Turbine blade with blade tip cooling passages

Details Turbine blade with blade tip cooling passages Turbine blade with blade tip cooling passages

2011-04-12

2011-04-12

Kershteyn, Igor (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

Changing state mass within or fluid flow through working...

C416S09700R, C415S115000, C415S173400, C415S173500

Reexamination Certificate

active

07922451

ABSTRACT:
A turbine blade for use in an industrial gas turbine engine, the blade having a squealer pocket with a plurality of discrete curved cooling channels to cool the blade tip and to reduce the hot gas flow leakage across the tip. The curved cooling channels include a side wall cooling channel, a tip rail crown cooling channel and an inner tip rail wall cooling channel all discharging cooling air from a cooling supply channel within the airfoil. Both the pressure side and suction side tip rails include this arrangement of cooling channels.

REFERENCES:
patent: 3899267 (1975-08-01), Dennis et al.
patent: 4142824 (1979-03-01), Andersen
patent: 4487550 (1984-12-01), Horvath et al.
patent: 4589823 (1986-05-01), Koffel
patent: 4893987 (1990-01-01), Lee et al.
patent: 5192192 (1993-03-01), Ourhaan
patent: 5403158 (1995-04-01), Auxier
patent: 5564902 (1996-10-01), Tomita
patent: 5660523 (1997-08-01), Lee
patent: 5733102 (1998-03-01), Lee et al.
patent: 6190129 (2001-02-01), Mayer et al.
patent: 6224336 (2001-05-01), Kercher
patent: 6224337 (2001-05-01), Lieland et al.
patent: 6461108 (2002-10-01), Lee et al.
patent: 6527514 (2003-03-01), Roeloffs
patent: 6602052 (2003-08-01), Liang
patent: 6837687 (2005-01-01), Lee et al.
patent: 7192250 (2007-03-01), Boury et al.

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