Gas turbine combustor

Details Gas turbine combustor Gas turbine combustor

1985-07-11

1986-11-11

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

148410, F02C 100, C22C 1905

Patent

active

046214992

ABSTRACT:
A gas turbine combustor defines a combustion chamber for combustion of injected fuel and for introduction of the resultant hot combustion gas to nozzles of a gas turbine. The combustor has parts subjected to hot combustion gas during operation of the turbine, such as a cap connected to a fuel injection nozzle, a liner connected to the cap, and a transition piece connected to the liner. These parts subjected to the hot combustion gas are made from an alloy having a composition consisting essentially of 0.02 to 0.2 wt % of C, 15 to 30 wt % of Cr and 10 to 25 wt % of W.

REFERENCES:
patent: 3099134 (1963-07-01), Calder et al.
patent: 3937628 (1976-02-01), Watanabe et al.
patent: 4283234 (1981-08-01), Fukui et al.

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