Low leakage turbine nozzle

Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Circumferentially spaced nozzle or stator segments

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Details

415138, F01D 520

Patent

active

056558767

ABSTRACT:
A turbine nozzle includes a circumferentially continuous annular outer band, and a plurality of circumferentially spaced apart vanes extending radially inwardly therefrom. A circumferentially segmented inner band is joined to the vanes and is disposed coaxially with the outer band. The inner band includes a plurality of circumferentially adjoining arcuate segments, adjacent ones of which have circumferentially facing end faces spaced apart to define a gap therebetween. In an exemplary embodiment, strip seals are inserted in corresponding slots formed in the end faces to seal leakage therebetween.

REFERENCES:
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patent: 3661477 (1972-05-01), Westrum
patent: 3975114 (1976-08-01), Kalkbrenner
patent: 4509238 (1985-04-01), Lee et al.
patent: 4701102 (1987-10-01), Pisz et al.
patent: 4762462 (1988-08-01), Lardellier
patent: 4818834 (1989-04-01), Rupert
patent: 5409415 (1995-04-01), Kawanami et al.
patent: 5531457 (1996-07-01), Tibbott et al.

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