发明名称 GAS TURBINE
摘要 <p>Disposed internally of a first blade ring member (8) and a second blade ring member (9) are blade ring cooling passageways (14, 15). These blade ring cooling passageways (14, 15) are made to communicate with each other by an axially installed connection pipe (16). Fixed blade cooling air (17) is fed under pressure from the outside of a car interior (1) into a fixed blade added to the blade ring inner wall, and thermal shields (18) are installed on the outer surface of the blade rings (14, 15) and on the outer surface of the connection pipe (16), with a clearance therebetween. Partitions for stagnating the fixed blade cooling air (17) are installed in the clearances between the outer surfaces of the blade rings (8, 9) and connection pipe (16) and the thermal shields (18).</p>
申请公布号 WO2002099253(P1) 申请公布日期 2002.12.12
申请号 JP2002005470 申请日期 2002.06.04
申请人 发明人
分类号 主分类号
代理机构 代理人
主权项
地址