An anti-icing protection system for an aircraft engine nacelle, the nacelle comprising an inner shroud provided with at least one acoustic panel, an air intake lip forming a leading edge of the nacelle, the protection system comprising a heat exchanger device including at least one heat pipe configured to transfer heat emitted by a heat source to the acoustic panel or panels.
AIRCRAFT ENGINE NACELLE COMPRISING AN ANTI-ICING PROTECTION SYSTEM
2020-04-23
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT ENGINE NACELLE WITH ANTI-ICING SYSTEM USING TWO-PHASE FLUID
Europäisches Patentamt | 2020
|