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題 名 | 1500°C級氣渦輪機之開發=Development of 1500°C Class Gas Turbine |
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作 者 | 劉陽秋; | 書刊名 | 台電工程月刊 |
卷 期 | 606 1999.02[民88.02] |
頁 次 | 頁1-9 |
分類號 | 448.2 |
關鍵詞 | 重型; 阻熱劑被覆; 內部的; 潛變破壞; 接口; 獨立式動葉片; 彎曲接頭; 馬赫值; 葉柵試驗; 超級耐熱合金; 斜向擾流發生; 閘流晶體管; Heavy duty; Thermal barrier coating; In house; Creep rupture; Spigot; Free sanding blades; Curvic coupling; Mach number; Cascade test; Super alloy; Angled turbulator; Thyristor; |
語 文 | 中文(Chinese) |
中文摘要 | 進氣溫度為1500℃級之下一代,大容量、重型、單軸之氣渦輪機,業於日本開發 完成,許多改良的組件技術,諸如:高效率的壓縮機、蒸汽冷卻之燃燒器、高溫之渦輪機等 ,均應用於這種氣渦輪機而達成最優越之複循環性能。所有重要要之特性,包括冷卻特性和 組件可靠性,均經試運轉後証實為真。 |
英文摘要 | The next generation of large, heavy-duty, single-shaft gas turbine, with a turbine inlet temperature in the 1500 ℃ range has been developed in Japan. Many advanced component technologies, such as:high efficiency compressor, steam cooled combustor, high temperature turbine, etc, are all employed in this turbine and achieve an excellent combined cycle performance. All important characteristics, including the cooling characteristics, and components reliability were verified during the trial operation. |
本系統中英文摘要資訊取自各篇刊載內容。