Air/fuel supply system for use in a gas turbine engine
First Claim
1. A fuel injector for use in a combustor assembly of a gas turbine engine, the fuel injector comprising:
- a main body having an inlet end and an outlet end and defining a longitudinal axis defining a longitudinal direction of the fuel injector and extending between said outlet end and said inlet end, said main body comprising a plurality of air/fuel passages extending therethrough, each air/fuel passage including an inlet that receives air from a source of air and an outlet, wherein said air/fuel passages comprise hexagonal-shaped passages positioned in a honeycomb configuration; and
a fuel supply structure extending in said longitudinal direction and communicating with and supplying fuel to said air/fuel passages for providing an air/fuel mixture within each air/fuel passage, the air/fuel mixtures exiting said main body through respective air/fuel passage outlets, wherein said fuel supply structure includes isolated fuel distribution passages that individually deliver respective portions of fuel from said fuel supply structure to each of said air/fuel passages.
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Accused Products
Abstract
A fuel injector for use in a gas turbine engine combustor assembly. The fuel injector includes a main body and a fuel supply structure. The main body has an inlet end and an outlet end and defines a longitudinal axis extending between the outlet and inlet ends. The main body comprises a plurality of air/fuel passages extending therethrough, each air/fuel passage including an inlet that receives air from a source of air and an outlet. The fuel supply structure communicates with and supplies fuel to the air/fuel passages for providing an air/fuel mixture within each air/fuel passage. The air/fuel mixtures exit the main body through respective air/fuel passage outlets.
66 Citations
20 Claims
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1. A fuel injector for use in a combustor assembly of a gas turbine engine, the fuel injector comprising:
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a main body having an inlet end and an outlet end and defining a longitudinal axis defining a longitudinal direction of the fuel injector and extending between said outlet end and said inlet end, said main body comprising a plurality of air/fuel passages extending therethrough, each air/fuel passage including an inlet that receives air from a source of air and an outlet, wherein said air/fuel passages comprise hexagonal-shaped passages positioned in a honeycomb configuration; and a fuel supply structure extending in said longitudinal direction and communicating with and supplying fuel to said air/fuel passages for providing an air/fuel mixture within each air/fuel passage, the air/fuel mixtures exiting said main body through respective air/fuel passage outlets, wherein said fuel supply structure includes isolated fuel distribution passages that individually deliver respective portions of fuel from said fuel supply structure to each of said air/fuel passages. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. An air/fuel supply system for use in a combustor assembly of a gas turbine engine, the air/fuel supply system comprising:
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a fuel injector comprising; a main body having an inlet end and an outlet end and defining a longitudinal axis defining a longitudinal direction of said fuel injector and extending between said outlet end and said inlet end, said main body comprising a plurality of air/fuel passages extending therethrough, each air/fuel passage including an inlet that receives air from a source of air and an outlet, wherein said air/fuel passages comprise hexagonal-shaped passages positioned in a honeycomb configuration; and a fuel supply structure in said main body extending in said longitudinal direction, said fuel supply structure including at least one fuel inlet that receives fuel from a source of fuel and a plurality of fuel outlets, each said fuel outlet communicating with and supplying fuel to at least one of said air/fuel passages, wherein said fuel supply structure includes isolated fuel distribution passages that individually deliver respective portions of fuel from said fuel supply structure to each of said air fuel passages; and wherein air passing through each said air/fuel passage is mixed with fuel from at least one of said fuel outlets, said mixing occurring within each said air/fuel passage to produce an air/fuel mixture within each air/fuel passage, said air/fuel mixture within each said air/fuel passage exiting said outlet end of said main body through a respective air/fuel passage outlet. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification