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Modularized instrument system for turbojet engine test facilitiesA modular instrument system is being developed to handle the many data channels encountered in turbojet engine testing. Each module contains a group of transducers and all the signal conditioning multiplexing, and digitizing electronics necessary for direct interface with a digital computer. The digital interface within each module is the same for all modules; in addition, each module provides a controlled environment for its contents. A minicomputer in the control room gathers the data, performs on-line calculation and display, and interfaces with a shared recording and computing system. The advantages of this system are: (1) reduced manpower for system installation, setup, and checkout; (2) standardized equipment interfaces; (3) increased reliability through automatic system testing and minimization of manual adjustments; and (4) reduced cost through minimization of wiring and simplification of control room display.
Document ID
19720024808
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nieberding, W. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Englund, D. R., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Instrumentation And Photography
Report/Patent Number
E-7089
NASA-TM-X-68123
Report Number: E-7089
Report Number: NASA-TM-X-68123
Meeting Information
Meeting: Symp. on Instrumentation for Airbreathing Propulsion
Location: Monterey, CA
Country: United States
Start Date: September 19, 1972
End Date: September 21, 1972
Sponsors: Army Aviation R and D Labs., Naval Air Systems Command, AFOSR, AFAPL, ONR
Accession Number
72N32458
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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