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NASA NTRS ยท 19980203171

Accelerometer Method and Apparatus for Integral Display and Control Functions

Abstract

Method and apparatus for detecting mechanical vibrations and outputting a signal in response thereto is discussed. An accelerometer package having integral display and control functions is suitable for mounting upon the machinery to be monitored. Display circuitry provides signals to a bar graph display which may be used to monitor machine conditions over a period of time. Control switches may be set which correspond to elements in the bar graph to provide an alert if vibration signals increase in amplitude over a selected trip point. The circuitry is shock mounted within the accelerometer housing. The method provides for outputting a broadband analog accelerometer signal, integrating this signal to produce a velocity signal, integrating and calibrating the velocity signal before application to a display driver, and selecting a trip point at which a digitally compatible output signal is generated.

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BibTeXRIS

Bozeman, Richard J., Jr.. 1998-04-07. Accelerometer Method and Apparatus for Integral Display and Control Functions. https://ntrs.nasa.gov/citations/19980203171

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