SENSOR SYSTEM AND METHOD FOR SENSING IN AN ELEVATED-TEMPERATURE ENVIRONMENT, WITH PROTECTION AGAINST EXTERNAL HEATING
    1.
    发明申请
    SENSOR SYSTEM AND METHOD FOR SENSING IN AN ELEVATED-TEMPERATURE ENVIRONMENT, WITH PROTECTION AGAINST EXTERNAL HEATING 审中-公开
    传感器系统和方法在高温环境中进行感应,防止外部加热

    公开(公告)号:WO2004099743A1

    公开(公告)日:2004-11-18

    申请号:PCT/US2004/013403

    申请日:2004-04-30

    Abstract: Sensing in an elevated-temperature environment is provided using a sensor system having a sensor housing with an exterior wall with a window-support region having an outwardly facing external face, and a window through the window-support region of the exterior wall and affixed to the exterior wall. A sensor unit contained within the sensor housing receives an input signal through the window. A thermal-insulation layer is on the external face of the window-support region of the exterior wall at a location immediately adjacent to the window. The sensor system is operated in an environment wherein the window-support region of the exterior wall is heated to a temperature of greater than about 100 °C in the event that no thermal-insulation layer is present. In a typical application, the sensor system is attached to an aircraft such that the external face is in a forward-facing orientation, and the aircraft is operated such that the external face is heated by aerodynamic heating.

    Abstract translation: 使用具有传感器壳体的传感器系统提供感测,所述传感器系统具有外壁,窗外支撑区域具有向外的外表面,以及通过外壁的窗口支撑区域的窗口,并被固定到 外墙。 包含在传感器壳体内的传感器单元通过窗口接收输入信号。 隔热层位于紧邻窗户的位置的外壁的窗口支撑区域的外表面上。 传感器系统在其中不存在绝热层的情况下将外壁的窗口支撑区域加热到大于约100℃的温度的环境中操作。 在典型的应用中,传感器系统附接到飞行器,使得外表面处于朝前的方向,并且飞行器被操作以使得外表面被空气动力加热加热。

    SENSOR SYSTEM AND METHOD FOR SENSING IN AN ELEVATED-TEMPERATURE ENVIRONMENT, WITH PROTECTION AGAINST EXTERNAL HEATING
    2.
    发明公开
    SENSOR SYSTEM AND METHOD FOR SENSING IN AN ELEVATED-TEMPERATURE ENVIRONMENT, WITH PROTECTION AGAINST EXTERNAL HEATING 有权
    传感器系统和方法用于测量用高温的环境中进行防护外部加热

    公开(公告)号:EP1618357A1

    公开(公告)日:2006-01-25

    申请号:EP04760648.8

    申请日:2004-04-30

    Abstract: Sensing in an elevated-temperature environment is provided using a sensor system having a sensor housing with an exterior wall with a window-support region having an outwardly facing external face, and a window through the window-support region of the exterior wall and affixed to the exterior wall. A sensor unit contained within the sensor housing receives an input signal through the window. A thermal-insulation layer is on the external face of the window-support region of the exterior wall at a location immediately adjacent to the window. The sensor system is operated in an environment wherein the window-support region of the exterior wall is heated to a temperature of greater than about 100 °C in the event that no thermal-insulation layer is present. In a typical application, the sensor system is attached to an aircraft such that the external face is in a forward-facing orientation, and the aircraft is operated such that the external face is heated by aerodynamic heating.

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