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    • 1. 发明授权
    • Crash survivable memory unit
    • 崩溃生存记忆单元
    • US08121752B2
    • 2012-02-21
    • US12117473
    • 2008-05-08
    • Michael WinterhalterEndre Berecz
    • Michael WinterhalterEndre Berecz
    • G01M17/00
    • B64D45/00B64D2045/0065
    • A flight recorder includes an information input device, heat sensitive memory device electrically connected to the information input device, and housing enclosing the heat sensitive memory device. The housing is made with a first material and having a plurality of openings made through the housing. A sacrificial material is disposed between the housing and heat sensitive memory device. The sacrificial material having a lower melting temperature than the first material such that the sacrificial material changes state and egresses through the openings in the housing when exposed to heat to create an air gap between the housing and heat sensitive memory device. The first material includes nickel and the sacrificial material includes aluminum. A heat insulating layer is disposed between the sacrificial material and heat sensitive memory device. A second sacrificial material is disposed between the heat insulating layer and heat sensitive memory device.
    • 飞行记录器包括信息输入装置,电连接到信息输入装置的热敏记忆装置和封闭热敏记忆装置的外壳。 壳体由第一材料制成并且具有通过壳体制成的多个开口。 牺牲材料设置在壳体和热敏记忆装置之间。 牺牲材料具有比第一材料更低的熔化温度,使得当暴露于热量时,牺牲材料改变状态并通过壳体中的开口排出,以在壳体和热敏记忆装置之间产生气隙。 第一种材料包括镍,牺牲材料包括铝。 绝热层设置在牺牲材料和热敏记忆装置之间。 第二牺牲材料设置在绝热层和热敏记忆装置之间。
    • 2. 发明申请
    • LOCATOR BEACON WIRELESS HEALTH MONITOR
    • 定位器BEACON无线健康监护仪
    • US20120200460A1
    • 2012-08-09
    • US13021133
    • 2011-02-04
    • Michael E. WeedEndre Berecz
    • Michael E. WeedEndre Berecz
    • G01S1/00
    • B64D45/00B64D2045/0065B64D2045/0085G01S1/022G01S5/0226G01S5/0231G01S13/756Y02T50/53
    • Systems (224, 222, 700) and methods (800) for providing wireless health monitoring for a locator beacon (216). The methods involve: coupling a Transponder and Sensor Module (TSM) to the locator beacon such that at least one condition of the locator beacon or a battery (230) of the locator beacon can be remotely monitored; periodically detecting the condition by the TSM (224); and periodically and wirelessly transmitting, from the TSM to a wireless device (222, 700) located in proximity to the TSM, a signal including information describing the condition detected by the TSM. The TSM can include, but is not limited to a transponder (e.g., an RFID tag) and sensor. The wireless device, can include, but is not limited to a transponder interrogator.
    • 用于为定位器信标(216)提供无线健康监测的系统(224,222,700)和方法(800)。 所述方法包括:将应答器和传感器模块(TSM)耦合到定位器信标,使得定位器信标的至少一个条件或定位器信标的电池(230)可以被远程监控; 通过TSM定期检测条件(224); 并且从TSM定期地和无线地发送位于TSM附近的无线设备(222,700),包括描述由TSM检测到的状况的信息的信号。 TSM可以包括但不限于应答器(例如,RFID标签)和传感器。 无线设备可以包括但不限于应答器询问器。
    • 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。
    • 4. 发明申请
    • SYSTEMS AND METHODS FOR SYNCHRONIZING VARIOUS TYPES OF DATA ON A SINGLE PACKET
    • 在单个数据包上同步数据类型的系统和方法
    • US20130010812A1
    • 2013-01-10
    • US13177136
    • 2011-07-06
    • Eduardo M. CarroEndre Berecz
    • Eduardo M. CarroEndre Berecz
    • H04J3/06
    • G07C5/085B64D2045/0065
    • Data recording systems (100) and methods (400) for synchronizing data of a plurality of different data types on a single packet (300). The methods involve: receiving the data and an audio frame containing voice data and timing data communicated over a plurality of channels; generating, in response to the reception of the audio frame, a combined packet on which the audio frame and at least a portion of the data are time synchronized to each other; and substantially simultaneously storing the combined packet in a primary data store and a secondary data store of a data recorder for subsequent use in reconstructing events leading up to a crash of a land vehicle, aircraft or vessel. The portion of data may include data link data, flight data and/or image/video data. The channels may include a cockpit channel and a plurality of pilot channels.
    • 数据记录系统(100)和方法(400),用于在单个分组(300)上同步多个不同数据类型的数据。 所述方法包括:接收数据和包含通过多个信道传送的语音数据和定时数据的音频帧; 响应于所述音频帧的接收,生成其上所述音频帧和所述数据的至少一部分在其上彼此时间同步的组合分组; 并且基本上同时将组合的分组存储在数据记录器的主数据存储器和辅助数据存储器中,用于随后用于重建导致陆地车辆,飞行器或船只的碰撞的事件。 数据部分可以包括数据链接数据,飞行数据和/或图像/视频数据。 信道可以包括驾驶舱信道和多个导频信道。
    • 6. 发明授权
    • Systems and methods for synchronizing various types of data on a single packet
    • 用于在单个数据包上同步各种类型的数据的系统和方法
    • US08467420B2
    • 2013-06-18
    • US13177136
    • 2011-07-06
    • Eduardo M. CarroEndre Berecz
    • Eduardo M. CarroEndre Berecz
    • H04J3/06
    • G07C5/085B64D2045/0065
    • Data recording systems and methods for synchronizing data of a plurality of different data types on a single packet. The methods involve: receiving the data and an audio frame containing voice data and timing data communicated over a plurality of channels; generating, in response to the reception of the audio frame, a combined packet on which the audio frame and at least a portion of the data are time synchronized to each other; and substantially simultaneously storing the combined packet in a primary data store and a secondary data store of a data recorder for subsequent use in reconstructing events leading up to a crash of a land vehicle, aircraft or vessel. The portion of data may include data link data, flight data and/or image/video data. The channels may include a cockpit channel and a plurality of pilot channels.
    • 用于在单个分组上同步多种不同数据类型的数据的数据记录系统和方法。 所述方法包括:接收数据和包含通过多个信道传送的语音数据和定时数据的音频帧; 响应于所述音频帧的接收,生成其上所述音频帧和所述数据的至少一部分在其上彼此时间同步的组合分组; 并且基本上同时将组合的分组存储在数据记录器的主数据存储器和辅助数据存储器中,用于随后用于重建导致陆地车辆,飞行器或船只的碰撞的事件。 数据部分可以包括数据链接数据,飞行数据和/或图像/视频数据。 信道可以包括驾驶舱信道和多个导频信道。
    • 7. 发明申请
    • Crash Survivable Memory Unit
    • 碰撞存储单元
    • US20090277683A1
    • 2009-11-12
    • US12117473
    • 2008-05-08
    • Michael WinterhalterEndre Berecz
    • Michael WinterhalterEndre Berecz
    • H05K5/02
    • B64D45/00B64D2045/0065
    • A flight recorder includes an information input device, heat sensitive memory device electrically connected to the information input device, and housing enclosing the heat sensitive memory device. The housing is made with a first material and having a plurality of openings made through the housing. A sacrificial material is disposed between the housing and heat sensitive memory device. The sacrificial material having a lower melting temperature than the first material such that the sacrificial material changes state and egresses through the openings in the housing when exposed to heat to create an air gap between the housing and heat sensitive memory device. The first material includes nickel and the sacrificial material includes aluminum. A heat insulating layer is disposed between the sacrificial material and heat sensitive memory device. A second sacrificial material is disposed between the heat insulating layer and heat sensitive memory device.
    • 飞行记录器包括信息输入装置,电连接到信息输入装置的热敏记忆装置和封闭热敏记忆装置的外壳。 壳体由第一材料制成并且具有通过壳体制成的多个开口。 牺牲材料设置在壳体和热敏记忆装置之间。 牺牲材料具有比第一材料更低的熔化温度,使得当暴露于热量时,牺牲材料改变状态并通过壳体中的开口排出,以在壳体和热敏记忆装置之间产生气隙。 第一种材料包括镍,牺牲材料包括铝。 绝热层设置在牺牲材料和热敏记忆装置之间。 第二牺牲材料设置在绝热层和热敏记忆装置之间。