A method and apparatus for generating a flow of heated air (124) in an airfoil model of an inlet (104) of an aircraft (108) engine. Heated air (124) is sent into a duct system associated with the airfoil model (110) of the inlet (104) of the aircraft (108) engine. The heated air (124) is circulated within the airfoil model (110) of the inlet (104) of the aircraft (108) engine using the duct system in a manner that simulates air flowing in the inlet (104) of the aircraft (108) engine.
Inlet icing protection simulation system
System zur Simulation eines Vereisungsschutzes für den Lufteinlass
Système de simulation de protection contre le givrage d'entrée d'air
2017-05-10
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
DYNAMIC RESONANCE SYSTEM AND METHOD FOR ANTI-ICING AND DE-ICING OF INLET GRIDS
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