Conical tip shroud fillet for a turbine bucket

a turbine bucket and conical tip technology, applied in the field of variable conical fillets, can solve the problems of premature failure of the bucket, reduced creep life of the tip shroud, and significant decreases in the life of the bucket, so as to minimize stress, minimize creep as well as the mass of the fillet, and reduce the effect of reducing the stress

a turbine bucket and conical tip technology, applied in the field of variable conical fillets, can solve the problems of premature failure of the bucket, reduced creep life of the tip shroud, and significant decreases in the life of the bucket, so as to minimize stress, minimize creep as well as the mass of the fillet, and reduce the effect of reducing the stress

US20050036890A1Inactive Publication Date: 2005-02-17GENERAL ELECTRIC CO

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  • Conical tip shroud fillet for a turbine bucket
  • Conical tip shroud fillet for a turbine bucket
  • Conical tip shroud fillet for a turbine bucket

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

Referring now to the drawings, particularly to FIG. 1, there is illustrated a hot gas path, generally designated 10, of a gas turbine 12 including a plurality of turbine stages. Three stages are illustrated. For example, the first stage comprises a plurality of circumferentially spaced nozzles 14 and buckets 16. The nozzles are circumferentially spaced one from the other and fixed about the axis of the rotor. The first stage buckets 16, of course, are mounted on the turbine rotor 17 via a rotor wheel 19. A second stage of the turbine 12 is also illustrated, including a plurality of circumferentially spaced nozzles 18 and a plurality of circumferentially spaced buckets 20 mounted on the rotor 17 via a rotor wheel 21. The third stage is also illustrated including a plurality of circumferentially spaced nozzles 22 and buckets 24 mounted on rotor 17 via a rotor wheel 23. It will be appreciated that the nozzles and buckets lie in the hot gas path 10 of the turbine, the direction of flow...

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Abstract

A turbine bucket airfoil has a conical fillet about the intersection of the airfoil tip and tip shroud having a nominal profile in accordance with coordinate values of X and Y, offset 1, offset 2 and Rho set forth in Table I. The shape parameters of offset 1, offset 2 and Rho define the configuration of the fillet at the specified X and Y locations about the fillet to provide a fillet configuration accommodating high localized stresses. The fillet shape may be parabolic, elliptical or hyperbolic as a function of the value of the shape parameter ratio of D1D1+D2at each X, Y location where D1 is a distance between an intermediate point along a chord between edge points determined by offsets O2 and O2 and a shoulder point on the fillet surface and D2 is a distance between the shoulder point and an apex location at the intersection of the airfoil tip and tip shroud.

Description

BACKGROUND OF THE INVENTION The present invention relates to a variable conical fillet between an airfoil tip of a turbine bucket and a bucket tip shroud and particularly relates to a conical fillet shaped and sized to improve part life, performance and manufacturing of the turbine bucket Turbine buckets generally comprise an airfoil, a platform, shank and dovetail along a radial inner end portion of the bucket and often a tip shroud at the tip of the airfoil in mechanical engagement with tip shrouds of adjacent buckets. The tip shroud and airfoil of a conventional turbine bucket are typically provided with a simple fillet shape of a predetermined size and generally of a constant radius about the intersection of the tip shroud and the airfoil tip. That is, a generally uniform radius was applied to the shroud fillet as the fillet was applied about the intersection of the airfoil tip and tip shroud. The fillet lowered the stress concentration between the airfoil and tip shroud. Whi...

Claims

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Application Information

Patent Timeline
17 Feb 2005
Publication
US20050036890A1
IPC
F01D5/14; F01D11/08; F01D5/16
CPC
F01D5/147; F01D5/225; F05D2260/94; Y10S415/914; F05D2250/70; F05D2250/14; F05D2250/17; F05D2250/16
Inventors
TOMBERG, STEVEN ERIC; NEELEY, MARVIN LUTHER