{
  "$type": "site.standard.document",
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  "description": "A gas turbine engine (100) includes a primary gas path (1060 having, in fluid series communication: an air inlet (112), a compressor section (104) fluidly connected to the air inlet, a combustor section (108) fluidly connected to an outlet of the compressor, and a turbine section (116) fluidly…",
  "path": "/patents/1404256",
  "publishedAt": "2025-04-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/20",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A gas turbine engine (100) includes a primary gas path (1060 having, in fluid series communication: an air inlet (112), a compressor section (104) fluidly connected to the air inlet, a combustor section (108) fluidly connected to an outlet of the compressor, and a turbine section (116) fluidly connected to an outlet of the combustor section. The gas turbine engine includes a heat exchanger (122) having a gas conduit (126) fluidly connected to the primary gas path, and a fluid conduit (128) in fluid isolation from, and in thermal communication with, the gas conduit. A hydrogen expansion turbine (134) receives hydrogen from the gas conduit of the heat exchanger.",
  "title": "DUAL CYCLE INTERCOOLED HYDROGEN ENGINE ARCHITECTURE"
}