A frost protection system for an aircraft engine nacelle, the nacelle comprising an inner shroud provided with at least one acoustic panel and an air intake lip forming a leading edge of the nacelle. The protection system comprises a heat exchanger device including at least one heat pipe configured to transfer heat emitted by a heat source to the at least one acoustic panel.
FROST PROTECTION SYSTEM FOR AN AIRCRAFT ENGINE NACELLE
2019-04-25
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT ENGINE NACELLE COMPRISING ICE PROTECTION SYSTEM
European Patent Office | 2020
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