{
  "$type": "site.standard.document",
  "description": "An aircraft comprising a plurality of fuel tanks (1-4) in each wing (7) is arranged such that each fuel tank (1-4) is provided with a venting pipe (11-14) connected to a single venting chamber (6). The venting chamber (6) is itself located in a central fuel tank (4) located in the wing centre-box…",
  "path": "/patents/1072849",
  "publishedAt": "2005-11-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D37/14",
    "AIRBUS UK LTD [GB]"
  ],
  "textContent": "An aircraft comprising a plurality of fuel tanks (1-4) in each wing (7) is arranged such that each fuel tank (1-4) is provided with a venting pipe (11-14) connected to a single venting chamber (6). The venting chamber (6) is itself located in a central fuel tank (4) located in the wing centre-box and is thus located inwardly of at least two of the fuel tanks (1-3). The venting chamber (6) has two venting pipes (15, 25) each being connected via a respective surge tank (5) in each wing to the exterior of the aircraft.",
  "title": "Aircraft and fuel venting system therefor"
}