{
  "$type": "site.standard.document",
  "description": "There is provided a fuel system (1) for an aircraft. The fuel system comprises a fuel tank (10) for storing fuel (102) during operation of the aircraft and a diffuser (11) disposed inside the fuel tank (10). The diffuser is configured such that it forms part of a flow path configured to connect a…",
  "path": "/patents/1410125",
  "publishedAt": "2024-10-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60K15/03",
    "AIRBUS OPERATIONS LTD [GB]"
  ],
  "textContent": "There is provided a fuel system (1) for an aircraft. The fuel system comprises a fuel tank (10) for storing fuel (102) during operation of the aircraft and a diffuser (11) disposed inside the fuel tank (10). The diffuser is configured such that it forms part of a flow path configured to connect a fuel source to the inside of the fuel tank. The diffuser (11) comprises a wall (111) which at least partially defines an internal space (113) of the diffuser; an opening (13) in the wall (111), which provides access to the internal space; and a blocking component (12a) configured to block the opening (13).",
  "title": "FUEL TANK DIFFUSER"
}