{
  "$type": "site.standard.document",
  "description": "The engine has a sealing unit including an annular segment (50) whose inner radial part (51) is housed in a radially sliding manner and seals a groove. The groove is provided at a periphery of an upstream port of an outer case of a diffuser grid (10). Periphery of the segment is supported by an…",
  "path": "/patents/1079284",
  "publishedAt": "2005-03-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/005",
    "SNECMA MOTEURS [FR]"
  ],
  "textContent": "The engine has a sealing unit including an annular segment (50) whose inner radial part (51) is housed in a radially sliding manner and seals a groove. The groove is provided at a periphery of an upstream port of an outer case of a diffuser grid (10). Periphery of the segment is supported by an inner surface of a sleeve which is integrated with an annular structure and surrounds the segment.",
  "title": "Piston ring type seal for the compressor of a gas turbine"
}