{
  "$type": "site.standard.document",
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  "description": "An embodiment of a torch ignitor system for a combustor of a gas turbine engine includes a torch ignitor (10), the torch ignitor include a combustion chamber (16) oriented about a torch axis (A), the combustion chamber having axially upstream (102) and downstream (104) ends defining a flow…",
  "path": "/patents/1409087",
  "publishedAt": "2024-03-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/264",
    "COLLINS ENGINE NOZZLES INC [US]"
  ],
  "textContent": "An embodiment of a torch ignitor system for a combustor of a gas turbine engine includes a torch ignitor (10), the torch ignitor include a combustion chamber (16) oriented about a torch axis (A), the combustion chamber having axially upstream (102) and downstream (104) ends defining a flow direction through the combustion chamber, along the axis. The torch ignitor further includes a tip (106) at a downstream end of the elbow for issuing the injection of combustion products. An embodiment of a method (200) includes initiating combustion (202) in a combustion chamber of a torch ignitor to produce an ignition jet flame extending along an ignition jet flame axis, and igniting (206) a fuel/air mixture in a gas turbine combustor by issuing a respective spray cone of the fuel/air mixture from a respective fuel injectors in a plurality of fuel injectors, wherein the ignition jet flame axis intersects a plurality of the spray cones.",
  "title": "TORCH IGNITOR SYTEM FOR A COMBUSTOR OF A GAS TURBINE ENGINE AND METHOD OF OPERATING THE SAME"
}