{
  "$type": "site.standard.document",
  "description": "A method of assembling a gas turbine engine (10) that includes rotatably coupling a first low-pressure turbine rotor (106) to a high-pressure turbine (100), rotatably coupling a second low pressure turbine rotor (108) to the first low-pressure turbine rotor, and rotatably coupling the second…",
  "path": "/patents/1067721",
  "publishedAt": "2006-05-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D1/24",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method of assembling a gas turbine engine (10) that includes rotatably coupling a first low-pressure turbine rotor (106) to a high-pressure turbine (100), rotatably coupling a second low pressure turbine rotor (108) to the first low-pressure turbine rotor, and rotatably coupling the second low-pressure turbine rotor to a turbine rear-frame (142) such that a weight of the high-pressure turbine is transmitted to the turbine rear-frame.",
  "title": "Gas turbine engine"
}