{
  "$type": "site.standard.document",
  "description": "A fuel supply system (100) for a combustion section (114) of a turbine engine (10). The turbine engine (10) including a heat source (110). The fuel supply system (100) comprising a first fuel supply (102) having a liquid fuel, a second fuel supply (104) having a first gaseous fuel, and a heat…",
  "path": "/patents/1398166",
  "publishedAt": "2026-04-22T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/22",
    "GE AVIO SRL [IT]"
  ],
  "textContent": "A fuel supply system (100) for a combustion section (114) of a turbine engine (10). The turbine engine (10) including a heat source (110). The fuel supply system (100) comprising a first fuel supply (102) having a liquid fuel, a second fuel supply (104) having a first gaseous fuel, and a heat exchanger (108) fluidly coupled to the first fuel supply (102) and the heat source (110). The heat exchanger (108) producing a heat sufficient to change the liquid fuel to a second gaseous fuel that is the same type of fuel as the first gaseous fuel.",
  "title": "FUEL SUPPLY SYSTEM FOR A COMBUSTOR"
}