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Integrated exhaust gas analysis system for aircraft turbine engine component testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Summers, R. L. Anderson, R. C. |
| Copyright Year | 1985 |
| Description | An 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. |
| File Size | 7778731 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850007791 |
| Archival Resource Key | ark:/13960/t0005146s |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Microprocessors Exhaust Gases Gas Turbine Engines Flow Distribution Numerical Control Engine Tests Gas Analysis Sampling Systems Integration Pneumatic Equipment Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
