{
  "$type": "site.standard.document",
  "description": "The method involves determining a value illustrating a thermo-mechanical condition (ET) of a turbine engine to illustrate expansion of an element of the engine based on thermal conditions, from measurement of exhaust or turbine gas temperature (T). The determined value is compared with threshold…",
  "path": "/patents/995131",
  "publishedAt": "2012-12-12T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/003",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The method involves determining a value illustrating a thermo-mechanical condition (ET) of a turbine engine to illustrate expansion of an element of the engine based on thermal conditions, from measurement of exhaust or turbine gas temperature (T). The determined value is compared with threshold values (S1, S2). Indications (I1-I3) relating to operation of the engine are displayed based on comparison result by a displaying unit on a viewing screen of an aircraft cockpit, where the indications relate to a damage risk for the engine, a lock risk for the engine and/or an operational procedure. Independent claims are also included for the following: (1) a device for providing assistance to automatically monitor a turbine engine of an aircraft (2) an aircraft system for an aircraft provided with a set of turbine engines.",
  "title": "Method and device for assisted monitoring of an aircraft turbine engine."
}