发明名称 TURBINE BLADE, ITS MANUFACTURING METHOD AND METHOD OF MEASURING TURBINE BLADE STRESS AND TURBINE BLADE TEMPERATURE
摘要 PROBLEM TO BE SOLVED: To improve the toughness and heat resistance of a turbine blade or a turbine wheel using a TiAl based alloy. SOLUTION: The turbine blade comprises a turbine blade body containing a TiAl based alloy and a first coating 3 formed in a plating method to cover the turbine blade body 2 with a Ni containing material having toughness higher than that of the turbine blade body 2. It is acceptable that the first coating 3 contains Cd 4 and the first coating 3 is covered with a second coating of a heat resistant material such as Cr higher than that of the first coating 3. COPYRIGHT: (C)2003,JPO
申请公布号 JP2003269105(A) 申请公布日期 2003.09.25
申请号 JP20020074961 申请日期 2002.03.18
申请人 MITSUBISHI HEAVY IND LTD 发明人 SHINDO KENTARO;TETSUI TOSHIMITSU;YOSHINO KAZUHIKO
分类号 F01D5/28;F01D25/00;F02C7/00;(IPC1-7):F01D5/28 主分类号 F01D5/28
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