タイトル | Integrated exhaust gas analysis system for aircraft turbine engine component testing |
本文(外部サイト) | http://hdl.handle.net/2060/19850007791 |
著者(英) | Anderson, R. C.; Summers, R. L. |
著者所属(英) | NASA Lewis Research Center |
発行日 | 1985-01-01 |
言語 | eng |
内容記述 | 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. |
NASA分類 | INSTRUMENTATION AND PHOTOGRAPHY |
レポートNO | 85N16100 NASA-TP-2424 NAS 1.60:2424 E-2302 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/157484 |