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    • 1. 发明申请
    • Wireless rotor track and balance system for rotorcraft
    • 用于旋翼航空器的无线转子轨道和平衡系统
    • US20120078544A1
    • 2012-03-29
    • US12924466
    • 2010-09-28
    • Michael A. LynchMokhtar SadokRadoslaw R. Zakrzewski
    • Michael A. LynchMokhtar SadokRadoslaw R. Zakrzewski
    • G01M1/22
    • B64C27/008
    • Disclosed is a rotor track and balance system for rotorcraft that includes a data processing unit, a tachometer sensor and at least one accelerometer. The tachometer sensor is located remotely from the data processing unit and is mounted proximate to the rotating blades of the rotorcraft. The tachometer sensor is adapted to measure the speed and position of the rotating blades and to wirelessly transmit speed and position data to the data processor. The at least one accelerometer is also located remotely from the data processing unit and is mounted proximate the rotating blades of the rotorcraft. Each accelerometer is adapted to measure vibration anomalies in the rotating blades and to wirelessly transmit vibration data to the data processor. The data processing unit synchronizes the wireless data transmitted from the tachometer sensor and the wireless accelerometer(s) and determines necessary adjustments to be made in order to reduce the vibration anomalies in the rotor blades.
    • 公开了一种用于旋翼航空器的转子轨道和平衡系统,其包括数据处理单元,转速计传感器和至少一个加速度计。 转速计传感器远离数据处理单元并且安装在旋翼机的旋转叶片附近。 转速计传感器适用于测量旋转叶片的速度和位置,并将数据无线传输到数据处理器。 所述至少一个加速度计也位于远离数据处理单元并且安装在旋翼飞机旋转叶片附近。 每个加速度计适于测量旋转叶片中的振动异常,并将振动数据无线传输到数据处理器。 数据处理单元使从转速计传感器和无线加速度计传送的无线数据同步,并确定为了减少转子叶片的振动异常而进行必要的调整。
    • 2. 发明授权
    • Wireless rotor track and balance system for rotorcraft
    • 用于旋翼航空器的无线转子轨道和平衡系统
    • US08812255B2
    • 2014-08-19
    • US12924466
    • 2010-09-28
    • Michael A. LynchMokhtar SadokRadoslaw R. Zakrzewski
    • Michael A. LynchMokhtar SadokRadoslaw R. Zakrzewski
    • G01R35/00
    • B64C27/008
    • Disclosed is a rotor track and balance system for rotorcraft that includes a data processing unit, a tachometer sensor and at least one accelerometer. The tachometer sensor is located remotely from the data processing unit and is mounted proximate to the rotating blades of the rotorcraft. The tachometer sensor is adapted to measure the speed and position of the rotating blades and to wirelessly transmit speed and position data to the data processor. The at least one accelerometer is also located remotely from the data processing unit and is mounted proximate the rotating blades of the rotorcraft. Each accelerometer is adapted to measure vibration anomalies in the rotating blades and to wirelessly transmit vibration data to the data processor. The data processing unit synchronizes the wireless data transmitted from the tachometer sensor and the wireless accelerometer(s) and determines necessary adjustments to be made in order to reduce the vibration anomalies in the rotor blades.
    • 公开了一种用于旋翼航空器的转子轨道和平衡系统,其包括数据处理单元,转速计传感器和至少一个加速度计。 转速计传感器远离数据处理单元并且安装在旋翼机的旋转叶片附近。 转速计传感器适用于测量旋转叶片的速度和位置,并将数据无线传输到数据处理器。 所述至少一个加速度计也位于远离数据处理单元并且安装在旋翼飞机旋转叶片附近。 每个加速度计适于测量旋转叶片中的振动异常,并将振动数据无线传输到数据处理器。 数据处理单元使从转速计传感器和无线加速度计传送的无线数据同步,并确定为了减少转子叶片的振动异常而进行必要的调整。
    • 5. 发明授权
    • Wire fault detection
    • 电线故障检测
    • US07512503B2
    • 2009-03-31
    • US10435926
    • 2003-05-12
    • Eric Robert BechhoeferMokhtar Sadok
    • Eric Robert BechhoeferMokhtar Sadok
    • G01R31/00
    • G01R31/11G01R31/008G01R31/088
    • Described are techniques used in a wire diagnostics system to detect events, such as defects, that may occur within a wire or cable under test. An incident voltage signal is sent out on the wire and a measured voltage signal is obtained which includes the incident voltage and the reflected voltage. Compensation processing is performed on the measured waveform to remove unwanted reflective components. Additionally, the waveform is then subject to attenuation processing and event detection processing. Detected events, such as defects, are classified and output as results. Events are classified by parametric classification using a library of known events or faults. The library of known events or faults is previously generated using empirical analysis and modeling techniques. Additionally, joint time-frequency domain reflectometry (TFDR) techniques are described for event identification and classification for a wire under test.
    • 描述的是用于线诊断系统中用于检测可能发生在被测试的电线或电缆内的诸如缺陷的事件的技术。 在线上发出入射电压信号,并且获得包括入射电压和反射电压的测量电压信号。 对测量波形执行补偿处理以去除不需要的反射部件。 此外,波形接受衰减处理和事件检测处理。 检测到的事件,如缺陷,被分类并作为结果输出。 事件通过使用已知事件或故障的库的参数分类进行分类。 先前使用经验分析和建模技术生成已知事件或故障的库。 另外,联合时频域反射(TFDR)技术被描述为用于被测电线的事件识别和分类。
    • 8. 发明授权
    • Detecting fire using cameras
    • 使用相机检测火灾
    • US07256818B2
    • 2007-08-14
    • US10152323
    • 2002-05-20
    • Mokhtar SadokRadoslaw Romuald Zakrzewski
    • Mokhtar SadokRadoslaw Romuald Zakrzewski
    • H04N7/18G08B17/12
    • G08B17/125
    • Detecting a fire, such as a fire in an aircraft cargo bay, includes receiving a plurality of frames of video information, determining an energy indicator for each of a subset of the plurality of frames, and detecting the presence of fire in response to the energy indicator for each of the subset of the plurality of frames corresponding to a predetermined pattern as a function of time. Detecting a fire may also include comparing energy indicators for each of the subset of the plurality of frames to a reference frame. The reference frame may correspond to a video frame taken when no fire is present or a video frame immediately preceding each of the subset of the plurality of frames. At least some of the subset of the plurality of frames may be provided by a camera having a sensitivity of between 400 nm and 1000 nm that may generates 640×480 pixels per frame. At least some of the subset of the plurality of frames may be provided by a CCD camera or a CMOS camera. At least some of the subset of the plurality of frames may be provided by a camera having a sensitivity of between 7 and 14 micrometers, which may be an IR camera.
    • 检测飞机货舱中的火灾,例如接收多个视频信息帧,确定多个帧的子集中的每一个的能量指示符,以及响应于能量来检测火灾的存在 指示符对应于作为时间的函数的预定模式的多个帧的每个子集。 检测火也可以包括将多个帧的子集中的每一个的能量指示符与参考帧进行比较。 参考帧可以对应于当不存在火焰时拍摄的视频帧或紧邻在多个帧的每个子集之前的视频帧。 多个帧的子集中的至少一些可以由具有在400nm和1000nm之间的灵敏度的相机提供,每帧可以产生640×480像素。 多个帧的子集中的至少一些可以由CCD照相机或CMOS照相机提供。 多个帧的子集中的至少一些可以由具有7至14微米的灵敏度的相机提供,其可以是IR相机。