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Flame holding tolerant fuel and air premixer for a gas turbine combustor

  • US 8,312,722 B2
  • Filed: 10/23/2008
  • Issued: 11/20/2012
  • Est. Priority Date: 10/23/2008
  • Status: Expired due to Fees
First Claim
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1. A fuel nozzle comprising:

  • an outer peripheral wall and an inner peripheral wall proximate said outer wall, said outer wall and said inner wall defining an annular cavity therebetween, said annular cavity forming a peripheral cooling passage;

    a nozzle center body disposed within said outer wall, the nozzle center body comprising;

    an end wall at a distal end thereof;

    a gas fuel passage defined within said nozzle center body and extending at least part of a length therein; and

    a nozzle cooling passage defined within said nozzle center body and extending at least part circumferentially of a length therein, the nozzle cooling passage defining an inlet for flow of a cooling fluid;

    a fuel/air premixer surrounding a proximal end portion of said nozzle center body and including an air inlet, a fuel inlet, and a plurality of vanes in flow communication with the fuel inlet;

    wherein said inner peripheral wall and said nozzle center body define a premixing passage therebetween, into which said premixing passage said fuel/air premixer discharges; and

    wherein said cooling fluid is conveyed from said nozzle cooling passage to said peripheral cooling passage;

    wherein said nozzle cooling passage is in fluid communication with a source of air or inert gas; and

    wherein said peripheral cooling passage is in flow communication with said premixing passage through at least one outlet orifice.

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