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Modularized instrument system for turbojet engine test facilitiesA new modular instrument system is being developed to handle the many channels of data commonly 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. Each module provides a controlled environment for its contents. A minicomputer in the control room gathers the data, performs some 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 through minimization of manual adjustments; and (4) reduced cost through minimization of wiring and simplification of control room display.
Document ID
19740045546
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Nieberding, W. C.
Englund, D. R., Jr.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: Symposium on Instrumentation for airbreathing propulsion
Location: Monterey, CA
Start Date: September 19, 1972
End Date: September 21, 1972
Accession Number
74A28296
Distribution Limits
Public
Copyright
Other

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