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Accelerometer Method and Apparatus for Integral Display and Control FunctionsMethod and apparatus for detecting mechanical vibrations and outputting a signal in response thereto. Art 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.
Document ID
19970017013
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
Authors
Bozeman, Richard J., Jr.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 17, 2013
Publication Date
May 14, 1996
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: NASA-Case-MSC-21961-1
Patent Application Number: US-Patent-Appl-SN-901626
Patent Number: US-Patent-5,517,183
Accession Number
97N19380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-MSC-21961-1|US-Patent-5,517,183
Patent Application
US-Patent-Appl-SN-901626
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