{
  "$type": "site.standard.document",
  "description": "Cooling architecture (30) for a cryogenic and superconducting powertrain (10) using liquid hydrogen on board and method for managing the cooling temperature of the powertrain components. The cooling architecture (30) comprises at least one heat exchanger (36a, 36b) configured to transfer heat from…",
  "path": "/patents/1388615",
  "publishedAt": "2025-06-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L58/33",
    "AIRBUS SAS [FR]"
  ],
  "textContent": "Cooling architecture (30) for a cryogenic and superconducting powertrain (10) using liquid hydrogen on board and method for managing the cooling temperature of the powertrain components. The cooling architecture (30) comprises at least one heat exchanger (36a, 36b) configured to transfer heat from a first fluid to a second fluid. The first fluid of each heat exchanger (36a, 36b) may be liquid hydrogen (H2), and the second fluid of each heat exchanger (36a, 36b) may be gaseous helium (He), liquid Neon or liquid Nitrogen (N2).",
  "title": "COOLING ARCHITECTURE FOR A CRYOGENIC AND SUPERCONDUCTING POWERTRAIN USING LIQUID HYDROGEN ON BOARD AND METHOD FOR MANAGING THE COOLING TEMPERATURE OF THE POWERTRAIN COMPONENTS"
}