发明名称 |
TURBINE ENGINE COMPONENT AND METHOD OF IMPROVING STRENGTH, CREEP AND FAILURE RESISTANCE OF SINGLE CRYSTAL COMPONENT |
摘要 |
PROBLEM TO BE SOLVED: To provide a method of improving the strength and failure resistance of single crystal gas turbine components. SOLUTION: The method of improving the strength and failure resistance of single crystal components broadly comprises the steps of forming a component having a single crystal microstructure with a plurality ofγ' platens and forming a limited amount of oriented platens in a particular direction prior to the component being placed into service to delay coalescence of the platens relative to the applied load. The platens in a limited amount may be pre-oriented in the direction parallel to the tensile loading expected in service or pre-oriented to be perpendicular to expected compressive loading, thus rafting caused by loading in service is delayed, so as to improve material characteristics such as creep resistance. COPYRIGHT: (C)2007,JPO&INPIT
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申请公布号 |
JP2007204849(A) |
申请公布日期 |
2007.08.16 |
申请号 |
JP20070023723 |
申请日期 |
2007.02.02 |
申请人 |
UNITED TECHNOL CORP <UTC> |
发明人 |
STAROSELSKY ALEXANDER;SIDWELL CARROLL V |
分类号 |
C22F1/10;C22C19/05;C22F1/00;C30B29/52;C30B33/02;F01D5/28;F01D25/00;F02C7/00 |
主分类号 |
C22F1/10 |
代理机构 |
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主权项 |
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