An integrated electronic engine control and environmental control system bleed control apparatus for use with an aircraft engine. The apparatus comprises an electronic engine controller (18), an environmental control system bleed controller (30) for controlling a flow of bleed air from the aircraft engine (12) to an environmental control system (28) located in an aircraft fuselage (14), and a housing (34) for mounting on or near the aircraft engine (12). The housing (34) contains both the electronic engine controller (18) and the environmental control system bleed controller (30).
Integrated bleed and engine controller
Integrierte Ablauf- und Motorsteuerung
Contrôleur de purge et moteur intégré
2019-06-05
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
BLEED-OFF VALVE DRIVE CONTROLLER FOR AIRCRAFT GAS TURBINE ENGINE
Europäisches Patentamt | 2020
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