{
  "$type": "site.standard.document",
  "description": "A bearing system (38A) for a gas turbine engine includes a spring (62) defined about an axis of rotation. The spring (62) has a multiple of beams (82) which extend between a flange structure (84) and an attachment structure (86). A damper (64) is defined about the axis of rotation and mounted to…",
  "path": "/patents/999998",
  "publishedAt": "2012-07-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/164",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A bearing system (38A) for a gas turbine engine includes a spring (62) defined about an axis of rotation. The spring (62) has a multiple of beams (82) which extend between a flange structure (84) and an attachment structure (86). A damper (64) is defined about the axis of rotation and mounted to the spring (62) to at least partially axially overlap the multiple of beams (82).",
  "title": "Bearing System for Gas Turbine Engine"
}