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A graphics subsystem retrofit design for the bladed-disk data acquisition systemA graphics subsystem retrofit design for the turbojet blade vibration data acquisition system is presented. The graphics subsystem will operate in two modes permitting the system operator to view blade vibrations on an oscilloscope type of display. The first mode is a real-time mode that displays only gross blade characteristics, such as maximum deflections and standing waves. This mode is used to aid the operator in determining when to collect detailed blade vibration data. The second mode of operation is a post-processing mode that will animate the actual blade vibrations using the detailed data collected on an earlier data collection run. The operator can vary the rate of payback to view differring characteristics of blade vibrations. The heart of the graphics subsystem is a modified version of AMD's ""super sixteen'' computer, called the graphics preprocessor computer (GPC). This computer is based on AMD's 2900 series of bit-slice components.
Document ID
19840004662
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Carney, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Computer Operations And Hardware
Report/Patent Number
NASA-TM-83510
E-1760
NAS 1.15:83510
Report Number: NASA-TM-83510
Report Number: E-1760
Report Number: NAS 1.15:83510
Accession Number
84N12730
Funding Number(s)
PROJECT: RTOP 505-33-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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