发明名称 GAS TURBINE AND METHOD OF FORMING COMBUSTOR INSERTION HOLE OF GAS TURBINE
摘要 <p><P>PROBLEM TO BE SOLVED: To easily assemble or disassemble a gas turbine. <P>SOLUTION: The gas turbine 1 is provided with a combustor 39, combustion part casing 31 cylindrically formed and storing the combustor 39 inside, and a combustor insertion hole 31a formed in the side circumferential part of the combustion part casing 31. The size of the insertion hole 31a in a direction perpendicular to the circumferential direction of the combustion part casing 31 is made to be larger than the size of the hole 31a in the circumferential direction of the combustion part casing 31. Also, when the combustor 39 inserted into the hole, a member moved with the combustor 39 and the hole are viewed from the moving direction of the combustor 39, the hole is formed so as to involve the entire externals of the combustor 39 and the member moving with the combustor 39. <P>COPYRIGHT: (C)2010,JPO&INPIT</p>
申请公布号 JP2009243309(A) 申请公布日期 2009.10.22
申请号 JP20080088746 申请日期 2008.03.28
申请人 MITSUBISHI HEAVY IND LTD 发明人 NAKAMURA SOSUKE;ARASE KENICHI;MOTOYAMA NOBUHIKO
分类号 F02C7/20;F02C7/00;F23R3/60 主分类号 F02C7/20
代理机构 代理人
主权项
地址