Method for forming thermal barrier coating on hot-gas-path components of gas turbine during operation,申请号KR20090058581-传众专利搜索

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发明名称	Method for forming thermal barrier coating on hot-gas-path components of gas turbine during operation
摘要
申请公布号	KR101125329(B1)	申请公布日期	2012.03.27
申请号	KR20090058581	申请日期	2009.06.29
申请人		发明人
分类号	B05D5/00;B05D1/08;B05D7/14	主分类号	B05D5/00
代理机构		代理人
主权项
地址

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