{
  "$type": "site.standard.document",
  "description": "The invention relates to an aircraft comprising a structure (202) comprising a leakproof tank (210) delimited by walls, of which at least one is in contact with the air outside the aircraft, and filled partly with a two-phase heat-transfer fluid, a fuel cell (102) that is passed through by a…",
  "path": "/patents/1408505",
  "publishedAt": "2025-04-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C1/061",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The invention relates to an aircraft comprising a structure (202) comprising a leakproof tank (210) delimited by walls, of which at least one is in contact with the air outside the aircraft, and filled partly with a two-phase heat-transfer fluid, a fuel cell (102) that is passed through by a heat-transfer fluid, and a line (106) which takes the heat-transfer fluid at an output of the fuel cell (102) and which reintroduces this heat-transfer fluid at an input of the fuel cell (102). The line (106) passes through the leakproof tank (210) immersed in the heat-transfer fluid in liquid phase. [0002] Such an installation avoids having to install a heat exchanger of large dimensions.",
  "title": "AIRCRAFT WITH A FUEL CELL AND A STRUCTURE HAVING A TANK CONTAINING A HEAT-TRANSFER FLUID ENSURING THE COOLING OF THE FUEL CELL"
}