{
  "$type": "site.standard.document",
  "description": "An axial divergent section slot nozzle (10) for an engine is provided. The nozzle has a plurality of spaced apart divergent flaps (12), at least one device for moving the divergent flaps (12) to change a cross sectional area of the nozzle in a throat region, and a bridge member (20) positioned…",
  "path": "/patents/1073679",
  "publishedAt": "2005-09-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "A47J27/64",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "An axial divergent section slot nozzle (10) for an engine is provided. The nozzle has a plurality of spaced apart divergent flaps (12), at least one device for moving the divergent flaps (12) to change a cross sectional area of the nozzle in a throat region, and a bridge member (20) positioned intermediate adjacent ones of the flaps (12). The bridge member (20) includes a bridge bracket (216) and a sealing element (204) joined to the bridge bracket (216). The sealing element (204) has an upper surface (226). The bridge bracket (216) has a lower surface (222,224) which diverges from the upper surface (226) of the sealing element (204). In a preferred embodiment of the present invention, the bridge bracket (216) has a shape which allows variable slot size depending on nozzle throat jet area.",
  "title": "Axial divergent section slot nozzle"
}