{
  "$type": "site.standard.document",
  "description": "The device has an annular tubular element (31) extended along a circumferential direction. The tubular element comprises outflow openings for supplying hot air to a ring lip region (29) of a double-walled nacelle (30) for removing snow and ice. The tube element is formed with pipe segments along…",
  "path": "/patents/995653",
  "publishedAt": "2012-11-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D15/04",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "The device has an annular tubular element (31) extended along a circumferential direction. The tubular element comprises outflow openings for supplying hot air to a ring lip region (29) of a double-walled nacelle (30) for removing snow and ice. The tube element is formed with pipe segments along the circumferential direction, where the pipe segments are fastenable relative to each other. The pipe segments are coupled with one another by plug connections. The pipe segments are centrally supported at the nacelle by a bearing support part i.e. metal sheet bending part.",
  "title": "De-icing device for an aviation gas turbine engine"
}