{
  "$type": "site.standard.document",
  "description": "A low emission turbine includes a reverse flow can-type combustor (102) that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at conditions other than design set point. The reverse…",
  "path": "/patents/1079096",
  "publishedAt": "2005-03-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/00",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A low emission turbine includes a reverse flow can-type combustor (102) that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at conditions other than design set point. The reverse flow can-type combustor (102) generally includes a swirler and mixer assembly (140) within the combustor, wherein each swirler and mixer assembly (140) comprises and array of annularly arranged swirlers and mixers, which include a primary and secondary fuel delivery system that can be independently controlled. Also disclosed herein is a can-type combustor (102) that includes fluid passageways (142) that perpendicularly impinge the backside of a heat shield (136). Processes for operating the can-type combustors are also disclosed.",
  "title": "Method and apparatus for reducing gas turbine engine emissions"
}