Patent · US Active

High effectiveness cooled turbine blade

US7625178B2 · kind B2 · utility

48Cited by
12References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 30, 2006
Grant dateDec 1, 2009
Priority date
Expiry dateOct 10, 2027

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49341
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

An air-cooled turbine blade is provided having an airfoil shape defined by a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root and a tip, the walls and the tip each including an interior surface that defines an interior with the root, the trailing edge including a plurality of slots formed thereon. The blade includes a suction side flow circuit formed therein comprising a forward and an aft flow circuit. The blade also includes a tip flow circuit extending along the tip interior surface to at least one of the trailing edge slots and including a first and a second opening, the first opening in flow communication with the suction side forward flow circuit outlet, and the second opening in flow communication with a cross-over hole of the suction side aft flow circuit. Methods of manufacturing the blade are also provided.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.