{
  "$type": "site.standard.document",
  "description": "An aircraft having a fuel cell () and an air supply device () for supplying air for operating the fuel cell () and for cooling a heat exchanger () connected to the fuel cell (), the aircraft () having at least one air duct () whose cross section widens in the direction of flow () of the air…",
  "path": "/patents/1368782",
  "publishedAt": "2024-09-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/24",
    "MTU Aero Engines AG"
  ],
  "textContent": "An aircraft having a fuel cell () and an air supply device () for supplying air for operating the fuel cell () and for cooling a heat exchanger () connected to the fuel cell (), the aircraft () having at least one air duct () whose cross section widens in the direction of flow () of the air downstream of an air inlet opening () in at least one region () of the peripheral surface. Also provided is a method for operating such a fuel cell () of an aircraft () with an air supply device () for operating the fuel cell () and for cooling a heat exchanger () connected to the fuel cell ().",
  "title": "AIRCRAFT HAVING A FUEL CELL AND METHOD FOR OPERATING A FUEL CELL OF AN AIRCRAFT"
}