发明名称 SHAFT STRUCTURE AND BEARING STRUCTURE FOR TAIL END OF ROTOR OF GAS TURBINE
摘要 A shaft structure of a rotor tail end of a gas turbine in which a steam passage for supplying and recovering a steam for cooling rotor blades of the gas turbine extends along a center axis of the rotor assembly of the gas turbine is provided, wherein a center hole of the rotor tail end coaxial to the center axis of the steam passage is formed in the rotor tail end. Provision is also made of a thermal sleeve between the steam passage and the inner surface of the center hole of the rotor tail end, so that a thermal insulation gas layer is formed between the inner surface of the center hole of the rotor tail end and the thermal sleeve. The thermal insulation gas layer is isolated gas-tightly and liquid-tightly from the outside.
申请公布号 CA2481810(A1) 申请公布日期 2002.03.26
申请号 CA20012481810 申请日期 2001.08.31
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 HIROKAWA, KAZUHARU;OYA, TAKEAKI;SHINOHARA, TANEHIRO;UEMATSU, KAZUO;TANIOKA, TADATERU;TANAKA, KATSUNORI
分类号 F01D5/02;F01D5/08;F01D5/18;F01D25/08;F01D25/12;F01D25/16;(IPC1-7):F01D5/08 主分类号 F01D5/02
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