{
  "$type": "site.standard.document",
  "description": "The engine has a crankcase whose outer shell is fixed to an annular structure (7) by a joint with brush (50) fixed to a periphery of an upstream part of an outer case (12) of a diffuser grid (10). The joint has radially extending bristles (52) supported on an inner surface (54) of a cylindrical…",
  "path": "/patents/1079105",
  "publishedAt": "2005-03-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/005",
    "SNECMA MOTEURS [FR]"
  ],
  "textContent": "The engine has a crankcase whose outer shell is fixed to an annular structure (7) by a joint with brush (50) fixed to a periphery of an upstream part of an outer case (12) of a diffuser grid (10). The joint has radially extending bristles (52) supported on an inner surface (54) of a cylindrical sleeve (53). The sleeve integrated to the structure that is connected to an outer shell (6) of a compressor (1), surrounds the joint.",
  "title": "Gas turbine brush seal arrangement for cabin air supply"
}