{
  "$type": "site.standard.document",
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  "description": "A computer-implemented method includes determining a thrust requirement to satisfy a desired glide slope and determining, based on the thrust requirement, whether thrust matching can be maintained while operating a first gas turbine engine in a fuel-burning mode and operating a second gas turbine…",
  "path": "/patents/1400268",
  "publishedAt": "2025-07-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/262",
    "RTX CORP [US]"
  ],
  "textContent": "A computer-implemented method includes determining a thrust requirement to satisfy a desired glide slope and determining, based on the thrust requirement, whether thrust matching can be maintained while operating a first gas turbine engine in a fuel-burning mode and operating a second gas turbine engine in an electrically powered mode. The method further includes, responsive to determining that thrust matching cannot be maintained, commanding fuel flow to a combustor of the second engine to cause the second gas turbine engine to operate in the fuel-burning mode.",
  "title": "HYBRID ELECTRIC SINGLE ENGINE DESCENT MODE ACTIVATION LOGIC"
}