{
  "$type": "site.standard.document",
  "description": "A method enables a variable vane assembly (44) for a gas turbine engine to be coupled to an engine casing (50). The variable vane assembly includes a bushing assembly (100) and at least one variable vane (52) that includes a platform (56) and a vane stem (54). The method comprises coupling a first…",
  "path": "/patents/1088723",
  "publishedAt": "2004-03-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/162",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method enables a variable vane assembly (44) for a gas turbine engine to be coupled to an engine casing (50). The variable vane assembly includes a bushing assembly (100) and at least one variable vane (52) that includes a platform (56) and a vane stem (54). The method comprises coupling a first bushing (142) to the engine casing in a press fit, coupling a second bushing (140) to the variable vane, and coupling the variable vane to the engine casing such that at least a portion of the first bushing is between the engine casing and the second bushing, and such that at least a portion of the second bushing is between the first bushing and the vane stem.",
  "title": "Methods and apparatus for sealing gas turbine engine variable vane assemblies"
}