Invention Grant
- Patent Title: Nacelle air intake provided with a mixed ice protection system
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Application No.: US17684667Application Date: 2022-03-02
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Publication No.: US11643967B2Publication Date: 2023-05-09
- Inventor: Arnaud Bourhis , Gregory Albet , Alain Porte
- 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: FR 02075 2021.03.03
- Main IPC: F02C7/047
- IPC: F02C7/047 ; F02C7/24

Abstract:
An optimized protection against ice on the inner and outer faces of an aircraft engine nacelle air intake with the air intake including an outer face and an inner face meeting at a line at the longitudinally extreme, called extremum line, an acoustic panel being installed on the inner surface of a part of the inner face. An elimination system based on vibration of the ice formed is put in place on at least a part of the outer face and an ice formation prevention system using a hot fluid is put in place on at least a part of the inner face and either an ice elimination system or an ice formation prevention system using a hot fluid is installed on the inner face and on the outer face, a marking line marking the boundary between the two systems.
Public/Granted literature
- US20220282669A1 NACELLE AIR INTAKE PROVIDED WITH A MIXED ICE PROTECTION SYSTEM Public/Granted day:2022-09-08
Information query
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