{
  "$type": "site.standard.document",
  "description": "The jet engine has a sealing system for insulating a cavity from a vein of primary flow. The system has a joint (50) mounted at periphery of an upstream portion (12a) of an external case (12) of a diffuser grid. Blades of the joint (50) are in support on a free end of a spoiler (71). Another joint…",
  "path": "/patents/1079092",
  "publishedAt": "2005-03-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/005",
    "SNECMA MOTEURS [FR]"
  ],
  "textContent": "The jet engine has a sealing system for insulating a cavity from a vein of primary flow. The system has a joint (50) mounted at periphery of an upstream portion (12a) of an external case (12) of a diffuser grid. Blades of the joint (50) are in support on a free end of a spoiler (71). Another joint (60) is situated upstream of the joint (50), and whose blades are in support on an upstream end of a spoiler (72) and on a spoiler (76).",
  "title": "Gas turbine sealing joint having lamellar structure"
}