{
  "$type": "site.standard.document",
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  "description": "A gas turbine engine system 100 comprises a hydrogen-burning gas turbine engine and a fuel system comprising (i) a fuel line 114 arranged to receive gaseous hydrogen at an input 115 thereof and provide the gaseous hydrogen to combustion apparatus 106 of the hydrogen-burning gas turbine engine and…",
  "path": "/patents/1396874",
  "publishedAt": "2025-06-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/22",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A gas turbine engine system 100 comprises a hydrogen-burning gas turbine engine and a fuel system comprising (i) a fuel line 114 arranged to receive gaseous hydrogen at an input 115 thereof and provide the gaseous hydrogen to combustion apparatus 106 of the hydrogen-burning gas turbine engine and (ii) a vent line 116 including a vent valve 104 and having a first end coupled to the fuel line and a second end disposed remotely from the hydrogen-burning gas turbine engine. A controller 112 is arranged to switch the vent valve from a closed state to an open state upon detection of an engine shaft-break or similar condition, thus providing rapid evacuation of gaseous hydrogen from the fuel line and hence rapid shut-down of the engine. The engine may be shut down more rapidly than is possible by means of a shut-off valve within the fuel line.",
  "title": "GAS TURBINE ENGINE SYSTEM"
}