{
  "$type": "site.standard.document",
  "description": "A torch igniter system for a combustor of a gas turbine engine includes a housing (23) defining a combustion chamber (22), an ignition source (20) disposed at least partially in the combustion chamber, a fuel injector (40), a first fluid path (46) connecting a first fuel source (34) to the fuel…",
  "path": "/patents/1410141",
  "publishedAt": "2024-04-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/264",
    "COLLINS ENGINE NOZZLES INC [US]"
  ],
  "textContent": "A torch igniter system for a combustor of a gas turbine engine includes a housing (23) defining a combustion chamber (22), an ignition source (20) disposed at least partially in the combustion chamber, a fuel injector (40), a first fluid path (46) connecting a first fuel source (34) to the fuel injector, a second fluid path (50) connecting an air source (38) to the fuel injector, and a third fluid path (48) connecting a second fuel source (36) to the combustion chamber. The fuel injector is configured to inject fuel, air, or a mixture of fuel and air into the combustion chamber and to impinge on the ignition source.",
  "title": "TORCH IGNITER SYSTEM"
}