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    • 6. 发明申请
    • METHODS FOR PROCESSING TITANIUM ALLOYS
    • 加工钛合金的方法
    • WO2014093009A1
    • 2014-06-19
    • PCT/US2013/071801
    • 2013-11-26
    • ATI PROPERTIES, INC.
    • BRYAN, David J.MANTIONE, John V.THOMAS, Jean-Philippe
    • C22C14/00C22F1/18
    • C22F1/183C22C14/00
    • Methods of refining the grain size of a titanium alloy workpiece include beta annealing the workpiece, cooling the beta annealed workpiece to a temperature below the beta transus temperature of the titanium alloy, and high strain rate multi-axis forging the workpiece. High strain rate multi-axis forging is employed until a total strain of at least 1 is achieved in the titanium alloy workpiece, or until a total strain of at least 1 and up to 3.5 is achieved in the titanium alloy workpiece. The titanium alloy of the workpiece may comprise at least one of grain pinning alloying additions and beta stabilizing content effective to decrease alpha phase precipitation and growth kinetics.
    • 精炼钛合金工件的晶粒尺寸的方法包括对工件进行β退火,将β退火工件冷却至低于钛合金的β转变温度的温度,以及高应变速率多轴锻造工件。 使用高应变率多轴锻造,直到在钛合金工件中达到至少为1的总应变,或者直到在钛合金工件中达到至少1和高达3.5的总应变为止。 工件的钛合金可以包括有效减少α相沉淀和生长动力学的颗粒钉扎合金添加剂和β稳定化成分中的至少一种。
    • 8. 发明申请
    • THERMO-MECHANICAL PROCESSING OF NICKEL-BASE ALLOYS
    • 镍基合金的热机械加工
    • WO2012166295A2
    • 2012-12-06
    • PCT/US2012036707
    • 2012-05-07
    • ATI PROPERTIES INCFORBES JONES ROBIN MROCK CHRISTOPHER A
    • FORBES JONES ROBIN MROCK CHRISTOPHER A
    • C22C19/05C22F1/10
    • C22C19/058B21D22/022B21J1/06C22C19/05C22F1/10
    • A thermo-mechanical treatment process is disclosed. A nickel-base alloy workpiece is heated in a first heating step to a temperature greater than the M23C6 carbide solvus temperature of the nickel-base alloy. The nickel-base alloy workpiece is worked in a first working step to a reduction in area of 20% to 70%. The nickel-base alloy workpiece is at a temperature greater than the M23C6 carbide solvus temperature when the first working step begins. The nickel-base alloy workpiece is heated in a second working step to a temperature greater than 1700 F (926 C) and less than the M23C6 carbide solvus temperature of the nickel-base alloy. The nickel-base alloy workpiece is not permitted to cool to ambient temperature between completion of the first working step and the beginning of the second heating step. The nickel-base alloy workpiece is worked to a second reduction in area of 20% to 70%. The nickel-base alloy workpiece is at a temperature greater than 1700 F (926 C) and less than the M23C6 carbide solvus temperature of the nickel-base alloy when the second working step begins.
    • 公开了一种热机械处理方法。 将镍基合金工件在第一加热步骤中加热到大于镍基合金的M23C6碳化物溶质温度的温度。 镍基合金工件在第一工作步骤中加工,以减少20%至70%的面积。 当第一工作步骤开始时,镍基合金工件处于大于M23C6碳化物溶质温度的温度。 镍基合金工件在第二工作步骤中被加热至高于1700°F(926℃)且小于镍基合金的M23C6碳化物溶质温度的温度。 镍基合金工件在第一工作步骤完成和第二加热步骤开始之间不允许冷却至环境温度。 镍基合金工件的工作面积为20%至70%的第二次减少。 当镍基合金工件在第二工作步骤开始时,其温度高于1700°F(926℃)且小于镍基合金的M23C6碳化物溶质温度。