{
  "$type": "site.standard.document",
  "description": "A method of operating an aircraft engine (10, 100) of an aircraft, the aircraft engine (10, 100) having a common-rail fuel injection system (102) for injecting fuel into a combustion chamber (32) of the aircraft engine (10, 100), including: pressurizing fuel for circulation through the common-rail…",
  "path": "/patents/1425737",
  "publishedAt": "2025-03-19T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01C1/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A method of operating an aircraft engine (10, 100) of an aircraft, the aircraft engine (10, 100) having a common-rail fuel injection system (102) for injecting fuel into a combustion chamber (32) of the aircraft engine (10, 100), including: pressurizing fuel for circulation through the common-rail injection system (102); circulating a portion of the pressurized fuel through a motive flow inlet (116a) of an ejector pump (116); and entraining a flow through the ejector pump (116) with the portion of the pressurized fuel circulating through the motive flow inlet (116a).",
  "title": "AIRCRAFT ENGINE HAVING A COMMON-RAIL FUEL SYSTEM WITH EJECTOR PUMP AND METHOD OF OPERATING AN AIRCRAFT ENGINE"
}