{
  "$type": "site.standard.document",
  "description": "The present application thus provides a gas turbine engine system (100). The gas turbine engine system (100) may include a gas turbine engine (110), a nitrogen oxides reduction system (200) in communication with a flow of combustion gases (160) downstream from the gas turbine engine (110), and a…",
  "path": "/patents/994876",
  "publishedAt": "2012-12-19T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/54",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The present application thus provides a gas turbine engine system (100). The gas turbine engine system (100) may include a gas turbine engine (110), a nitrogen oxides reduction system (200) in communication with a flow of combustion gases (160) downstream from the gas turbine engine (110), and a nitrogen oxides controller (300) to control the ratio of nitrogen dioxide to nitrogen oxides in the flow of combustion gases (160) entering the nitrogen oxides reduction system (200).",
  "title": "Systems and methods for combustor emissions control"
}