发明名称 Gas turbine and turbine rotor for a gas turbine
摘要 A refrigerant supplied from a refrigerant supply pipe flows into a first space, being a passage of the refrigerant, from a space between first stage and second stage rotor disks. The refrigerant supplied to the first space is guided to second, third and forth spaces through a gap between a spindle bolt and a bolt hole, during which the rotor disks are warmed up or cooled. In the second stage rotor disk, a refrigerant through hole axially penetrating this rotor disk is provided near the center thereof. The refrigerant flowing into the first space passes through the refrigerant through hole to flow into the second space, to thereby promote the convection in the first, second, third and fourth spaces and equalization of temperatures in the rotor disks.
申请公布号 US2003133786(A1) 申请公布日期 2003.07.17
申请号 US20030339293 申请日期 2003.01.10
申请人 MITSUBISHI HEAVY INDUSTRIES LTD. 发明人 UEMATSU KAZUO;HIROKAWA KAZUHARU
分类号 F01D5/06;F01D5/08;F02C6/18;F02C7/16;(IPC1-7):F01D5/14 主分类号 F01D5/06
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