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    • 3. 发明授权
    • Methods and systems for predicting very high cycle fatigue properties in metal alloys
    • 用于预测金属合金中非常高的循环疲劳性能的方法和系统
    • US08155940B2
    • 2012-04-10
    • US12182314
    • 2008-07-30
    • Qigui WangBob R. Powell, Jr.Peggy E. JonesCherng-Chi Chang
    • Qigui WangBob R. Powell, Jr.Peggy E. JonesCherng-Chi Chang
    • G06G7/48
    • G06F17/5009G06F2217/10G06F2217/16G06F2217/76
    • A system and method for predicting fatigue life in metal alloys for very high cycle fatigue applications. The system and method are especially useful for cast metal alloys, such as cast aluminum alloys, where a fatigue endurance limit is either non-existent or hard to discern. Fatigue properties, such as fatigue strength in the very high cycle fatigue region, are based on a modified random fatigue limit model, where the very high cycle fatigue strength and infinite life fatigue strength are refined to take into consideration the sizes of the discontinuities and microstructure constituents since the fatigue life scatter depends upon the presence of discontinuities and microstructure constituents. The sizes of the discontinuities and microstructure constituents that can initiate fatigue cracks can be determined with extreme value statistics, then input to the modified random fatigue limit model.
    • 用于预测非常高循环疲劳应用中金属合金疲劳寿命的系统和方法。 该系统和方法对于铸造金属合金(例如铸铝合金)尤其有用,其中疲劳耐力极限不存在或难以辨别。 疲劳性能,如非常高的循环疲劳区域的疲劳强度,基于改进的随机疲劳极限模型,其中非常高的循环疲劳强度和无限寿命疲劳强度得到细化,以考虑到不连续性和微观结构的尺寸 因为疲劳寿命分散取决于不连续性和微结构组分的存在。 可以用极值统计量确定可以引发疲劳裂纹的不连续性和微观组分的尺寸,然后输入到修改的随机疲劳极限模型。
    • 4. 发明授权
    • Artificial aging process for aluminum alloys
    • 铝合金人造老化工艺
    • US08323425B2
    • 2012-12-04
    • US12042639
    • 2008-03-05
    • Qigui WangPeggy E. Jones
    • Qigui WangPeggy E. Jones
    • C21D11/00C22C21/00C22F1/04
    • C22C21/00C22F1/04
    • Embodiments of a method for non-isothermally aging an aluminum alloy are provided. The method comprises heating an aluminum alloy at a first ramp-up rate to a maximum temperature below a precipitate solvus value, cooling the alloy at a first cooling rate sufficient to produce a maximum number of primary precipitates, cooling at a second cooling rate until a minimum temperature is reached wherein the growth rate of primary precipitates is equal to or substantially zero, and heating the alloy at a second ramp-up rate to a temperature sufficient to produce a maximum number of secondary precipitates.
    • 提供了一种非等温老化铝合金的方法的实施例。 该方法包括将铝合金以第一加速速率加热至低于沉淀溶质值的最高温度,以足以产生最大数量的一次沉淀的第一冷却速率冷却合金,以第二冷却速率冷却至 达到最初温度,其中初级沉淀物的生长速率等于或基本上为零,并且以第二升温速率将合金加热至足以产生最大数量的二次沉淀物的温度。
    • 5. 发明申请
    • METHODS AND SYSTEMS TO PREDICT FATIGUE LIFE IN ALUMINUM CASTINGS
    • 在铝铸件中预测疲劳寿命的方法和系统
    • US20090276166A1
    • 2009-11-05
    • US12114875
    • 2008-05-05
    • Qigui WangPeggy E. Jones
    • Qigui WangPeggy E. Jones
    • G06F19/00G06F15/00
    • G06F17/5009G01M5/0033G06F2217/10
    • Methods and systems of predicting fatigue life in aluminum castings that combines extreme values of both casting flaws and microstructures with multiscale life models. The multiscale life models account for differing fatigue crack initiation based on the size scale of the defect and microstructure features, including provisions for generally millimeter scale casting flaws, generally micrometer scale second phase particles by cracking or debonding, or submicrometer scale dislocation interactions with precipitates which form persistent slip bands. In the presence of casting flaws, the fatigue initiation life is negligible and the total fatigue life is spent in propagation of a fatigue crack from such flaws. In the absence of casting flaws, however, the total fatigue life is spent in both crack initiation and propagation, except for the case where fatigue cracks initiate from large second phase particles in a coarse microstructure. The extreme values of casting flaws, second phase particles, mean free path through an aluminum matrix or grain sizes are obtained from extreme value statistics when two or three dimensional sizes of casting flaws and microstructure features are provided by either direct measurement or analytical prediction. The upper bound flaw or microstructure feature size is calculated by extreme value statistics.
    • 预测铝铸件疲劳寿命的方法和系统,其将铸造缺陷和微观结构的极值与多尺度寿命模型相结合。 多尺度寿命模型基于缺陷和微结构特征的尺寸规模来考虑不同的疲劳裂纹开始,包括通常为毫米级铸造缺陷的规定,通常是通过裂纹或剥离的微米级第二相颗粒,或与沉淀物的亚微米级位错相互作用 形成持续滑带。 在存在铸造缺陷的情况下,疲劳起始寿命可以忽略不计,并且疲劳寿命用于从这种缺陷传播疲劳裂纹。 然而,在没有铸造缺陷的情况下,除了在粗糙微结构中的大的第二相颗粒引发疲劳裂纹的情况下,总的疲劳寿命也用于裂纹开始和扩展。 通过直接测量或分析预测提供铸造瑕疵和微结构特征的两维或三维尺寸时,铸造缺陷,第二相颗粒,平均通过铝基体或颗粒尺寸的自由程的极值来自极值统计。 通过极值统计计算上界缺陷或微结构特征尺寸。
    • 8. 发明申请
    • METHODS AND SYSTEMS FOR PREDICTING VERY HIGH CYCLE FATIGUE PROPERTIES IN METAL ALLOYS
    • 用于预测金属合金中非常高的周期疲劳特性的方法和系统
    • US20100030537A1
    • 2010-02-04
    • US12182314
    • 2008-07-30
    • Qigui WangBob R. Powell, JR.Peggy E. JonesCherng-Chi Chang
    • Qigui WangBob R. Powell, JR.Peggy E. JonesCherng-Chi Chang
    • G06G7/48
    • G06F17/5009G06F2217/10G06F2217/16G06F2217/76
    • A system and method for predicting fatigue life in metal alloys for very high cycle fatigue applications. The system and method are especially useful for cast metal alloys, such as cast aluminum alloys, where a fatigue endurance limit is either non-existent or hard to discern. Fatigue properties, such as fatigue strength in the very high cycle fatigue region, are based on a modified random fatigue limit model, where the very high cycle fatigue strength and infinite life fatigue strength are refined to take into consideration the sizes of the discontinuities and microstructure constituents since the fatigue life scatter depends upon the presence of discontinuities and microstructure constituents. The sizes of the discontinuities and microstructure constituents that can initiate fatigue cracks can be determined with extreme value statistics, then input to the modified random fatigue limit model.
    • 用于预测非常高循环疲劳应用中金属合金疲劳寿命的系统和方法。 该系统和方法对于铸造金属合金(例如铸铝合金)尤其有用,其中疲劳耐力极限不存在或难以辨别。 疲劳性能,如非常高的循环疲劳区域的疲劳强度,基于改进的随机疲劳极限模型,其中非常高的循环疲劳强度和无限寿命疲劳强度得到细化,以考虑到不连续性和微观结构的尺寸 因为疲劳寿命分散取决于不连续性和微结构组分的存在。 可以用极值统计量确定可以引发疲劳裂纹的不连续性和微观组分的尺寸,然后输入到修改的随机疲劳极限模型。
    • 9. 发明授权
    • Methods and systems to predict fatigue life in aluminum castings
    • 预测铝铸件疲劳寿命的方法和系统
    • US07623973B1
    • 2009-11-24
    • US12114875
    • 2008-05-05
    • Qigui WangPeggy E. Jones
    • Qigui WangPeggy E. Jones
    • G01B3/44G06F7/60
    • G06F17/5009G01M5/0033G06F2217/10
    • Methods and systems of predicting fatigue life in aluminum castings that combines extreme values of both casting flaws and microstructures with multiscale life models. The multiscale life models account for differing fatigue crack initiation based on the size scale of the defect and microstructure features, including provisions for generally millimeter scale casting flaws, generally micrometer scale second phase particles by cracking or debonding, or submicrometer scale dislocation interactions with precipitates which form persistent slip bands. In the presence of casting flaws, the fatigue initiation life is negligible and the total fatigue life is spent in propagation of a fatigue crack from such flaws. In the absence of casting flaws, however, the total fatigue life is spent in both crack initiation and propagation, except for the case where fatigue cracks initiate from large second phase particles in a coarse microstructure.
    • 预测铝铸件疲劳寿命的方法和系统,其将铸造缺陷和微观结构的极值与多尺度寿命模型相结合。 多尺度寿命模型基于缺陷和微结构特征的尺寸规模来考虑不同的疲劳裂纹开始,包括通常为毫米级铸造缺陷的规定,通常是通过裂纹或剥离的微米级第二相颗粒,或与沉淀物的亚微米级位错相互作用 形成持续滑带。 在存在铸造缺陷的情况下,疲劳起始寿命可以忽略不计,并且疲劳寿命用于从这种缺陷传播疲劳裂纹。 然而,在没有铸造缺陷的情况下,除了在粗糙微结构中的大的第二相颗粒引发疲劳裂纹的情况下,总的疲劳寿命也用于裂纹开始和扩展。