{
  "$type": "site.standard.document",
  "description": "A method and a system for synthesizing thrust from a turbofan engine (100) are provided. The turbofan engine (100) comprising a compressor section (14), a combustor (16), and a turbine section (18) in serial fluid flow communication. The engine is operated and, during the operating of the turbofan…",
  "path": "/patents/1399299",
  "publishedAt": "2025-04-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/04",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A method and a system for synthesizing thrust from a turbofan engine (100) are provided. The turbofan engine (100) comprising a compressor section (14), a combustor (16), and a turbine section (18) in serial fluid flow communication. The engine is operated and, during the operating of the turbofan engine (100), a pressure of fluid at an exit of the compressor section (14) and a temperature of fluid at a location upstream of the exit of the compressor section (14) are determined. A synthesized value of thrust from the turbofan engine (100) is determined based on a product of at least a first factor and a second factor, the first factor being a function of the pressure and the second factor being a function of the temperature. The synthesized value of thrust from the turbofan engine (100) is output.",
  "title": "SYSTEM AND METHOD FOR SYNTHESIZING THRUST FROM A TURBOFAN ENGINE"
}