Gas turbine and gas turbine nozzle

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Plural rigidly related blade sets

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415200, 148428, 148425, 420448, 420436, C22C 3000, C22C 1905, F01D 102

Patent

active

054802830

ABSTRACT:
A Ni-base superalloy consisting essentially of, by weight: 0.05 to 0.20% C, 20 to 25% Co, 15 to 25% Cr, 1.0 to 3.0% Al, 1.0 to 3.0% Ti, 1.0 to 3.0% Nb, 5 to 10% W, and at least 55% Ni, the combination of the [Al+Ti] and tungsten contents being determined as shown in FIG. 5. This superalloy has a high thermal-fatigue resistance, a great high-temperature strength, particularly, a great creep rupture strength, and a good weldability. The superalloy is used to form gas turbine nozzles, which are employed in a gas turbine. Using such a gas turbine, a combined power generating system is built.

REFERENCES:
patent: 4850187 (1989-07-01), Siga et al.
patent: 5008072 (1991-04-01), Siga et al.
patent: 5370497 (1994-12-01), Doi et al.

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