{
  "$type": "site.standard.document",
  "description": "A fuel supply system (10) for a gas turbine engine includes a fuel tank (12), a pumping unit (18) downstream of the fuel tank (12) and configured to receive fuel from the fuel tank (12), and a sharing valve (24) downstream of the pumping unit (18) and configured to receive fuel from the cruise pump…",
  "path": "/patents/1419846",
  "publishedAt": "2023-05-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/232",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A fuel supply system (10) for a gas turbine engine includes a fuel tank (12), a pumping unit (18) downstream of the fuel tank (12) and configured to receive fuel from the fuel tank (12), and a sharing valve (24) downstream of the pumping unit (18) and configured to receive fuel from the cruise pump (36) of the pumping unit (18) during a first operating condition. The pumping unit (18) includes a boost pump (34), an actuation pump (38) downstream of the boost pump (34) and in fluid communication with at least one actuator of the gas turbine engine, and a cruise pump (36) downstream of the boost pump (34) and in fluid communication with nozzles of a gas generator of the gas turbine engine.",
  "title": "DUAL PUMP UNIT WITH BOOST PUMP"
}