並列タイトル等“A Study on Control System of High Efficiency Gas Turbine AGTJ100 (I) - Control System Development Facilities and its Characteristics”
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-895
一般注記A national R＆D program on “High Efficiency Gas Turbine” is under way. The target of the program is to develop an intercool-reheat type gas turbine engine for 100-MW-class power generation with very high thermal efficiency, resulting in energy conservation. The requirement for engine control is severe due to complexity of engine cycle and geometry. Therefore, development of an engine controller, inherently sophisticated multivariable controller, is considered to be one of the most important items for success of the program. This paper describes the basic plan, fabrication and characteristics of control system development facilities for the “High Efficiency Gas Turbine”, installed at NAL. The facilities consist of a high speed digital simulator (AD10) for real-time gas turbine simulation, a peripheral array processor (MAP300) for matrix operation and time series analysis, and a general purpose super mini-computer (VAX11/750). These can be utilized effectively in various stages of development of a control system, such as design, evaluation and hardware test.
資料番号: NALTR0895000
レポート番号: NAL TR-895
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