{
  "$type": "site.standard.document",
  "description": "A fuel injector for a gas turbine engine includes a compression section, combustion section, and turbine section in serial flow arrangement. The fuel injector arranged in the combustion section and includes an inner nozzle defining a fuel injector axis and an outer nozzle in annular arrangement…",
  "path": "/patents/1380454",
  "publishedAt": "2026-04-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "General Electric Company"
  ],
  "textContent": "A fuel injector for a gas turbine engine includes a compression section, combustion section, and turbine section in serial flow arrangement. The fuel injector arranged in the combustion section and includes an inner nozzle defining a fuel injector axis and an outer nozzle in annular arrangement about the inner nozzle. The outer nozzle at least partially defines a mixing region. An inner air passage and an outer air passage exhaust to the mixing region. A fuel body positions between the inner air passage and the outer air passage and has an outer fuel passage exhausting to the mixing region.",
  "title": "FUEL INJECTOR FOR A TURBINE ENGINE"
}