{
  "$type": "site.standard.document",
  "description": "A method for assembling a gas turbine engine assembly, including a gas turbine engine (10), a power turbine coupled to the gas turbine engine, and a thrust bearing coupled to the power turbine. The method includes coupling a first annular portion (110) having a first radius (112) to the power…",
  "path": "/patents/1066451",
  "publishedAt": "2006-06-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/164",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method for assembling a gas turbine engine assembly, including a gas turbine engine (10), a power turbine coupled to the gas turbine engine, and a thrust bearing coupled to the power turbine. The method includes coupling a first annular portion (110) having a first radius (112) to the power turbine, coupling a second annular portion (114) having a second radius (116) to the thrust bearing, wherein the first radius is different than the second radius, and coupling a plurality of structural members (120) between the first and second portions such that the thrust assembly has a substantially frusto-conical shape.",
  "title": "Thrust bearing assembly for a gas turbine engine"
}