一部分镍和/或钛中,被选自Cr,Fe,Co,V,Mn,B,Cu,Al,Nb,W和Zr中的一种或多种元素代替,使得这些 待更换的元素总计为2%以下(原子百分比),其中在Af和Af + 5°之间的温度下,应力 - 应变曲线中的加载和卸载应力之间的应力滞后小至50至150 MPa。 由于具有上述组成的Ni-Ti-Pd超弹性合金材料的热加工性优异,因此可以将其热加工成直径为1〜5mm的线材,并以低成本制造。 然后,在300〜700℃的温度范围内对热加工材料进行最终的热处理,直到最终冷拉伸的步骤,以截面积为20以上的截面积 %,由此获得优异的超弹性材料,其应力滞后在50至150MPa的范围内,并且卸载后的残余应变为0%或接近0%,并且其可适用于正牙弓丝。
    • 3. 发明授权
    • Ni-Ti-Pd superelastic alloy material, its manufacturing method, and
orthodontic archwire made of this alloy material
    • Ni-Ti-Pd超弹性合金材料,其制造方法和由该合金材料制成的正畸弓丝
    • US5885381A
    • 1999-03-23
    • US28496
    • 1998-02-24
    • Kengo MitoseTatsuhiko Ueki
    • Kengo MitoseTatsuhiko Ueki
    • A61C7/20C22C14/00C22F1/00C21D8/06
    • C22C14/00C22F1/006A61C2201/007A61C7/20
    • The present invention provides a Ni--Ti--Pd superelastic alloy material of a composition consisting of, by atomic percent, 34 to 49% nickel, 48 to 52% titanium and 3 to 14% palladium. Optionally, a part of nickel and/or titanium of this alloy is replaced with one or more elements selected from a group of Cr, Fe, Co, V, Mn, B, Cu, Al, Nb, W and Zr such that these elements to be replaced amount to 2% or less in total (by atomic percent), wherein a stress hysteresis between the loading and unloading stresses in the stress-strain curve at temperatures between Af and Af+5.degree. is as small as 50 to 150 MPa. Since the Ni--Ti--Pd superelastic alloy material having the above composition is excellent in hot workability, it can be hot-worked into a wire having a diameter up to the range from 1 to 5 mm and manufactured at a low cost. Then, a final heat-treatment is given to the hot-worked material at a temperature in the range from 300.degree. to 700.degree. C. through a step of final cold-drawing at a reduction ratio in a cross section area of not less than 20%, whereby an excellent superelastic material is obtained, with a stress hysteresis in the range from 50 to 150 MPa, and a residual strain of 0% or close to 0% after unloading, and which can be suitably used for an orthodontic archwire.
    • 本发明提供一种Ni-Ti-Pd超弹性合金材料,其组成为原子百分比为34-49%的镍,48-52%的钛和3-14%的钯。 可选地,该合金的一部分镍和/或钛被选自Cr,Fe,Co,V,Mn,B,Cu,Al,Nb,W和Zr中的一种或多种元素代替,使得这些元素 待更换总量为2%以下(原子百分比),其中在Af和Af + 5°之间的温度下,应力 - 应变曲线中的加载和卸载应力之间的应力滞后小至50至150MPa 。 由于具有上述组成的Ni-Ti-Pd超弹性合金材料的热加工性优异,因此可以将其热加工成直径为1〜5mm的线材,并以低成本制造。 然后,在300〜700℃的温度范围内对热加工材料进行最终的热处理,通过最终冷拉拔的步骤,其截面积为不小于 20%,由此获得优异的超弹性材料,其应力滞后在50至150MPa的范围内,并且卸载后的残余应变为0%或接近0%,并且其可适用于正牙弓丝。