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An electronic pressure profile display system for aeronautic test facilitiesThe NASA Lewis Research Center has installed an Electronic Pressure Profile Display system. This system provides for the real-time display of pressure readings on high resolution graphics monitors. The Electronic Pressure Profile Display system will replace manometer banks currently used in aeronautic test facilities. The Electronic Pressure Profile Display system consists of an industrial type Digital Pressure Transmitter (DPT) unit which interfaces with a host computer. The host computer collects the pressure data from the DPT unit, converts it into engineering units, and displays the readings on a high resolution graphics monitor in bar graph format. Software was developed to accomplish the above tasks and also draw facility diagrams as background information on the displays. Data transfer between host computer and DPT unit is done with serial communications. Up to 64 channels are displayed with one second update time. This paper describes the system configuration, its features, and its advantages over existing systems.
Document ID
19900006648
Document Type
Conference Paper
Authors
Woike, Mark R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-102478
NAS 1.15:102478
E-5265
Meeting Information
Meeting: International Instrumentation Symposium
Location: Denver, CO
Country: United States
Start Date: May 6, 1990
End Date: May 10, 1990
Sponsors: Instrument Society of America
Accession Number
90N15964
Funding Number(s)
PROJECT: RTOP 505-62-3B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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