Engineering PapersSearch

NASA NTRS · 20040013345

Silicon Carbide High Temperature Anemometer and Method for Assembling the Same

Abstract

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.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Okojie, Robert S., Fralick, Gustave C., Saad, George J.. 2003-11-18. Silicon Carbide High Temperature Anemometer and Method for Assembling the Same. https://ntrs.nasa.gov/citations/20040013345

Cite the original work for its findings. Save a collection to share your selection of sources.