- Patent Title: Aircraft engine nacelle comprising an anti-icing protection system
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Application No.: US16655387Application Date: 2019-10-17
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Publication No.: US11518526B2Publication Date: 2022-12-06
- Inventor: Alain Porte , Jacques Lalane , Gregory Albet , Maxime Zebian , Arnaud Bourhis
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1871238 20181019
- Main IPC: B64D15/04
- IPC: B64D15/04 ; B64D29/00 ; B64D33/02
Abstract:
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.
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