{
  "$type": "site.standard.document",
  "description": "The present disclosure relates to a gas turbine engine and to a method of controlling a net thrust load on a thrust bearing. The gas turbine engine (20) includes a first non-contacting dynamic rotor seal (84A, 84B, 84C) interfaced with a spool (32), the first non-contacting dynamic seal (84A, 84B…",
  "path": "/patents/985492",
  "publishedAt": "2013-03-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/025",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "The present disclosure relates to a gas turbine engine and to a method of controlling a net thrust load on a thrust bearing. The gas turbine engine (20) includes a first non-contacting dynamic rotor seal (84A, 84B, 84C) interfaced with a spool (32), the first non-contacting dynamic seal (84A, 84B, 84C) operates to seal adjacent to an outer diameter and a second non-contacting dynamic rotor seal (86) with respect to the spool, the second non-contacting dynamic seal (86) operates to seal adjacent to an inner diameter.",
  "title": "THRUST BEARING SYSTEM WITH INVERTED NON-CONTACTING DYNAMIC SEALS FOR GAS TURBINE ENGINE"
}