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    • 1. 发明申请
    • TEMPERATURE SENSOR WITH CONTROLLED THERMAL OFFSET FOR DETERMINING STATIC TEMPERATURE
    • 具有控制温度传感器的温度传感器用于确定静态温度
    • US20050232331A1
    • 2005-10-20
    • US10825447
    • 2004-04-15
    • John Severson
    • John Severson
    • G01K13/02G01J5/00
    • G01K13/02G01K13/028
    • The present invention relates to providing a temperature sensor that is mountable on an aircraft and includes a thermometer or temperature sensing element for sensing temperature of airflow. A heater is provided on the probe to bias the temperature sensed by the thermometer or temperature sensing element, in a manner such that the temperature measured is at a substantially known offset from the static temperature surrounding the temperature sensor. Control of the offset can be achieved by regulating airflow or heat provided. The heating effect is controlled to be a substantially equal and opposite match to the decreased total temperature resulting from lower airspeed or decreased airflow. In this manner, the thermometer or temperature sensing element will essentially operate at a fixed offset above static temperature, that is the temperature in undisturbed air in which the aircraft is operating, over a fairly wide range of flow rates.
    • 本发明涉及提供一种可安装在飞行器上的温度传感器,并且包括用于感测气流温度的温度计或温度感测元件。 在探针上设置加热器,以使得温度计或温度感测元件感测到的温度偏移,使得所测量的温度与温度传感器周围的静态温度基本上已知的偏差。 可以通过调节提供的气流或热量来实现偏移的控制。 加热效果被控制为与由较低空速或气流减小导致的降低的总温度基本上相等和相反。 以这种方式,温度计或温度感测元件将基本上在静态温度以上的固定偏移(即,在相当宽的流速范围内飞机在其中运行的不受干扰的空气中的温度)下操作。