{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (20) according to an exemplary aspect of the present disclosure includes, among other things, a shaft (74) configured to rotate during operation of the gas turbine engine (20), and a squeeze film damper (60') radially outside the shaft (74). The squeeze film damper (60)…",
  "path": "/patents/1420113",
  "publishedAt": "2024-02-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/164",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine (20) according to an exemplary aspect of the present disclosure includes, among other things, a shaft (74) configured to rotate during operation of the gas turbine engine (20), and a squeeze film damper (60') radially outside the shaft (74). The squeeze film damper (60) includes a cavity (62') including a film of lubricant axially between first and second cavity seals (84, 86), and further includes a reservoir (70') fluidly coupled to the cavity (62'). A method is also disclosed.",
  "title": "GAS TURBINE ENGINE INCLUDING SQUEEZE FILM DAMPER WITH RESERVOIR"
}