{
  "$type": "site.standard.document",
  "description": "A flexible seal system (16) for a gas turbine engine (10) includes an annular mounting bracket (92), an annular support bracket (96), an annular flexible seal (40) and a plurality of mounting spacers (100). The flexible seal (40) extends axially between a first mounting segment (56) and a second…",
  "path": "/patents/990517",
  "publishedAt": "2013-05-22T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/28",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A flexible seal system (16) for a gas turbine engine (10) includes an annular mounting bracket (92), an annular support bracket (96), an annular flexible seal (40) and a plurality of mounting spacers (100). The flexible seal (40) extends axially between a first mounting segment (56) and a second mounting segment (58). The first mounting segment (56) is connected axially between the mounting bracket (92) and the support bracket (96), and includes a plurality of mounting apertures (68) that extend axially through the first mounting segment (56). Each of the mounting spacers (100) is arranged within a respective one of the mounting apertures (68), and extends axially between the mounting bracket (92) and the support bracket (96).",
  "title": "Flexible seal system for a gas turbine engine"
}