{
  "$type": "site.standard.document",
  "description": "A bearing support assembly (14) for supporting a bearing assembly (16) within a bearing compartment (12) of a gas turbine engine (10) includes a centering spring (44) and a bearing support member (42) integrally joined together to form a one-piece structure. The centering spring (44) connects to…",
  "path": "/patents/994647",
  "publishedAt": "2012-12-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/164",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A bearing support assembly (14) for supporting a bearing assembly (16) within a bearing compartment (12) of a gas turbine engine (10) includes a centering spring (44) and a bearing support member (42) integrally joined together to form a one-piece structure. The centering spring (44) connects to the bearing assembly (16) and has a portion (46) that extends conically relative to a centerline axis of the gas turbine engine. The bearing support member (42) extends from the centering spring to connect to an engine case (38) of the gas turbine engine.",
  "title": "Integral bearing support and centering spring assembly for a gas turbine engine"
}