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    • 2. 发明申请
    • ELECTRONIC VIBRATION SENSOR
    • 电子振动传感器
    • US20070272023A1
    • 2007-11-29
    • US11419938
    • 2006-05-23
    • Michael D. DwyerDean R. Hellickson
    • Michael D. DwyerDean R. Hellickson
    • G01H11/00
    • G01H1/003
    • An electronic sensor is disclosed. The electronic sensor includes a processor, a processor memory coupled to the processor, and at least one input/output block in communication with the processor and with at least one external component monitor. The sensor further includes one or more accelerometers in communication with the processor and coupled directly to at least one component, the one or more accelerometers sensing one or more mechanical vibrations from the at least one component, and the one or more mechanical vibrations oscillating below 1 MHz. The processor compares the one or more mechanical vibrations with a plurality of vibration samples programmed into the processor memory, each vibration sample specific to at least one sensor application.
    • 公开了一种电子传感器。 电子传感器包括处理器,耦合到处理器的处理器存储器以及与处理器和至少一个外部元件监视器通信的至少一个输入/输出块。 传感器还包括与处理器通信并直接耦合到至少一个部件的一个或多个加速度计,所述一个或多个加速度计感测来自至少一个部件的一个或多个机械振动,以及一个或多个振动在1以下的机械振动 MHz。 处理器将一个或多个机械振动与编程到处理器存储器中的多个振动样本进行比较,每个振动样本特定于至少一个传感器应用。
    • 6. 发明申请
    • AUTOMATED HEATING SYSTEM FOR PORTS SUSCEPTIBLE TO ICING
    • 自动加热系统,适用于不可靠的加热
    • US20100116806A1
    • 2010-05-13
    • US11745660
    • 2007-05-08
    • David R. HollingsworthMichael D. DwyerDean G. Psiropoulos
    • David R. HollingsworthMichael D. DwyerDean G. Psiropoulos
    • B60L1/02
    • B64D15/12G01P5/165
    • An improved heating system air pressure sensing port. An example aircraft pitot tube heater uses Positive Temperature Coefficient (PTC) switching thermistors arranged to automatically sense the outside air temperature and heat to a design set point temperature. When a high outside air temperature is experienced, the pitot tube will not turn on. The pitot tube heater only turns on below the design set point and will consumes less current than the standard aircraft pitot tube heaters when operating at very cold temperatures. Virtually no current is drawn when the pitot tube increases past the set point, thus reducing the power drain on the aircraft system. The use of multiple thermistors gives the example pitot tube a level of failure redundancy that is not available in current pitot tube heaters.
    • 改进的加热系统气压检测口。 一个示例飞机皮托管加热器使用正温度系数(PTC)切换热敏电阻,其被布置成自动感测外部空气温度和热量达到设计设定点温度。 当外部空气温度过高时,皮托管不能打开。 皮托管加热器仅在设计设定点以下开启,在非常冷的温度下运行时,比标准飞机皮托管加热器消耗的电流要少。 当皮托管增加超过设定点时,几乎没有电流被拉出,从而减少飞机系统的功率消耗。 使用多个热敏电阻为皮托管示例提供了当前皮托管加热器不可用的故障冗余度。
    • 9. 发明申请
    • DATA RECORDER
    • 数据记录器
    • US20080249680A1
    • 2008-10-09
    • US11696453
    • 2007-04-04
    • Michael D. DwyerCarlos A. IbarraJohn W. Thornberry
    • Michael D. DwyerCarlos A. IbarraJohn W. Thornberry
    • G07C5/08
    • G07C5/085G07C5/008
    • Systems and methods for recording information in a vehicle data recorder device. The vehicle data recorder device includes an inertial measurement unit (IMU), a crash survivable unit having memory, and a microcontroller in data communication with the IMU and the memory. The microcontroller receives angular rate information and acceleration information from the IMU and stores the received angular rate information and acceleration information in the memory. The IMU includes two or more MEMS gyroscopes or ring laser gyroscopes. In one example, the microcontroller stores angular rate information and acceleration information in the memory until a threshold event has occurred. The threshold event includes at least one of the angular rate information or acceleration information indicating zero with respect to a rotating earth coordinate frame for a predetermined period of time.
    • 用于在车辆数据记录装置中记录信息的系统和方法。 车辆数据记录装置包括惯性测量单元(IMU),具有存储器的碰撞存活单元和与IMU和存储器进行数据通信的微控制器。 微控制器从IMU接收角速率信息和加速度信息,并将接收到的角速率信息和加速度信息存储在存储器中。 IMU包括两个或更多个MEMS陀螺仪或环形激光陀螺仪。 在一个示例中,微控制器将角速度信息和加速度信息存储在存储器中直到出现阈值事件。 阈值事件包括角速率信息或加速度信息中的至少一个,其指示相对于旋转的地球坐标系为零的预定时间段。