Combustion liner for gas turbine formed of cast nickel-based...

Details Combustion liner for gas turbine formed of cast nickel-based... Combustion liner for gas turbine formed of cast nickel-based...

2005-11-21

2009-06-02

Casaregola, Louis J (Department: 3741)

Power plants

Combustion products used as motive fluid

Combustion products generator

C431S356000

Reexamination Certificate

active

07540156

ABSTRACT:
A combustion liner for a gas turbine combustion system is provided. The combustion liner comprises a combustion zone between an inlet end and an exhaust end. The combustion liner comprises a one-piece casting construction. The combustion liner is formed from a nickel-based superalloy having strength characteristics.

REFERENCES:
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patent: 4236378 (1980-12-01), Vogt
patent: 5335502 (1994-08-01), Roberts et al.
patent: 6416596 (2002-07-01), Wood et al.
patent: 6428637 (2002-08-01), Wood et al.
patent: 6553767 (2003-04-01), Farmer et al.
patent: 2004/0079083 (2004-04-01), Stumpf et al.
patent: WO 99/06771 (1999-02-01), None

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