{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (300) includes a primary gas path (106) having, in fluid series communication: a primary air inlet (112), a compressor (104) fluidly connected to the primary air inlet (112), a combustor (108) fluidly connected to an outlet of the compressor, and a turbine fluidly connected to…",
  "path": "/patents/1402789",
  "publishedAt": "2024-11-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A gas turbine engine (300) includes a primary gas path (106) having, in fluid series communication: a primary air inlet (112), a compressor (104) fluidly connected to the primary air inlet (112), a combustor (108) fluidly connected to an outlet of the compressor, and a turbine fluidly connected to an outlet of the combustor (108). The turbine (116) is operatively connected to the compressor (104) to drive the compressor. A turbine cooling air conduit (372) extends from an air inlet of the turbine cooling air conduit (372) to an air outlet (376) of the turbine cooling air conduit (372).",
  "title": "DUAL CYCLE INTERCOOLED ENGINE ARCHITECTURES"
}