{
  "$type": "site.standard.document",
  "description": "A gas turbine engine nozzle (14) includes a flap (18) movable relative to a structure (20). A seal assembly (22) is supported by one of the structure (20) and the flap (18) and includes a seal (26) hinged about an axis. The seal (26) has a sealing profile engaging a seal land of the other of the…",
  "path": "/patents/992611",
  "publishedAt": "2013-02-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/005",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine nozzle (14) includes a flap (18) movable relative to a structure (20). A seal assembly (22) is supported by one of the structure (20) and the flap (18) and includes a seal (26) hinged about an axis. The seal (26) has a sealing profile engaging a seal land of the other of the structure (20) and the flap (18). A biasing member (36) is configured to urge the hinged seal (26) toward the seal land.",
  "title": "Flap seal for gas turbine engine movable nozzle flap"
}