发明名称 COMBUSTOR AND GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To improve durability of a combustion cylinder by preventing thermal fatigue in a connecting part of the combustion cylinder and a bypass tube. SOLUTION: Air and fuel compressed by a compressor is made to react and combusted by the combustor which introduces generated combustion gas into a turbine through a combustion cylinder 5. A through-hole 20 is formed on a side wall of the bypass tube 6 for introducing air into the combustion cylinder 5, and a sleeve 21 for guiding air which is sucked into the bypass tube 6 through the through-hole 20, to the connecting part of the combustion cylinder 5 and the bypass tube 6, is provided inside the bypass tube 6. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004092409(A) 申请公布日期 2004.03.25
申请号 JP20020251025 申请日期 2002.08.29
申请人 MITSUBISHI HEAVY IND LTD 发明人 TANAKA KATSUNORI;KISHIDA HIROAKI
分类号 F02C7/18;(IPC1-7):F02C7/18 主分类号 F02C7/18
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