公开(公告)号：US20250042565A1

公开(公告)日：2025-02-06

申请号：US18787458

申请日：2024-07-29

Applicant: Airbus Operations SAS

Inventor： Emeric CHANCERELLE ,  Franck DOBIGEON ,  Brice SAUDEL ,  Grégoire SMITH

IPC: B64D33/02 ,  F02C7/04

Abstract: An aircraft air intake comprising a lip, an internal panel which comprises a front edge linked to the lip, a front frame which comprises an outer edge and an inner edge linked to the lip and/or to the internal panel, a rear frame which comprises an outer edge, directly or indirectly linked to the lip and an inner edge linked to the rear edge of the internal panel, and at least one joining element linking the outer edges of the front frame and of the rear frame.

公开(公告)号：US20250002168A1

公开(公告)日：2025-01-02

申请号：US18742140

申请日：2024-06-13

Applicant: Airbus Operations SAS

Inventor： Florent CREBASSOL ,  Grégoire SMITH ,  Florent HUET ,  François PONS

IPC: B64D33/02 ,  B64D45/02

Abstract: An acoustic attenuation panel comprising, from a first face to an opposite second face, an acoustically resistive structure, at least one cellular structure and a reflective layer. This acoustic attenuation panel comprises an induction-based frost treatment system which comprises at least one electromagnetic field generator positioned at the reflective layer and at least one electrically conductive element situated at the first face of the acoustic attenuation panel and configured to generate a heating through an induction phenomenon. Also an aircraft and an air intake of an aircraft nacelle comprising at least one such panel.