{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
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    "mimeType": "image/png",
    "size": 87222
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  "description": "The arrangement has shells (1-3) connected with one another in a circumferential direction (U) and arranged adjacent to each other in an axial direction (A). The shells comprise V or U-shaped cross sections opened opposite to a through flow direction and/or thread axis inclined opposite to the…",
  "path": "/patents/988313",
  "publishedAt": "2013-07-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/08",
    "MTU AERO ENGINES GMBH [DE]"
  ],
  "textContent": "The arrangement has shells (1-3) connected with one another in a circumferential direction (U) and arranged adjacent to each other in an axial direction (A). The shells comprise V or U-shaped cross sections opened opposite to a through flow direction and/or thread axis inclined opposite to the through flow direction. The cross sections are constant over the entire length of the shells, and the arrangement is arranged at a rotor and/or stator of a turbomachine. The thread axis is inclined at an angle to a radial direction (R), where the angle amounts to preferably 50 degrees. An independent claim is also included for a method for manufacturing a sealing arrangement.",
  "title": "Flow engine seal assembly"
}