Measurement Specialties, Incorporated

The United States of America As Represented by the Administrator of the

Chris Gross

Damon Germanton

A method for making a pressure transducer comprising: forming a recess in a diaphragm, the diaphragm having a thinned region that deflects responsively to pressure being applied thereto; depositing a glass frit in the recess; embedding a plurality of strain gages in the glass frit; and, wire bonding the strain gages into a Wheatstone bridge configuration.

Method of making pressure transducer and apparatus

A semiconductor strain gage having an electrically resistive substrate layer and a layer of electrically conductive silicon supported by the substrate layer. The silicon layer can be an epitaxial silicon layer grown on a surface of the substrate layer or a diffused or ion-implanted layer formed in the surface of the substrate layer. Also, a force measuring and detecting device including a force responsive member and the above-described semiconductor strain gage attached to the force responsive member, the strain gage measuring forces applied to the force responsive member.

Silicon strain gage having a thin layer of highly conductive silicon

A sensor plate for use in a load cell for use in an electronic scale comprising a planar first surface; a planar second surface opposite the first surface having a depression formed therein defining a flexure area; a load cavity formed in the second surface having a conical receptacle end for receiving a strut; and sensors disposed over the flexure area for generating a signal in response to a load applied to the loading cavity wherein the strut has a first conical projection end coupled to the conical receptacle end of the loading cavity and a second end coupled to a footer member such that the strut mechanically floats therebetween for providing the applied load at a substantially central position at the load cavity.

Load cell with bossed sensor plate for an electrical weighing scale

This invention is a multiple channel high data rate pressure sensing device for use in wind tunnels, spacecraft, airborne, process control, automotive, etc., pressure measurements. This device offers data rates in excess of 100,000 measurements per second with inaccuracies from temperature shifts less than 0.25% (nominal) of full scale over a temperature span of 55.degree. C. This device consists of thirty-two solid state sensors 11, signal multiplexing electronics to electronically address each sensor, and ditital electronic circuitry to automatically correct the inherent thermal shift errors of the pressure sensors and their associated electronics.

Self-correcting electronically scanned pressure sensor

This invention is a high data rate pressure sensor module with an in situ calibration capability to help reduce energy consumption in wind tunnel facilities without loss of measurement accuracy. The sensor module allows for nearly a two order of magnitude increase in data rates over conventional electromechanically scanned pressure sampling techniques. The module consists of 16 solid state pressure sensor chips and signal multiplexing electronics integrally mounted to a four position pressure selector switch. One of the four positions of the pressure selector switch allows the in situ calibration of the 16 pressure sensors; the three other positions allow 48 channels (three sets of 16) pressure inputs to be measured by the sensors. The small size of the sensor module will allow mounting within many wind tunnel models, thus eliminating long tube lengths and their corresponding slow pressure response.

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Yorktown, VA, United States of America

Chris Gross