{
  "$type": "site.standard.document",
  "description": "A fuel control system (200) for an aircraft engine (100), comprises a fuel feed conduit (122) including an inlet end (126) and an outlet end (128). A fuel metering mechanism (146) is disposed in the fuel feed conduit (122) between the inlet end (126) and the outlet end (128) operable to regulate…",
  "path": "/patents/1402712",
  "publishedAt": "2025-03-19T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A fuel control system (200) for an aircraft engine (100), comprises a fuel feed conduit (122) including an inlet end (126) and an outlet end (128). A fuel metering mechanism (146) is disposed in the fuel feed conduit (122) between the inlet end (126) and the outlet end (128) operable to regulate flow through the fuel feed conduit (122). A position feedback sensor (148) is operatively connected to the fuel metering mechanism (146) and operable to generate a signal indicative of a position of the fuel metering mechanism (146).",
  "title": "CONTROLLING GASEOUS FUEL FLOW IN AN AIRCRAFT ENGINE"
}