发明名称 Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine
摘要 Described is a cooled gas turbine guide blade for a gas turbine, with a hollow blade profile which comprises an onflow edge onto which a working medium is capable of flowing, and with, for guiding a cooling medium, an onflow edge duct running inside the blade profile along the onflow edge. Furthemore, to the use of such a gas turbine guide blade and to a method for operating a gas turbine with an abovementioned gas turbine guide blade. In order to provide a gas turbine guide blade with an increased lifetime by means of the invention, it is proposed that, in the onflow edge duct, an electrical heating element be provided, which extends approximately completely over the entire length of the onflow edge duct and through which a heating current flows, before the operation of the gas turbine, for the preheating of the gas turbine guide blade.
申请公布号 US7465150(B2) 申请公布日期 2008.12.16
申请号 US20060479183 申请日期 2006.06.30
申请人 SIEMENS AKTIENGESELLACHAFT 发明人 AHMAD FATHI
分类号 F01D9/06;F01D25/10;F01D25/12 主分类号 F01D9/06
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