发明名称 Turbine blade
摘要 The turbine has a ring of aerofoil blades mounted between inner and outer end blocks. The working fluid path between adjacent blades is closed in cross-section by the end walls formed by the end blocks. The blades and their associated end blocks are formed integrally and machined to provide fillets between the blade aerofoil surfaces and the end walls. The fillets have a radius in the range 0.15 to 0.3 of a throat dimension between adjacent blades. The fillets multiplying factor of the fillet radius lies in the range 0.2 to 0.25.
申请公布号 GB9417406(D0) 申请公布日期 1994.10.19
申请号 GB19940017406 申请日期 1994.08.30
申请人 GEC ALSTHOM LIMITED 发明人
分类号 F01D5/14;F01D9/02 主分类号 F01D5/14
代理机构 代理人
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