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    • 2. 发明申请
    • Method for producing low thermal expansion Ni-base superalloy
    • 生产低热膨胀Ni基超级合金的方法
    • US20050236079A1
    • 2005-10-27
    • US11115159
    • 2005-04-27
    • Shigeki UetaToshiharu NodaRyuichi YamamotoYoshikuni KadoyaRyotaro MagoshiShin Nishimoto
    • Shigeki UetaToshiharu NodaRyuichi YamamotoYoshikuni KadoyaRyotaro MagoshiShin Nishimoto
    • C22C19/03C22C19/05C22F1/00C22F1/10
    • C22C19/056C22C19/03C22C19/057C22C19/058C22F1/10
    • The present invention provides a method for producing a low thermal expansion Ni-base superalloy, which includes: preparing an alloy including, by weight %, C: 0.15% or less, Si: 1% or less, Mn: 1% or less, Cr: 5 to 20%, at least one of Mo, W and Re, which satisfy the relationship Mo+½(W+Re): 17 to 27%, Al: 0.1 to 2%, Ti: 0.1 to 2%, Nb and Ta, which satisfy the relationship Nb+Ta/2: 1.5% or less, Fe: 10% or less, Co: 5% or less, B: 0.001 to 0.02%, Zr: 0.001 to 0.2%, a reminder of Ni and inevitable components; subjecting the alloy to a solution heat treatment under the condition of at a temperature of 1000 to 1200° C.; subjecting the alloy to either a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides under the conditions of at a temperature of not less than 850° C. and less than 1000° C. and for 1 to 50 hours, or a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides by cooling from the temperature in the solution heat treatment to 850° C. at a cooling rate of 100° C. or less per hour; subjecting the alloy to a first aging treatment for precipitating γ′ phase under the conditions of at a temperature of 720 to 900° C. and for 1 to 50 hours; and subjecting the alloy to a second aging treatment for precipitating A2B phase under the conditions of at a temperature of 550 to 700° C. and for 5 to 100 hours.
    • 本发明提供一种低热膨胀型Ni基超合金的制造方法,其特征在于,包括:以重量%计含有C:0.15%以下,Si:1%以下,Mn:1%以下的合金, Cr:5〜20%,满足Mo +½(W + Re):17〜27%,Al:0.1〜2%,Ti:0.1〜2%的Mo,W和Re中的至少一种,Nb 和Ta,其满足Nb + Ta / 2:1.5%以下的关系,Fe:10%以下,Co:5%以下,B:0.001〜0.02%,Zr:0.001〜0.2%,提示Ni 和不可避免的组成部分; 在1000〜1200℃的温度下对合金进行固溶热处理; 使合金进行碳化物稳定化处理,在晶界上形成凝集碳化物,并在不低于850℃且小于1000℃的温度和1至50小时的条件下稳定碳化物,或 碳化物稳定化处理,用于通过从固溶热处理中的温度冷却至850℃,以每小时100℃或更低的冷却速度使晶界上的聚集碳化物稳定化; 在720〜900℃的温度和1〜50小时的条件下对合金进行第一时效处理以使γ相析出; 并在550-700℃的温度和5〜100小时的条件下对该合金进行第二时效处理以沉淀A 2 B相。
    • 3. 发明授权
    • Method for producing low thermal expansion Ni-base superalloy
    • 生产低热膨胀Ni基超级合金的方法
    • US08083874B2
    • 2011-12-27
    • US11115159
    • 2005-04-27
    • Shigeki UetaToshiharu NodaRyuichi YamamotoYoshikuni KadoyaRyotaro MagoshiShin Nishimoto
    • Shigeki UetaToshiharu NodaRyuichi YamamotoYoshikuni KadoyaRyotaro MagoshiShin Nishimoto
    • C22F1/10C22C19/05
    • C22C19/056C22C19/03C22C19/057C22C19/058C22F1/10
    • A method for producing a low thermal expansion Ni-base superalloy including the steps of subjecting the alloy to a solution heat treatment under the condition of at a temperature of 1000 to 1200° C. and subjecting the alloy to either a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides under the conditions of at a temperature of not less than 850° C. and less than 1000° C. and for 1 to 50 hours, or a carbide stabilizing treatment for making aggregated carbides on grain boundaries and stabilizing the carbides by cooling from the temperature in the solution heat treatment to 850° C. at a cooling rate of 100° C. or less per hour. The method also including the steps of subjecting the alloy to a first aging treatment for precipitating y′ phase under the conditions of at a temperature of 720 to 900° C. and for 1 to 50 hours, and subjecting the alloy to a second aging treatment for precipitating A2B phase under the conditions of at a temperature of 550 to 700° C. and for 5 to 100 hours.
    • 一种生产低热膨胀Ni基超合金的方法,包括以下步骤:在1000-1200℃的温度下对合金进行固溶热处理,并对合金进行碳化物稳定化处理 在不低于850℃,小于1000℃的温度和1〜50小时的条件下,在晶界上凝集的碳化物并使碳化物稳定,或者在晶界上形成碳化碳的碳化物稳定化处理 并且通过从固溶热处理中的温度冷却至850℃,以每小时100℃或更低的冷却速度来稳定碳化物。 该方法还包括以下步骤:在720至900℃的温度和1至50小时的条件下对合金进行第一时效处理以沉淀y相,并对合金进行第二时效处理 用于在550-700℃的温度和5-100小时的条件下沉淀A2B相。
    • 4. 发明授权
    • TiAl turbine rotor and method of manufacturing
    • TiAl涡轮转子及其制造方法
    • US6007301A
    • 1999-12-28
    • US953249
    • 1997-10-17
    • Toshiharu NodaMichio OkabeTakao Shimizu
    • Toshiharu NodaMichio OkabeTakao Shimizu
    • B23K1/00F01D5/02F01D5/04F01D5/28B63H1/28
    • B23K1/0018F01D5/025F01D5/043F01D5/28B23K2201/04F05D2230/23F05D2300/133F05D2300/173
    • A turbine rotor consisting of a wheel made of a TiAl alloy of good heat resistance and a rotor shaft made of a steel with good bonding strength is disclosed. As the shaft material a structural steel or a martensitic heat resistant steel is used. A TiAl turbine wheel made by precision casting is butted to the shaft with insertion of a brazing filler in the butted interfaces and stress of 0.01 kgf/mm.sup.2 or higher but lower than yield stress of the shaft is applied on the butted interfaces under heating by high frequency induction heating in atmosphere of an inert gas or a reducing gas to a temperature higher than the liquidus temperature of the brazing metal but not exceeding 100.degree. C. above the liquidus temperature. Turbine rotors with good accordance of the axes of the wheel and the shaft will be obtained by fitting a projection (or recess) and a recess (or projection) formed at the base of the wheel and the end of the shaft concentrically to the outer shape thereof, and by brazing the ring-shaped area outside the fitted parts.
    • 公开了一种涡轮转子,由具有良好耐热性的TiAl合金制成的车轮和由具有良好接合强度的钢制成的转子轴组成。 作为轴材料,使用结构钢或马氏体耐热钢。 通过精密铸造制成的TiAl涡轮机叶片在对接界面上插入钎焊料,并且在0.01kgf / mm2以上的应力下被接合到轴上,但低于在加热下的对接界面上的屈服应力高 在惰性气体或还原气体的气氛中进行高频感应加热至比钎焊金属的液相线温度高但不超过液相温度100℃以上的温度。 通过将形成在车轮的底部和轴的端部的突起(或凹部)和凹部(或凸起)同心地配合到外部形状来获得与车轮和轴的轴线良好一致的涡轮转子 并且通过将环形区域钎焊在装配部件的外部。
    • 5. 发明授权
    • Titanium alloy having good heat resistance and method of producing parts therefrom
    • 具有良好耐热性的钛合金及其制造方法
    • US06284071B1
    • 2001-09-04
    • US09261388
    • 1999-03-03
    • Akihiro SuzukiToshiharu NodaMichio Okabe
    • Akihiro SuzukiToshiharu NodaMichio Okabe
    • C22F118
    • C22F1/183C22C14/00
    • A titanium alloy having improved heat resistance in addition to the inherent properties of lightness and corrosion resistance. The alloy consists essentially of, by weight %, Al: 5.0-7.0%, Sn: 3.0-5.0%, Zr: 2.5-6.0%, Mo: 2.0-4.0%, Si: 0.05-0.80%, C: 0.001-0.200%, O: 0.05-0.20%, optionally further one or two of Nb and Ta: 0.3-2.0%, and the balance of Ti and inevitable impurities. A method of producing parts from this alloy comprises subjecting the titanium alloy of the above described alloy composition to heat treatment at a temperature of &bgr;-region, combination of rapid cooling and slow cooling or combination of water quenching and annealing, hot processing in &agr;+&bgr; region, solution treatment and aging treatment.
    • 除耐酸性和耐腐蚀性的固有特性外,还具有耐热性提高的钛合金。 该合金主要由Al:5.0-7.0%,Sn:3.0-5.0%,Zr:2.5-6.0%,Mo:2.0-4.0%,Si:0.05-0.80%,C:0.001-0.200重量%组成 %,O:0.05-0.20%,任选进一步的Nb和Ta中的一种或两种:0.3-2.0%,余量为Ti和不可避免的杂质。 从该合金制造零件的方法包括将上述合金组合物的钛合金在β区域的温度下进行热处理,快速冷却和缓慢冷却的组合或水淬和退火的组合,α+ β区,溶液处理和时效处理。