並列タイトル等High Pressure Combustion Test Facility for Gas Turbine Research
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-801
一般注記A new high pressure combustion test facility was constructed in the National Aerospace Laboratory, Tokyo, to assist the national project for developing a high efficiency combined cycle gas turbine. It enables continuous combustion tests by an air mass flow of 4 kg/s at a pressure of 5.53 MPa and a temperature of 736 K in the design condition. Two kinds of fuel, i.e., natural gas and kerosene, are available for tests at a maximum supply pressure of 10 MPa. In this paper, datails of the planning of the facility and the structure are described. In designing the building, special care was taken to prevent anticipated noise pollution of the surrounding area. Test runs, made early in the spring of 1983, proved successful.
資料番号: NALTR0801000
レポート番号: NAL TR-801
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45059&item_no=1&attribute_id=31&file_no=1
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