Aircraft engine control during icing of temperature probe
Aircraft engine control during icing of temperature probe
- New search for: CALANDRA SALVATORE
- New search for: GIROUX FREDERIC
- New search for: IACOBACCI MARK
- New search for: CHABOT MARTIN
- New search for: HARTROPP SIMON
- New search for: SYED YUSUF
- New search for: CHMIEL DARIUSZ
- New search for: BAJAJ ADRIENNE
- New search for: CALANDRA SALVATORE
- New search for: GIROUX FREDERIC
- New search for: IACOBACCI MARK
- New search for: CHABOT MARTIN
- New search for: HARTROPP SIMON
- New search for: SYED YUSUF
- New search for: CHMIEL DARIUSZ
- New search for: BAJAJ ADRIENNE
Methods for controlling an aircraft turbofan engine during icing of a temperature probe and devices for carrying out such methods are described. The methods may comprise: using one or more signals representative of temperature received from a heated temperature probe to generate one or more control signals for use in controlling the engine; determining that an icing condition associated with the probe exists; and using data representing one or more substitute signals in place of signals representative of temperature received from the heated temperature probe to generate the one or more control signals for use in controlling the engine.
Document information
Aircraft engine control during icing of temperature probe
2015-08-25
Patent
Electronic Resource
English
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen / G01K MEASURING TEMPERATURE , Messen der Temperatur / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte |
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