{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "A torch ignitor system for combustor of a gas turbine engine includes a torch ignitor (10), the torch ignitor (10) having a combustion chamber oriented about an axis, the combustion chamber having axially upstream and downstream ends (102, 104) defining a flow direction through the combustion…",
  "path": "/patents/1409076",
  "publishedAt": "2024-05-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/00",
    "COLLINS ENGINE NOZZLES INC [US]"
  ],
  "textContent": "A torch ignitor system for combustor of a gas turbine engine includes a torch ignitor (10), the torch ignitor (10) having a combustion chamber oriented about an axis, the combustion chamber having axially upstream and downstream ends (102, 104) defining a flow direction through the combustion chamber, along the axis. The torch ignitor system also includes a cap (34) defining the axially upstream end of the combustion chamber and oriented about the axis, wherein the cap (34) is configured to receive a fuel injector (45) and at least one glow plug (50), a tip (106) at a downstream end of the combustion chamber, and a passage (108) for pressurized oxygen containing gas passing through the cap (34) from an exterior of the combustion chamber and in fluid communication with the combustion chamber.",
  "title": "TORCH IGNITOR SYSTEM WITH GAS ASSIST START"
}