{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "There is provided a fuel management system (500A) for a gas turbine engine (10), the fuel management system (500A) comprising a fuel supply line (510) configured to supply fuel from a system inlet (520) to a combustor (16) of the gas turbine engine via a combustor pump (530) and combustor valve…",
  "path": "/patents/1397351",
  "publishedAt": "2025-08-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/224",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "There is provided a fuel management system (500A) for a gas turbine engine (10), the fuel management system (500A) comprising a fuel supply line (510) configured to supply fuel from a system inlet (520) to a combustor (16) of the gas turbine engine via a combustor pump (530) and combustor valve (550). A heat exchanger (540) is configured to reject heat from a thermal load (44) of the gas turbine engine (10) to fuel in the fuel supply line (510) between the system inlet (520) and the combustor valve (550). There is a downstream recirculation line (511) configured to recirculate a downstream excess portion of fuel from the fuel supply line (510), the downstream recirculation line (511) extending from a downstream recirculation point (512) on the fuel supply line (510) between the heat exchanger (540) and the combustor valve (550).",
  "title": "FUEL MANAGEMENT SYSTEM"
}