{
  "$type": "site.standard.document",
  "description": "The nozzle has controlled and follower flaps (14, 16) made up of composite ceramic matrix material. Each flap is formed as a single unit with cylindrical parts (20, 22) on a peripheral sealing joint at its upstream end and with longitudinal edges (30) performing a longitudinal sealing between the…",
  "path": "/patents/1070351",
  "publishedAt": "2006-02-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/12",
    "SNECMA [FR]"
  ],
  "textContent": "The nozzle has controlled and follower flaps (14, 16) made up of composite ceramic matrix material. Each flap is formed as a single unit with cylindrical parts (20, 22) on a peripheral sealing joint at its upstream end and with longitudinal edges (30) performing a longitudinal sealing between the flaps. The flaps have sphere portions (26, 28) at the upstream end, where the portions (26, 28) rotate on upstream ends of adjacent flaps.",
  "title": "Jet engine convergent nozzle"
}