NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Integrated exhaust gas analysis system for aircraft turbine engine component testingAn integrated exhaust gas analysis system was designed and installed in the hot-section facility at the Lewis Research Center. The system is designed to operate either manually or automatically and also to be operated from a remote station. The system measures oxygen, water vapor, total hydrocarbons, carbon monoxide, carbon dioxide, and oxides of nitrogen. Two microprocessors control the system and the analyzers, collect data and process them into engineering units, and present the data to the facility computers and the system operator. Within the design of this system there are innovative concepts and procedures that are of general interest and application to other gas analysis tasks.
Document ID
19850007791
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Summers, R. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Anderson, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TP-2424
E-2302
NAS 1.60:2424
Report Number: NASA-TP-2424
Report Number: E-2302
Report Number: NAS 1.60:2424
Accession Number
85N16100
Funding Number(s)
PROJECT: RTOP 505-40-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available