{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
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  "description": "Disclosed is an ice protection system (140) for an aerodynamic surface of an aircraft, a surface having a flow facing side and an inwardly facing side that opposes the flow facing side, the system having: a perforated sheet (170) configured for disposal in the surface; a heating source connected to…",
  "path": "/patents/1409454",
  "publishedAt": "2024-03-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D15/00",
    "GOODRICH CORP [US]"
  ],
  "textContent": "Disclosed is an ice protection system (140) for an aerodynamic surface of an aircraft, a surface having a flow facing side and an inwardly facing side that opposes the flow facing side, the system having: a perforated sheet (170) configured for disposal in the surface; a heating source connected to the perforated sheet; and a suction source (160) disposed to draw ice melted by the heating source (150) through the perforated sheet (170) and heating source.",
  "title": "ICE PROTECTION SYSTEM FOR A COMPONENT OF AN AERODYNAMIC SYSTEM"
}