{
  "$type": "site.standard.document",
  "description": "A method of operating a dual fuel gas turbine engine (102) includes operating the engine (102) with a first fuel according to a first control loop (202). The method also includes while the engine (102) is operating with the first fuel, bumplessly transitioning the engine (102) to operate with a…",
  "path": "/patents/965177",
  "publishedAt": "2026-05-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/40",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A method of operating a dual fuel gas turbine engine (102) includes operating the engine (102) with a first fuel according to a first control loop (202). The method also includes while the engine (102) is operating with the first fuel, bumplessly transitioning the engine (102) to operate with a second fuel, and operating the engine (102) with the second fuel according to a second control loop (204).",
  "title": "SWITCHABLE AERO ENGINE DUAL FUEL CONTROL SYSTEM WITH DHFC"
}