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    • 1. 发明申请
    • Flight Recorder Having Integral Reserve Power Supply Within Form Factor of Enclosure and Method Therefor
    • 具有整体储备电力的飞行记录仪的外壳尺寸及其方法
    • US20090319102A1
    • 2009-12-24
    • US12142129
    • 2008-06-19
    • Michael C. WinterhalterGlenn C. Wilson
    • Michael C. WinterhalterGlenn C. Wilson
    • G06F19/00
    • G07C5/085
    • A flight recorder includes an enclosure having a notch formed on one side or corner of the enclosure. An electronic interface is disposed within the enclosure. The electronic interface is coupled for receiving flight data, video data, and audio data. A memory unit is disposed within the enclosure and electrically connected to the electronic interface for storing the data. The memory unit contains a non-volatile memory device. A reserve power supply is physically disposed within the notch of the enclosure. The reserve power supply contains a rechargeable battery. A clamp secures the reserve power supply to the enclosure to make the reserve power supply removable from the enclosure. The reserve power supply has an electrical connector coupled to the enclosure for providing an operating voltage to the electronic interface and memory unit. The reserve power supply and electrical connector physically reside within a form factor of the enclosure.
    • 飞行记录器包括具有形成在外壳的一侧或角上的凹口的外壳。 电子接口设置在外壳内。 电子接口被耦合用于接收飞行数据,视频数据和音频数据。 存储器单元设置在外壳内并电连接到电子接口以存储数据。 存储器单元包含非易失性存储器件。 备用电源物理地设置在外壳的凹口内。 备用电源包含可充电电池。 夹具将备用电源固定到外壳,以使备用电源从外壳中移除。 备用电源具有耦合到外壳的电连接器,用于向电子接口和存储器单元提供工作电压。 备用电源和电气连接器物理上位于外壳的外形。
    • 2. 发明授权
    • Flight recorder having integral reserve power supply within form factor of enclosure and method therefor
    • 飞行记录仪具有外壳尺寸内的整体式备用电源及其方法
    • US08165730B2
    • 2012-04-24
    • US12142129
    • 2008-06-19
    • Michael C. WinterhalterGlenn C. Wilson
    • Michael C. WinterhalterGlenn C. Wilson
    • B64D47/00
    • G07C5/085
    • A flight recorder includes an enclosure having a notch formed on one side or corner of the enclosure. An electronic interface is disposed within the enclosure. The electronic interface is coupled for receiving flight data, video data, and audio data. A memory unit is disposed within the enclosure and electrically connected to the electronic interface for storing the data. The memory unit contains a non-volatile memory device. A reserve power supply is physically disposed within the notch of the enclosure. The reserve power supply contains a rechargeable battery. A clamp secures the reserve power supply to the enclosure to make the reserve power supply removable from the enclosure. The reserve power supply has an electrical connector coupled to the enclosure for providing an operating voltage to the electronic interface and memory unit. The reserve power supply and electrical connector physically reside within a form factor of the enclosure.
    • 飞行记录器包括具有形成在外壳的一侧或角上的凹口的外壳。 电子接口设置在外壳内。 电子接口被耦合用于接收飞行数据,视频数据和音频数据。 存储器单元设置在外壳内并电连接到电子接口以存储数据。 存储器单元包含非易失性存储器件。 备用电源物理地设置在外壳的凹口内。 备用电源包含可充电电池。 夹具将备用电源固定到外壳,以使备用电源从外壳中移除。 备用电源具有耦合到外壳的电连接器,用于向电子接口和存储器单元提供工作电压。 备用电源和电气连接器物理上位于外壳的外形。
    • 3. 发明申请
    • Locator Beacon Disposed Internal to an Enclosure of a Flight Data Recorder and Method Therefor
    • 飞行数据记录仪及其方法的内部放置定位灯
    • US20100063654A1
    • 2010-03-11
    • US12206585
    • 2008-09-08
    • Michael C. WinterhalterEndre Berecz
    • Michael C. WinterhalterEndre Berecz
    • G06F19/00B64D45/00
    • B64D45/00G01S5/18G01S5/183Y10T29/49002Y10T29/49005
    • A flight data recorder includes an enclosure and electronic interface within the enclosure. The electronic interface is coupled for receiving data. A crash survivable memory unit is disposed within the enclosure. The crash survivable memory unit includes a memory module electrically coupled to the electronic interface for storing the data. A locator beacon is disposed within the enclosure or within the crash survivable memory unit. The locator beacon is an acoustic resonator which emits ultrasonic pulses. A battery is disposed within the enclosure or within the crash survivable memory unit for providing operating power to the locator beacon. The battery is rechargeable. The battery status is stored in the memory module. A beacon control circuit is disposed within the enclosure or within the crash survivable memory unit for monitoring the battery. A beacon activation device detects a crash event and notifies the beacon control circuit to activate the locator beacon.
    • 飞行数据记录仪包括外壳内的外壳和电子接口。 电子接口被耦合用于接收数据。 崩溃可存储存储器单元设置在外壳内。 崩溃可存储存储器单元包括电耦合到电子接口用于存储数据的存储器模块。 定位器信标设置在机壳内或碰撞可存储存储器单元内。 定位信标是发射超声脉冲的声共振器。 电池设置在外壳内或在碰撞存活的存储器单元内,用于向定位器信标提供操作电力。 电池是可充电的。 电池状态存储在内存模块中。 信标控制电路设置在机壳内或在碰撞可存储的存储器单元内,用于监测电池。 信标激活装置检测碰撞事件并通知信标控制电路以激活定位信标。