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    • 2. 发明授权
    • Aircraft brake health monitoring system and method
    • 飞机制动器健康监测系统及方法
    • US09242628B2
    • 2016-01-26
    • US13943360
    • 2013-07-16
    • HONEYWELL INTERNATIONAL INC.
    • Dinkar MylaraswamyAndrew Peter VechartMark E. BehnkeRichard Rateick, Jr.Emmanuel Obiesie NwadiogbuGiles HorbanMatthew Brown
    • B60T17/22B64C25/42F16D55/36B60T8/88
    • B60T17/221B60T8/885B60T2270/406B64C25/42F16D55/36
    • A system method of estimating health of aircraft brake system friction material includes sensing a temperature of the friction material, and supplying the sensed temperature to a processor-implemented thermal model that is configured to estimate friction material temperatures at one or more locations on the friction material. The estimates of friction material temperatures are supplied to a processor-implemented thermal oxidation model that is configured, based on the estimates of friction material temperatures, to estimate friction material loss due to thermal oxidation. Data representative of runway fluid exposure are supplied to a processor-implemented catalytic oxidation model that is configured, based on the runway fluid exposure, to estimate friction material loss due to catalytic oxidation. The health of the friction material is estimated based on the estimates of friction material loss from the processor-implemented thermal oxidation model and the processor-implemented catalytic oxidation model.
    • 估计飞机制动系统摩擦材料的健康的系统方法包括感测摩擦材料的温度,并将检测到的温度提供给处理器实施的热模型,其被配置为估计摩擦材料上的一个或多个位置处的摩擦材料温度 。 摩擦材料温度的估计被提供给处理器实施的热氧化模型,其基于摩擦材料温度的估计被配置为估计由于热氧化引起的摩擦材料损失。 跑道流体暴露的代表数据被提供给基于跑道流体暴露构造的处理器实施的催化氧化模型,以估计由于催化氧化引起的摩擦材料损失。 基于处理器实施的热氧化模型和处理器实施的催化氧化模型的摩擦材料损耗的估计,估计摩擦材料的健康。
    • 4. 发明申请
    • ENVIRONMENTAL CONTROL SYSTEMS AND TECHNIQUES FOR MONITORING HEAT EXCHANGER FOULING
    • 环境调控系统及监控热交换器的技术
    • US20140008035A1
    • 2014-01-09
    • US13930568
    • 2013-06-28
    • HONEYWELL INTERNATIONAL INC.
    • Ravindra PatankarSunil MenonEmmanuel Obiesie Nwadiogbu
    • G01N17/00F28F27/00
    • G01N17/008B64D13/00F28F27/00G05B23/0221
    • Environmental control systems and techniques for monitoring heat exchanger fouling are provided herein. In an embodiment, a technique for monitoring heat exchanger fouling includes providing a correlation of heat exchanger fouling to an operating variable. The correlation is programmed into a maintenance system that includes a processor that is adapted to receive data regarding the operating variable. The operating variable is chosen from inlet temperatures of input streams into the heat exchanger and outlet temperatures of output streams out of the heat exchanger, heat exchanger pressure drop, overall heat transfer coefficient value, speed of rotation of an air conditioning machine that includes the heat exchanger, and combinations thereof. Data regarding the operating variable is gathered via a sensor that is adapted to measure the operating variable. The measured operating variable is determined to correspond to excessive heat exchanger fouling in accordance with the correlation using the processor.
    • 本文提供了用于监测热交换器结垢的环境控制系统和技术。 在一个实施例中,用于监测热交换器结垢的技术包括提供热交换器结垢与操作变量的相关性。 相关性被编程到维护系统中,该维护系统包括适于接收关于操作变量的数据的处理器。 操作变量选自进入热交换器的输入流的入口温度和热交换器外的输出流的出口温度,热交换器压降,总体传热系数值,包括热量的空调机的旋转速度 交换器及其组合。 关于操作变量的数据通过适于测量操作变量的传感器来收集。 根据使用该处理器的相关性,测量的操作变量被确定为对应于过热的热交换器结垢。
    • 5. 发明申请
    • AIRCRAFT BRAKE HEALTH MONITORING SYSTEM AND METHOD
    • 飞机制动健康监测系统及方法
    • US20150025735A1
    • 2015-01-22
    • US13943360
    • 2013-07-16
    • HONEYWELL INTERNATIONAL INC.
    • Dinkar MylaraswamyAndrew Peter VechartMark E. BehnkeRichard Rateick, Jr.Emmanuel Obiesie NwadiogbuGiles HorbanMatthew Brown
    • B60T17/22
    • B60T17/221B60T8/885B60T2270/406B64C25/42F16D55/36
    • A system method of estimating health of aircraft brake system friction material includes sensing a temperature of the friction material, and supplying the sensed temperature to a processor-implemented thermal model that is configured to estimate friction material temperatures at one or more locations on the friction material. The estimates of friction material temperatures are supplied to a processor-implemented thermal oxidation model that is configured, based on the estimates of friction material temperatures, to estimate friction material loss due to thermal oxidation. Data representative of runway fluid exposure are supplied to a processor-implemented catalytic oxidation model that is configured, based on the runway fluid exposure, to estimate friction material loss due to catalytic oxidation. The health of the friction material is estimated based on the estimates of friction material loss from the processor-implemented thermal oxidation model and the processor-implemented catalytic oxidation model.
    • 估计飞机制动系统摩擦材料的健康的系统方法包括感测摩擦材料的温度,并将检测到的温度提供给处理器实施的热模型,其被配置为估计摩擦材料上的一个或多个位置处的摩擦材料温度 。 摩擦材料温度的估计被提供给处理器实施的热氧化模型,该热氧化模型基于摩擦材料温度的估计来估计由于热氧化引起的摩擦材料损失。 跑道流体暴露的代表数据被提供给基于跑道流体暴露构造的处理器实施的催化氧化模型,以估计由于催化氧化引起的摩擦材料损失。 基于处理器实施的热氧化模型和处理器实施的催化氧化模型的摩擦材料损耗的估计,估计摩擦材料的健康。