{
  "$type": "site.standard.document",
  "description": "A fuel system for a gas turbine engine comprising a regenerative pump (11) having an inlet (13), an outlet (14), and a flow channel (17) extending between the inlet and the outlet along which fuel is transferred in use by rotation of an impeller (15) of the regenerative pump, a fuel supply line…",
  "path": "/patents/1096248",
  "publishedAt": "2003-05-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "GOODRICH CONTROL SYS LTD [GB]"
  ],
  "textContent": "A fuel system for a gas turbine engine comprising a regenerative pump (11) having an inlet (13), an outlet (14), and a flow channel (17) extending between the inlet and the outlet along which fuel is transferred in use by rotation of an impeller (15) of the regenerative pump, a fuel supply line (18) in use supplying fuel at low pressure to said pump inlet (13), an output line (21) in use receiving fuel at high pressure from said pump outlet (14) for distribution to a gas turbine engine (24), and, a spill line (25) into which fuel from said pump outlet (14) can be spilled, said spill line (25) being connected to said flow channel (17) of said regenerative pump (11) at a selected point between the inlet (13) and outlet (14) of said pump (11) to discharge spilled fuel in use into said flow channel (17).",
  "title": "Regenerative fuel pump system"
}