{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10) includes an intercooling turbine section (24A) to at least partially drive one of a low spool (42') and a high spool (46'). An intercooling turbine section bypass is provided to selectively bypass at least a portion of a core flow (60) through an intercooling turbine…",
  "path": "/patents/991233",
  "publishedAt": "2013-05-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/143",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine (10) includes an intercooling turbine section (24A) to at least partially drive one of a low spool (42') and a high spool (46'). An intercooling turbine section bypass is provided to selectively bypass at least a portion of a core flow (60) through an intercooling turbine section bypass path (112) around the intercooling turbine section (24A).",
  "title": "Gas turbine engine with intercooling turbine section and intercooling turbine section bypass"
}