{
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"description": "A fuel delivery system for a gas turbine engine (103) comprises a cryogenic fuel tank (104), a first fuel line (601) for connection to the cryogenic fuel tank (104), a fuel pump (301) connected to receive fuel via the first fuel line (601), a plurality of fuel lines (602-606) connecting the fuel…",
"path": "/patents/1400825",
"publishedAt": "2023-11-01T00:00:00.000Z",
"site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
"tags": [
"B64D37/32",
"ROLLS ROYCE PLC [GB]"
],
"textContent": "A fuel delivery system for a gas turbine engine (103) comprises a cryogenic fuel tank (104), a first fuel line (601) for connection to the cryogenic fuel tank (104), a fuel pump (301) connected to receive fuel via the first fuel line (601), a plurality of fuel lines (602-606) connecting the fuel pump to a combustor (207) of the gas turbine engine (103), a controller (613) configured to operate the fuel delivery system, a purge gas tank (611) connected to the first fuel line (601) and configured to store a purge gas for purging the plurality of fuel lines (602-606) and a fuel gas tank (612) connected to the first fuel line (601) and configured to store a fuel gas for flushing purge gas from the plurality of fuel lines (602-606).",
"title": "FUEL DELIVERY SYSTEM"
}