Turbine bucket shroud internal core profile

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

Reexamination Certificate

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Details

C416S191000, C416S22300B, C416S232000

Reexamination Certificate

active

07976280

ABSTRACT:
A turbine bucket including a bucket airfoil having a hollow tip shroud, the hollow tip shroud having a hollow core having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I, in inches, wherein the shape of the core is defined by the cloud of points listed which are distributed around each surface of the shroud, and the complete hollow portion of the tip shroud could be constructed by defining smooth sheet surfaces through the listed points.

REFERENCES:
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patent: 6722851 (2004-04-01), Brittingham et al.
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patent: 6994520 (2006-02-01), Humanchuk et al.
patent: 7887295 (2011-02-01), Brittingham et al.
U.S. Application of Brittingham et al.; U.S. Appl. No. 11/987,315, filed Nov. 29, 2007.
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