Multi-point staging strategy for low emission and stable combustion
AssigneeUnited Technologies Corporation
InventorsAlexander G. Chen, Donald W. Kendrick
Life of this patent
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Abstract
The present invention relates to an improved multi-point injector for use in a gas turbine engine or other types of combustors. The multi-point fuel injector has a plurality of nozzles arranged in at least two arrays such as concentric rings. The injector further has different fuel circuits for independently controlling the fuel flow rate for the nozzles in each of the arrays. Each of the nozzles include a fluid channel and one or more swirler vanes in the fluid channel for creating a swirling flow within the fluid channel. A method for injecting a fuel/air mixture into a combustor stage of a gas turbine engine is also described. At least one zone has a flame hot enough to stabilize the entire combustor flame.
Claims7
A multi-point fuel injector for use in a combustor stage of a gas turbine engine comprising:
- a plurality of nozzles arranged in at least two arrays;
- each of said nozzles in each of said arrays having an inlet and an outlet;
- said nozzle outlets in each of said arrays being arranged in a common plane to promote flame stability and interaction between the nozzles in adjacent arrays;
- means for independently controlling a flow of fuel to the nozzles in each said array;
- and
- wherein each of said arrays defines a zone and said injector further comprises means for controlling flow to a first zone as a function of flow to a second zone.
Dependencies are inferred from the claim text.