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    • 4. 发明授权
    • Computerized method and system for designing an aerodynamic focusing lens stack
    • 用于设计气动聚焦透镜叠层的计算机化方法和系统
    • US08065119B2
    • 2011-11-22
    • US12052597
    • 2008-03-20
    • Eric GardVincent RiotKeith CoffeeBruce WoodsHerbert TobiasJim BirchTodd Weisgraber
    • Eric GardVincent RiotKeith CoffeeBruce WoodsHerbert TobiasJim BirchTodd Weisgraber
    • G06F17/50
    • G01N1/24G01N1/22G01N2001/2223G01N2001/244G01N2015/0026G01N2015/0046
    • A computerized method and system for designing an aerodynamic focusing lens stack, using input from a designer related to, for example, particle size range to be considered, characteristics of the gas to be flowed through the system, the upstream temperature and pressure at the top of a first focusing lens, the flow rate through the aerodynamic focusing lens stack equivalent at atmosphere pressure; and a Stokes number range. Based on the design parameters, the method and system determines the total number of focusing lenses and their respective orifice diameters required to focus the particle size range to be considered, by first calculating for the orifice diameter of the first focusing lens in the Stokes formula, and then using that value to determine, in iterative fashion, intermediate flow values which are themselves used to determine the orifice diameters of each succeeding focusing lens in the stack design, with the results being output to a designer. In addition, the Reynolds numbers associated with each focusing lens as well as exit nozzle size may also be determined to enhance the stack design.
    • 用于设计空气动力学聚焦透镜叠层的计算机化方法和系统,使用来自设计者的输入,例如要考虑的粒度范围,要流过系统的气体的特性,顶部的上游温度和压力 的第一聚焦透镜,通过空气动力学聚焦透镜叠层在大气压下相当的流速; 和斯托克斯号码范围。 基于设计参数,方法和系统通过首先计算斯托克斯公式中的第一聚焦透镜的孔直径来确定聚焦透镜的总数及其相应的孔径直径,以聚焦要考虑的粒度范围, 然后使用该值以迭代方式确定本身用于确定堆叠设计中每个后续聚焦透镜的孔口直径的中间流量值,其结果被输出给设计者。 此外,还可以确定与每个聚焦透镜相关联的雷诺数以及出口喷嘴尺寸以增强堆叠设计。
    • 5. 发明申请
    • Computerized Method and System for Designing an Aerodynamic Focusing Lens Stack
    • 用于设计气动聚焦镜头叠层的计算机化方法和系统
    • US20080221842A1
    • 2008-09-11
    • US12052597
    • 2008-03-20
    • Eric GardVincent RiotKeith CoffeeBruce WoodsHerbert TobiasJim BirchTodd Weisgraber
    • Eric GardVincent RiotKeith CoffeeBruce WoodsHerbert TobiasJim BirchTodd Weisgraber
    • G06F17/50G06F17/10
    • G01N1/24G01N1/22G01N2001/2223G01N2001/244G01N2015/0026G01N2015/0046
    • A computerized method and system for designing an aerodynamic focusing lens stack, using input from a designer related to, for example, particle size range to be considered, characteristics of the gas to be flowed through the system, the upstream temperature and pressure at the top of a first focusing lens, the flow rate through the aerodynamic focusing lens stack equivalent at atmosphere pressure; and a Stokes number range. Based on the design parameters, the method and system determines the total number of focusing lenses and their respective orifice diameters required to focus the particle size range to be considered, by first calculating for the orifice diameter of the first focusing lens in the Stokes formula, and then using that value to determine, in iterative fashion, intermediate flow values which are themselves used to determine the orifice diameters of each succeeding focusing lens in the stack design, with the results being output to a designer. In addition, the Reynolds numbers associated with each focusing lens as well as exit nozzle size may also be determined to enhance the stack design.
    • 用于设计空气动力学聚焦透镜叠层的计算机化方法和系统,使用来自设计者的输入,例如要考虑的粒度范围,要流过系统的气体的特性,顶部的上游温度和压力 的第一聚焦透镜,通过空气动力学聚焦透镜叠层在大气压下相当的流速; 和斯托克斯号码范围。 基于设计参数,方法和系统通过首先计算斯托克斯公式中的第一聚焦透镜的孔直径来确定聚焦透镜的总数及其相应的孔径直径,以聚焦要考虑的粒度范围, 然后使用该值以迭代方式确定本身用于确定堆叠设计中每个后续聚焦透镜的孔口直径的中间流量值,其结果被输出给设计者。 此外,还可以确定与每个聚焦透镜相关联的雷诺数以及出口喷嘴尺寸以增强堆叠设计。