发明名称 MODULAR BLADE OR VANE FOR GAS TURBINE, AND GAS TURBINE WITH SUCH BLADE OR VANE
摘要 PROBLEM TO BE SOLVED: To provide a modular blade or vane, in which individual components are arranged in a way to improve the mechanical stability and maintainability of the blade or vane and an improved internal cooling of the blade or vane can be performed with a less amount of cooling medium, and to provide a gas turbine with such a blade or vane.SOLUTION: An outer shell (34) is joined in a combined manner to a carrying structure (33) via a first joint in a region below a platform level (56) of a platform. The outer shell (34) is also joined to the carrying structure (33) via at least one additional joint, which is a form-fitting joint, allowing relative movement in a longitudinal direction between the outer shell (34) and the carrying structure (33).
申请公布号 JP2014047788(A) 申请公布日期 2014.03.17
申请号 JP20130179557 申请日期 2013.08.30
申请人 ALSTOM TECHNOLOGY LTD 发明人 HERBERT BRANDL
分类号 F01D5/18;F01D9/02;F01D25/00;F01D25/12;F02C7/00;F02C7/16 主分类号 F01D5/18
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