{
  "$type": "site.standard.document",
  "description": "In accordance with at least one aspect of this disclosure, there is provided a fuel control system for gaseous fuel in an aircraft (1). The system includes a control module (144) operatively connected to a metering device (146) in a fuel flow conduit (122), the control module (144) operable to…",
  "path": "/patents/1402379",
  "publishedAt": "2025-11-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "In accordance with at least one aspect of this disclosure, there is provided a fuel control system for gaseous fuel in an aircraft (1). The system includes a control module (144) operatively connected to a metering device (146) in a fuel flow conduit (122), the control module (144) operable to control the flow of fuel through the fuel flow conduit (122). The control module (144) includes an input line (148) operable to receive a command input (150) indicative of a requested engine state. In embodiments, the control module (144) includes a compressibility logic and machine readable instructions. The machine readable instruction can be configured to cause the control module (144) to control the metering device (146) to achieve the requested engine state based on a compressibility factor input from the compressibility logic.",
  "title": "TRANSIENT GASEOUS FUEL FLOW SCHEDULING"
}