並列タイトル等On the Test Installation of the High Pressure Ratio Compressor
タイトル（掲載誌）航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-536
一般注記The fan engine for aircraft has been used widely in recent years because of its low fuel consumption and low levels of noise and emission. The high pressure ratio compressor(HPC) is one of the important components of the fan engine. Therefore, the improvement of HPC performance is essential to the improvement of fan engine performance, and more experiments are required for the research and development of HPC. For aerodynamic performance tests on HPC, test apparatuses were installed in the established compressor test facilities of the Aeroengine Division, National Aerospace Laboratory, in 1972. Test apparatuses for HPC such as the variable stator vane control system, the air bleeding apparatus, the measurement and monitoring system, etc. were set in the test cell and the control room of the compressor test facility, and were connected to the compressor drive system and the data processing system. This report presents the details of planning, mechanism, function and arrangement of the test apparatuses.
資料番号: NALTR0536000
レポート番号: NAL TR-536
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ