{
  "$type": "site.standard.document",
  "description": "An aircraft cooling system comprises a first loop (100) intended to cool fuel cells (110) and on which is present a dynamic air heat exchanger (120), and a second loop (200) intended to cool power electronic equipment (210) and to supply heat to an evaporator (230) to vaporize dihydrogen in order…",
  "path": "/patents/1387858",
  "publishedAt": "2025-07-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L58/33",
    "AIRBUS SAS [FR]"
  ],
  "textContent": "An aircraft cooling system comprises a first loop (100) intended to cool fuel cells (110) and on which is present a dynamic air heat exchanger (120), and a second loop (200) intended to cool power electronic equipment (210) and to supply heat to an evaporator (230) to vaporize dihydrogen in order to supply the fuel cells (110). The first loop (100) and the second loop (200) are interconnected by a flow line (301) starting at the outlet of the dynamic air heat exchanger (120) and by a return line (302). A controller (300) regulates the temperature of cooling liquid in the first loop (100), as well as in the second loop (200) by controlling the opening of the flow line (200). The temperature of the power electronic equipment (210) is regulated with limited impact on the aircraft drag.",
  "title": "COOLING SYSTEM FOR AN AIRCRAFT",
  "updatedAt": "2026-06-14T15:41:05.554Z"
}