发明名称 TURBINE COMPONENT INTERNAL HEATING SYSTEMS AND COATING SYSTEMS
摘要 Turbine component internal heating systems (10) include at least one turbine component support platform (20) that supports a turbine component (50) having one or more internal cavities (55) by temporarily engaging at least a side wall (51) of the turbine component (50), and, at least one heat source (30) that extends from the at least one turbine component support platform (20), wherein when the at least one turbine component support platform (20) supports the turbine component (50), the at least one heat source (30) is at least partially disposed within at least one of the one or more internal cavities (55) such that it can heat the turbine component (50) from the inside.
申请公布号 EP2942420(B1) 申请公布日期 2017.02.22
申请号 EP20150165276 申请日期 2015.04.27
申请人 General Electric Company 发明人 Levy, Lawrence Matthew;Souther, Ronald Lee
分类号 C23C4/12;B05B13/02;B05B15/04;C23C4/02;F01D25/28 主分类号 C23C4/12
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