发明名称 GAS TURBINE COMBUSTOR
摘要 PURPOSE:To prevent the generation of thermal stress and heighten cooling performance by fixing good heat conductive material particles on an inner cylinder air side surface to make it coarse. CONSTITUTION:Air compressed by a compressor is supplied to a combustor part through a compressor diffuser 6, air allowed to flow in the circumference of a tail cylinder 2 is allowed to flow between a guide cylinder 5 and an inner cylinder body 1 to flow into the inside of the inner cylinder body through an air hole. In the inside of the inner cylinder a fuel supplied from a combustion nozzle 3 is mixed with the air to burn so as to produce high temperature combustion gas. The combustion gas is introduced in a turbine through the inside of the tail cylinder 2 to be exhausted after expansion. The inner cylinder body 1, and the tail cylinder 2 are heated because high temperature combustion gas is allowed to flow in their insides, but cooled with the use of air flowing on their periphery, a condition to fix cooling promotion bodies on the inner cylindrical main body 1 is made for a coarse surface body 7, and a condition to fix them on the tail cylinder 2 is made for a coarse surface body 8. A cooling effect by the air allowed to flow between the guide cylinder 5 and the inner cylinder body 1 can be heightened by the improvement of heat transfer coefficient with the use of the coarse surface bodies 7, 8.
申请公布号 JPH02183721(A) 申请公布日期 1990.07.18
申请号 JP19890000346 申请日期 1989.01.06
申请人 HITACHI LTD 发明人 TSUKAHARA SATOSHI;HAYASHI NORIYUKI;ISHIBASHI YOJI;ANZAI SHUNICHI
分类号 F23R3/08;F23L15/00;F23M5/00;F23M5/08;F23R3/42 主分类号 F23R3/08
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