{
  "$type": "site.standard.document",
  "description": "A gas turbine engine includes a first spool associated with a diffuser (68) and a primary combustor (70) and a second spool (12) associated with a secondary combustor (84). The first spool includes a first compressor and a first turbine mounted to a first shaft, and the second spool (12) includes a…",
  "path": "/patents/1395849",
  "publishedAt": "2025-04-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/08",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine includes a first spool associated with a diffuser (68) and a primary combustor (70) and a second spool (12) associated with a secondary combustor (84). The first spool includes a first compressor and a first turbine mounted to a first shaft, and the second spool (12) includes a second compressor (74) and a second turbine (82) mounted to a second shaft (76). An inlet duct (110) fluidly connects the diffuser (68) to the second compressor (74). An outlet duct assembly (80) fluidly connects the second turbine (82) to the diffuser (68) and the primary combustor (70).",
  "title": "GAS TURBINE ENGINE WITH AN OUTLET DUCT ASSEMBLY"
}