{
  "$type": "site.standard.document",
  "description": "The invention provides improved measures for monitoring and manufacturing tanks for cryogenic liquids. It is proposed that the tank (22) is manufactured in a way that signal and power lines from a control unit (38) to sensors (34) of the cryogenic tank (22) are integrated with the tank walls (24…",
  "path": "/patents/1397513",
  "publishedAt": "2025-12-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D37/04",
    "AIRBUS SAS [FR]"
  ],
  "textContent": "The invention provides improved measures for monitoring and manufacturing tanks for cryogenic liquids. It is proposed that the tank (22) is manufactured in a way that signal and power lines from a control unit (38) to sensors (34) of the cryogenic tank (22) are integrated with the tank walls (24, 26). The conductive track structure (32) so formed has a layer structure (47) that uses the naturally oc-curing or artificially generated insulating layer (48) on the tank wall material as a substrate on top of which conductive paths (32a-d) are formed that connect the sensors (34) to the control unit (38).",
  "title": "CRYOGENIC LIQUID TANK FOR AN AIRCRAFT AND METHOD FOR MANUFACTURING THE SAME"
}