{
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  "description": "A supply system (100) for the energy supply in an aircraft comprising an engine (101) for propelling an aircraft, a fuel cell (102) for supplying an aircraft with electric energy, a first fuel reservoir (103) for supplying the engine (101) with engine fuel and a second fuel reservoir (104) for…",
  "path": "/patents/1015403",
  "publishedAt": "2011-03-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D11/02",
    "AIRBUS GMBH [DE]"
  ],
  "textContent": "A supply system (100) for the energy supply in an aircraft comprising an engine (101) for propelling an aircraft, a fuel cell (102) for supplying an aircraft with electric energy, a first fuel reservoir (103) for supplying the engine (101) with engine fuel and a second fuel reservoir (104) for supplying the fuel cell (102) with fuel cell fuel. The first fuel reservoir (103) is arranged separately of the second fuel reservoir (104).",
  "title": "Supply system and method for energy supply in an aircraft"
}