{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10; 100) having: an engine core having, in serial flow communication, a low-pressure compressor (12a), a high-pressure compressor (14a), a high-pressure turbine (14b) drivingly connected to the high-pressure compressor (14a), and a low-pressure turbine (12b) drivingly…",
  "path": "/patents/1419405",
  "publishedAt": "2024-08-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/04",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A gas turbine engine (10; 100) having: an engine core having, in serial flow communication, a low-pressure compressor (12a), a high-pressure compressor (14a), a high-pressure turbine (14b) drivingly connected to the high-pressure compressor (14a), and a low-pressure turbine (12b) drivingly connected to an output shaft (18); and a clutch (40; 140) having a disengaged configuration in which the low-pressure turbine (12b) is drivingly disconnected from the low-pressure compressor (12a) such that, in the disengaged configuration, the clutch (40; 140) disengages the low-pressure turbine (12b) from the low-pressure compressor (12a), and an engaged configuration in which the low-pressure turbine (12b) is drivingly connected to the low-pressure compressor (12a), the low-pressure turbine (12b) drivingly connected to the output shaft (18) in both of the engaged and disengaged configurations of the clutch (40; 140).",
  "title": "GAS TURBINE ENGINE WITH CLUTCH SYSTEM"
}