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1. 发明申请

WO2007034240A3 SENSOR DEVICE WITH BACKSIDE CONTACTS 审中-公开
标题翻译：带背面接触的传感器装置
公开(公告)号：WO2007034240A3
公开(公告)日：2007-11-29
申请号：PCT/GB2006050295
申请日：2006-09-19
申请人： BAE SYSTEMS PLC , WARSOP CLYDE , PRESS ANDREW JULIAN , HUCKER MARTYN JOHN
发明人： WARSOP CLYDE , PRESS ANDREW JULIAN , HUCKER MARTYN JOHN
IPC分类号： G01P5/12 , G01F1/684
CPC分类号： G01F1/6845 , G01P5/12 , G01P13/025
摘要： A sensor device for sensing air flow speed at the exterior of an aircraft, comprising a substrate having an upper side on which is mounted a diaphragm over an aperture or recess in the substrate, the diaphragm being thermally and electrically insulative, and mounting on its upper surface a heating element comprising a layer of resistive material, and wherein electrical connections to the heating element are buried in the diaphragm and/or the substrate, and provide electrical terminals at the lower side of the substrate. The heating element is exposed to the environment, but the remaining electrical parts of the device are not exposed. Portions of a conductive substrate may be cut or etched away to define a conductive pillar. Signals may be transmitted through the conductive pillar from one surface carrying the sensor element to the other surface carrying contact pads.
摘要翻译：一种用于感测飞行器外部的空气流速的传感器装置，包括：具有上侧的基板，在基板上的孔或凹部上方安装有隔膜，所述隔膜具有热和电绝缘性，并且安装在其上部表面包括电阻材料层的加热元件，并且其中与所述加热元件的电连接被掩埋在所述隔膜和/或所述基板中，并在所述基板的下侧提供电端子。加热元件暴露在环境中，但是该设备的其余电气部件不暴露。可以切割或蚀刻导电基底的一部分以限定导电柱。信号可以通过导电柱从承载传感器元件的一个表面传输到另一个承载接触垫的表面。

2. 发明申请

WO2009068918A1 IMPROVEMENTS RELATING TO TEMPERATURE MONITORING 审中-公开
标题翻译：关于温度监测的改进
公开(公告)号：WO2009068918A1
公开(公告)日：2009-06-04
申请号：PCT/GB2008/051133
申请日：2008-11-28
申请人： BAE SYSTEMS PLC , PRESS, Andrew, Julian
发明人： PRESS, Andrew, Julian
IPC分类号： B64D15/00 , B64D15/12 , B64D15/20
CPC分类号： B64D15/12 , B64D15/20
摘要： A temperature monitoring arrangement for an electro-thermal ice protection system is provided for a slat (2) of an aircraft wing, incorporating heater mats 12 1 , 12 2 , 12 3 , 12 4 of composite material, wherein, in order to avoid or at least substantially reduce some of the problems associated with use of discrete temperature sensing elements, one or more optical fibre temperature sensors are embedded within the heater mats for sensing an overheating condition of each mat. Advantageously, a control system is used to monitor the temperature of the mats, and adjusts power supplied, or switches off power, in response to detection of an overheating condition.
摘要翻译：为飞机机翼的板条（2）提供电热保冰系统的温度监控装置，其中包括复合材料的加热垫121,122,123,124，其中为了避免或至少大大减少与使用离散的温度感测元件相关联的一些问题，一个或多个光纤温度传感器嵌入在加热器垫内，用于感测每个垫的过热状况。有利地，控制系统用于响应于过热条件的检测来监测垫的温度，并且调节供应的功率或关闭电力。

3. 发明申请

WO2007034240A2 SENSOR DEVICE 审中-公开
标题翻译：传感器设备
公开(公告)号：WO2007034240A2
公开(公告)日：2007-03-29
申请号：PCT/GB2006/050295
申请日：2006-09-19
申请人： BAE SYSTEMS PLC , WARSOP, Clyde , PRESS, Andrew, Julian , HUCKER, Martyn, John
发明人： WARSOP, Clyde , PRESS, Andrew, Julian , HUCKER, Martyn, John
IPC分类号： G01P5/12 , G01F1/684
CPC分类号： G01F1/6845 , G01P5/12 , G01P13/025
摘要： A sensor device for sensing air flow speed at the exterior of an aircraft, comprising a substrate having an upper side on which is mounted a diaphragm over an aperture or recess in the substrate, the diaphragm being thermally and electrically insulative, and mounting on its upper surface a heating element comprising a layer of resistive material, and wherein electrical connections to the heating element are buried in the diaphragm and/or the substrate, and provide electrical terminals at the lower side of the substrate. The heating element is exposed to the environment, but the remaining electrical parts of the device are not exposed.
摘要翻译：一种用于感测飞行器外部的空气流速的传感器装置，包括具有上侧的基板，在基板上的孔或凹部上安装有隔膜，所述隔膜具有热和电绝缘性，并且安装在其上部表面包括电阻材料层的加热元件，并且其中与所述加热元件的电连接被掩埋在所述隔膜和/或所述基板中，并且在所述基板的下侧提供电端子。加热元件暴露于环境中，但是该设备的其余电气部分不暴露。

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