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
2022-01-11
Patent
Electronic Resource
English
AIRCRAFT ENGINE NACELLE COMPRISING ICE PROTECTION SYSTEM
European Patent Office | 2020
|