{
  "$type": "site.standard.document",
  "description": "A method for assembling a gas turbine engine (10) that includes providing a low-pressure turbine inner rotor (120) that includes a first plurality of turbine blade rows (124) configured to rotate in a first direction, providing a low-pressure turbine outer rotor (110) that includes a second…",
  "path": "/patents/1067594",
  "publishedAt": "2006-05-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/162",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method for assembling a gas turbine engine (10) that includes providing a low-pressure turbine inner rotor (120) that includes a first plurality of turbine blade rows (124) configured to rotate in a first direction, providing a low-pressure turbine outer rotor (110) that includes a second plurality of turbine blade rows (114) configured to rotate in a second direction that is opposite the first direction, coupling a turbine mid-frame assembly (150) including a plurality of spokes within the engine such that the spokes are spaced axially forward of the inner rotor, coupling a bearing (140) between the turbine mid-frame assembly and the inner rotor such that the inner rotor is rotatably coupled to the turbine mid-frame, and adjusting the plurality of spokes to align the bearing in a radial direction.",
  "title": "Gas turbine engine and method of assembling same"
}