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    • 22. 发明授权
    • Hot stretch straightening of high strength α/β processed titanium
    • 高强度α/β加工钛的热拉伸矫直
    • US08499605B2
    • 2013-08-06
    • US12845122
    • 2010-07-28
    • David J. Bryan
    • David J. Bryan
    • C22F1/18B21D3/12
    • B21D3/12C22F1/183
    • A method for straightening a solution treated and aged (STA) titanium alloy form includes heating an STA titanium alloy form to a straightening temperature of at least 25° F. below the age hardening temperature, and applying an elongation tensile stress for a time sufficient to elongate and straighten the form. The elongation tensile stress is at least 20% of the yield stress and not equal to or greater than the yield stress at the straightening temperature. The straightened form deviates from straight by no greater than 0.125 inch over any 5 foot length or shorter length. The straightened form is cooled while simultaneously applying a cooling tensile stress that balances the thermal cooling stress in the titanium alloy form to thereby maintain a deviation from straight of no greater than 0.125 inch over any 5 foot length or shorter length.
    • 用于矫正溶液处理和老化(STA)钛合金形式的方法包括将STA钛合金形式加热至低于时效硬化温度至少25°F的矫直温度,并且将延伸拉伸应力施加足够的时间 伸长和拉直形式。 伸长拉伸应力是屈服应力的至少20%,不等于或大于矫直温度下的屈服应力。 拉直的形状在任何5英尺长度或更短的长度上从直线偏离不大于0.125英寸。 将矫直形式冷却,同时施加平衡钛合金形式的热冷应力的冷却拉伸应力,从而在任何5英尺长度或更短长度上保持与直线偏差不大于0.125英寸。
    • 24. 发明申请
    • NICKEL-BASE ALLOY HEAT TREATMENTS, NICKEL-BASE ALLOYS, AND ARTICLES INCLUDING NICKEL-BASE ALLOYS
    • 镍基合金热处理,镍基合金和包括镍基合金的文章
    • US20130133793A1
    • 2013-05-30
    • US13307097
    • 2011-11-30
    • Erin T. McDevitt
    • Erin T. McDevitt
    • C22F1/10C22C19/05C22C30/00C22F1/00
    • C22C19/056C22C19/055C22F1/10
    • A method for heat treating a 718-type nickel-base comprises heating a 718-type nickel-base alloy to a heat treating temperature, and holding the alloy at the heat treating temperature for a heat treating time sufficient to form an equilibrium or near-equilibrium concentration of δ-phase grain boundary precipitates within the nickel-base alloy and up to 25 percent by weight of total γ′-phase and γ″-phase. The 718-type nickel-base alloy is air cooled. The present disclosure also includes a 718-type nickel-base alloy comprising a near-equilibrium concentration of δ-phase grain boundary precipitates and up to 25 percent by weight of total γ′-phase and γ″-phase precipitates. Alloys according to the disclosure may be included in articles of manufacture such as, for example, face sheet, honeycomb core elements, and honeycomb panels for thermal protection systems for hypersonic flight vehicles and space vehicles.
    • 用于热处理718型镍基的方法包括将718型镍基合金加热至热处理温度,并将该合金在热处理温度下保持足以形成平衡或近似的热处理时间, 镍基合金内的δ相晶界析出物的平衡浓度高达总γ相和γ相的25%(重量)。 718型镍基合金是空气冷却的。 本公开还包括718型镍基合金,其包含近平衡浓度的δ相晶界析出物和高达25重量%的总γ相和γ'相析出物。 根据本公开的合金可以包括在制造品中,例如面板,蜂窝芯元件和用于超音速飞行器车辆和太空车辆的热保护系统的蜂窝板。