发明名称 TURBINE ROTOR FOR GAS TURBINE, AND GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To uniformize temperatures of a turbine rotor. SOLUTION: A cooling medium supplied from cooling medium supply pipes 25 flows into a space A as a cooling medium passage via a clearance between rotors disks 50a and 50b. The cooling medium supplied into the space A is led to spaces B to D via clearances between spindle bolts 60 and bolt holes 62, and in this process, warms and cools the rotor disks 50a to 50d. The rotor disk 50b of a second stage has a cooling medium passing hole 70 axially through the rotor disk 50b about the center thereof. The cooling medium flowing into the space A flows into the space B also via the cooling medium passing hole 70 to promote convection in the spaces A to D and promote the temperature evenness of the rotor disk 50b, etc. COPYRIGHT: (C)2003,JPO
申请公布号 JP2003206701(A) 申请公布日期 2003.07.25
申请号 JP20020005031 申请日期 2002.01.11
申请人 MITSUBISHI HEAVY IND LTD 发明人 UEMATSU KAZUO;HIROKAWA KAZUHARU
分类号 F01D5/06;F01D5/08;F02C6/18;F02C7/16;(IPC1-7):F01D5/08 主分类号 F01D5/06
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