Invention Grant
US09476592B2 System for injecting fuel in a gas turbine combustor 有权
在燃气轮机燃烧器中喷射燃料的系统

System for injecting fuel in a gas turbine combustor
Abstract:
A combustion system uses a fuel nozzle with an inner wall having a fuel inlet in fluid communication with a fuel outlet in a fuel cartridge. The inner wall defines a mounting location for inserting the fuel cartridge. A pair of annular lip seals around the cartridge outer wall on both sides of the fuel outlet seals the fuel passage between the fuel inlet and the fuel outlet.
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