{
  "$type": "site.standard.document",
  "description": "A heat management system (100) includes a fuel tank (110) storing a fuel (111); a first heat exchanger (120) thermally coupled to the fuel tank (110); a hydraulic pump (130) for circulating a hydraulic fluid (131); a hydraulic circuit (140) including first and second hydraulic lines (141, 142)…",
  "path": "/patents/1393169",
  "publishedAt": "2025-01-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/10",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A heat management system (100) includes a fuel tank (110) storing a fuel (111); a first heat exchanger (120) thermally coupled to the fuel tank (110); a hydraulic pump (130) for circulating a hydraulic fluid (131); a hydraulic circuit (140) including first and second hydraulic lines (141, 142) fluidly coupled to the first heat exchanger (120) and the hydraulic pump (130), such that the first heat exchanger (120) brings the hydraulic fluid (131) and the fuel (111) into a heat exchange relationship; an oil circuit (150); and a second heat exchanger (170) thermally coupled to the oil circuit (150) and at least one of the first and second hydraulic lines (141, 142), such that the second heat exchanger (170) brings the hydraulic fluid (131) and the oil (151) into a heat exchange relationship, thereby allowing heat transfer between the fuel (111) and the oil (151) via the hydraulic fluid (131).",
  "title": "HEAT MANAGEMENT SYSTEM FOR AIRCRAFT"
}