{
  "$type": "site.standard.document",
  "description": "A fuel system (200) for a hydrogen fuelled aircraft propulsion system (103) comprises a tank (104) configured to store hydrogen, a first inductor (436a-c) provided within the tank (104) and configured to heat hydrogen fuel within the tank (104), and a second inductor (432a-c) provided externally to…",
  "path": "/patents/1386502",
  "publishedAt": "2025-11-19T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D37/10",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A fuel system (200) for a hydrogen fuelled aircraft propulsion system (103) comprises a tank (104) configured to store hydrogen, a first inductor (436a-c) provided within the tank (104) and configured to heat hydrogen fuel within the tank (104), and a second inductor (432a-c) provided externally to the tank (104), and configured to induce a current in the first inductor (436a-c).",
  "title": "GAS TURBINE ENGINE"
}