{
  "$type": "site.standard.document",
  "description": "A system (10) and method for warming a fuel cell (20) on an aircraft, the system includes at least one fuel cell (20). The fuel cell (20) includes an anode and a cathode for creating thermal and electrical energy. A temperature sensor (44) measures a first temperature of the fuel cell (20). A…",
  "path": "/patents/982415",
  "publishedAt": "2013-10-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D41/00",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A system (10) and method for warming a fuel cell (20) on an aircraft, the system includes at least one fuel cell (20). The fuel cell (20) includes an anode and a cathode for creating thermal and electrical energy. A temperature sensor (44) measures a first temperature of the fuel cell (20). A control unit (50) is coupled to the temperature sensor (44). The control unit (50) increases the first temperature to a second temperature in response to the first temperature being at least equal to a selected temperature threshold. Increasing of the first temperature is indicative of the control unit (50) operating in a warming mode. The second temperature is higher than the selected temperature threshold.",
  "title": "Warming feature for aircraft fuel cells"
}