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    • 161. 发明授权
    • System, method, and computer program product to provide wireless sensing based on an aggregate magnetic field reading
    • 系统,方法和计算机程序产品,提供基于集合磁场读数的无线传感
    • US09329020B1
    • 2016-05-03
    • US13732957
    • 2013-01-02
    • Lockheed Martin Corporation
    • Nathaniel Napoletano
    • G01B7/24G06F19/00G01B7/14G06F17/00
    • G06F17/00G09B9/00G09B23/18
    • A system including a plurality of actuation devices with each actuation device configured to have a magnetized part which moves to a designated position representative of a designated manipulation, when at least one actuation device is manipulated, a magnetic sensor array configured to measure a composite magnetic field produced by the magnetized parts of the plurality of actuation devices, an acquisition device configured to acquire magnetic field data from the sensor array indicative of the measured composite magnetic field, a converter configured to convert the acquired composite magnetic field data into analog values, and a processor configured to evaluate to the analog values to determine which of the at least one activation device is manipulated, how the manipulation reflects collective operation of the plurality of actuation devices, and/or to provide a response indicative of the manipulation. A method and a computer program product are also disclosed.
    • 一种包括多个致动装置的系统,其中每个致动装置被配置为当操纵至少一个致动装置时具有移动到代表指定操纵的指定位置的磁化部分,构造成测量复合磁场的磁传感器阵列 由所述多个致动装置的磁化部分产生的获取装置,被配置为从所述传感器阵列获取指示所述测量的复合磁场的磁场数据的获取装置,被配置为将所获取的复合磁场数据转换为模拟值的转换器,以及 处理器,被配置为评估所述模拟值以确定所述至少一个激活装置中的哪个被操纵,所述操作如何反映所述多个致动装置的集体操作,和/或提供指示所述操纵的响应。 还公开了一种方法和计算机程序产品。
    • 166. 发明申请
    • AIRCRAFT VEHICULAR PROPULSION SYSTEM MONITORING DEVICE AND METHOD
    • 飞机车辆推进系统监控装置及方法
    • US20090055129A1
    • 2009-02-26
    • US12099461
    • 2008-04-08
    • Russell E. AltieriJames F. KuhnMark R. JollySteve C. SouthwardAskari Badre-AlamLeslie P. FowlerMatthew Ferguson
    • Russell E. AltieriJames F. KuhnMark R. JollySteve C. SouthwardAskari Badre-AlamLeslie P. FowlerMatthew Ferguson
    • G01B7/24G06F15/00
    • B64C29/005B64F5/60G01B7/31
    • Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vertical propulsion dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The collar misalignment measuring system of the invention provide a misalignment measurement of the propulsion system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.
    • 描述了用于监测飞行器推进系统中的旋转轴轴和联轴器的方法和系统。 测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。 测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机,其中垂直推进动态旋转驱动轴系统和联轴器被实时监控。 车轴联轴器未对准测量系统利用多个位置传感器来提供对推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。 传感器的相对位置通过结构框架从旋转目标的外部刚性固定。 本发明的套环未对准测量系统提供了推进系统驱动轴柔性联轴器的不对准测量,其涉及在飞行器车辆的操作中的旋转轴联轴器的关键性能。 该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。