发明名称 SHROUD RING FOR GAS TURBINE
摘要 PURPOSE:To prevent a shroud ring from cracking due to the temperature difference between its inner and outer circumferential surfaces, by providing a cover plate along the inner circumferential surface of the shroud ring to form a cooling air layer. CONSTITUTION:A cover plate 6 is provided along the inner circumferential surface of a shroud ring 2. A cooling air hole 8 is opened in the shroud ring 2 so that cooling air 7 is caused to flow in between the shroud ring and the cover plate 6. This results in reducing the temperature difference between the inner and outer circumferential surfaces of the shroud ring 2.
申请公布号 JPS5910706(A) 申请公布日期 1984.01.20
申请号 JP19820119816 申请日期 1982.07.12
申请人 HITACHI SEISAKUSHO KK 发明人 GUNJI TSUTOMU
分类号 F01D11/10;F01D11/08;(IPC1-7):01D11/08 主分类号 F01D11/10
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