发明名称 Method of assembling a silicon carbide high temperature anemometer
摘要 A high temperature anemometer includes a pair of substrates. One of the substrates has a plurality of electrodes on a facing surface, while the other of the substrates has a sensor cavity on a facing surface. A sensor is received in the sensor cavity, wherein the sensor has a plurality of bondpads, and wherein the bond pads contact the plurality of electrodes when the facing surfaces are mated with one another. The anemometer further includes a plurality of plug-in pins, wherein the substrate with the cavity has a plurality of trenches with each one receiving a plurality of plug-in pins. The plurality of plug-in pins contact the plurality of electrodes when the substrates are mated with one another. The sensor cavity is at an end of one of the substrates such that the sensor partially extends from the substrate. The sensor and the substrates are preferably made of silicon carbide.
申请公布号 US6794213(B1) 申请公布日期 2004.09.21
申请号 US20030637083 申请日期 2003.08.05
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 OKOJIE ROBERT S.;FRALICK GUSTAVE C.;SAAD GEORGE J.
分类号 G01F1/28;G01P5/02;(IPC1-7):H01L21/00 主分类号 G01F1/28
代理机构 代理人
主权项
地址