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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
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.
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公开(公告)号:US20230365265A1
公开(公告)日:2023-11-16
申请号:US18316334
申请日:2023-05-12
Applicant: Airbus Operations SAS , Institut National des Sciences Appliquées de Toulouse (INSAT) , Centre National de la Recherche Scientifique (CNRS) , Université Toulouse III - Paul Sabatier (UT3) , Institut Supérieur de l'Aéronautique et de l'Espace (ISAE) , École nationale supérieure des Mines d'Albi - Carmaux (IMT Mines ALBI)
Inventor: Arnaud BOURHIS , Younes RAFIK , Valerian PALANQUE , Valérie POMMIER BUDINGER , Marc BUDINGER , Brice SAUDEL , Yves CLERGENT , Philippe OLIVIER
Abstract: A de-icing element having a skin with a surface to be de-iced, at least one excitation actuator attached to the skin, the excitation actuator configured to excite the skin according to at least one predetermined vibration mode generating a deformation of the skin, the deformation of the skin comprising at least one antinode and one node. The skin having a characteristic thickness generally constant with, locally, at least one thickness variation that is localized according to the predetermined vibration mode or modes.
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