Turbine nozzle segment

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

Reexamination Certificate

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Reexamination Certificate

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06942453

ABSTRACT:
A turbine nozzle segment1of a turbine nozzle assembly comprises a plurality of stator vanes7, an arc-like inner band9integrally molded at the inner end of a plurality of the stator vanes7, an arc-like outer band11integrally molded at the outer end of a plurality of the stator vanes7. An outer band11includes an outer platform19, a forward outer leg21, a aft outer leg23and a hook member29formed at the back end and also in the central portion in the circumferential direction of the outer platform19.

REFERENCES:
patent: 2903237 (1959-09-01), Petrie et al.
patent: 4391565 (1983-07-01), Speak
patent: 4511306 (1985-04-01), Hultgren
patent: 4553901 (1985-11-01), Laurello
patent: 5131813 (1992-07-01), Przytulski et al.
patent: 5131814 (1992-07-01), Przytulski et al.
patent: 5232340 (1993-08-01), Morgan
patent: 5249920 (1993-10-01), Shepherd et al.
patent: 5333995 (1994-08-01), Jacobs et al.
patent: 5-26004 (1993-02-01), None
patent: 11-36802 (1999-02-01), None

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