{
  "$type": "site.standard.document",
  "description": "A turbine engine (10) having a compressor section (12), a combustion section (14) and a turbine section (16) in serial flow arrangement. The turbine engine (10) further having a combustor (80), provided within the combustion section (14), defining a combustion chamber (86) and having at least one…",
  "path": "/patents/1398933",
  "publishedAt": "2025-06-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/00",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A turbine engine (10) having a compressor section (12), a combustion section (14) and a turbine section (16) in serial flow arrangement. The turbine engine (10) further having a combustor (80), provided within the combustion section (14), defining a combustion chamber (86) and having at least one fuel injector (76). The fuel injector (140) having a fuel channel (120), a first set of fuel orifices (122), and a flow restrictor (124) located within the fuel channel (120) and having a second set of fuel orifices (126).",
  "title": "COMBUSTOR WITH A FUEL INJECTOR"
}