发明名称 Tip Shrouded Turbine Blade
摘要 A turbine blade is provided comprising: an airfoil including upper and lower ends; a root coupled to the airfoil lower end; a shroud coupled to the airfoil upper end; and at least one sealing rail extending radially outwardly from an upper surface of the shroud and extending generally along a circumferential length of the shroud. The sealing rail may comprise a mid-section, opposing end sections and at least one intermediate section located between the mid-section and one of the opposing end sections. An axial thickness of the rail may vary.
申请公布号 US2010290897(A1) 申请公布日期 2010.11.18
申请号 US20090464492 申请日期 2009.05.12
申请人 BEECK ALEXANDER R;NELLIAN SANKAR 发明人 BEECK ALEXANDER R.;NELLIAN SANKAR
分类号 F01D11/08;F01D5/22 主分类号 F01D11/08
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