{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "A gas turbine engine system (10) includes a compressor (12), a combustor (14), and a turbine (16); a fuel system (20) comprising one or more fuel circuits (102) configured to provide fuel from a fuel flow to the combustor; a non-catalytic fuel reformer (32, 100) in fluid communication with the one…",
  "path": "/patents/1007366",
  "publishedAt": "2011-12-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine engine system (10) includes a compressor (12), a combustor (14), and a turbine (16); a fuel system (20) comprising one or more fuel circuits (102) configured to provide fuel from a fuel flow to the combustor; a non-catalytic fuel reformer (32, 100) in fluid communication with the one or more fuel circuits, wherein the non-catalytic fuel reformer is configured to receive an oxidant from an oxidant flow and a fraction of fuel in the one or more fuel circuits in a predetermined ratio and reform the fraction of the fuel to produce a reformate; and a control system (18) configured to regulate at least one of fuel flow and oxidant flow to the non-catalytic fuel reformer to control a Modified Wobbe Index of the fuel entering the combustor..",
  "title": "Gas turbine combustion system with rich premixed fuel reforming and methods of use thereof"
}