A method for controlling a pressure control mechanism in a turbofan engine having a precooler permitting heat exchange between ambient air and bleed air includes detecting at least one of an engine failure or a bleed system failure, detecting at least one of an ice condition or an activation of an anti-ice system, and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air.
CONTROL METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT AND AIRCRAFT ENGINE
REGELVERFAHREN ZUM BETRIEB EINES VORKÜHLERS IN EINEM FLUGZEUG UND FLUGZEUGTRIEBWERK
PROCÉDÉ POUR FAIRE FONCTIONNER UN PRÉREFROIDISSEUR DANS UN AÉRONEF ET MOTEUR AÉRONEF
2022-02-09
Patent
Elektronische Ressource
Englisch
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT
Europäisches Patentamt | 2017
|CONTROL SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT
Europäisches Patentamt | 2018
|System and method for operating a precooler in an aircraft
Europäisches Patentamt | 2017
|Novel high-temperature precooler for aircraft environmental control system
Europäisches Patentamt | 2020
|Aircraft turbomachine comprising a heat exchanger of the precooler type
Europäisches Patentamt | 2021
|