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US 2011/0209481 A1Published application
Turbine Combustor End Cover
AssigneeGeneral Electric Company
InventorScott Robert Simmons
Life of this patent
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Abstract
An end cover assembly for a combustor includes a first plate receptive of one of more combustor fuel nozzles and a second plate. One or more intermediate plates are located between the first plate and the second plate and define one or more cavities to distribute fuel to one or more combustor fuel nozzles. The first plate, the second plate, and the one or more intermediate plates are secured in a stack.
Claims20
An end cover assembly for a combustor comprising:
- a first plate receptive of one of more combustor fuel nozzles;
- a second plate;
- and
- one or more intermediate plates disposed between the first plate and the second plate, the one or more intermediate plates defining one or more cavities to distribute fuel to one or more combustor fuel nozzles;
- wherein the first plate, second plate and one or more intermediate plates are secured in a stack.
2 more elements
A combustor for a turbomachine comprising:
- one or more combustor fuel nozzles;
- and
- an end cover assembly operably connected to the one or more combustor fuel nozzles including:
- a first plate receptive of the one of more combustor fuel nozzles;
- a second plate;
- and
- one or more intermediate plates disposed between the first plate and the second plate, the one or more intermediate plates defining one or more cavities to distribute fuel to one or more combustor fuel nozzles;
- wherein the first plate, second plate and one or more intermediate plates are secured in a stack.
5 more elements
Dependencies are inferred from the claim text.