公开(公告)号：US20220282669A1

公开(公告)日：2022-09-08

申请号：US17684667

申请日：2022-03-02

Applicant: Airbus Operations SAS

Inventor： Arnaud BOURHIS ,  Gregory ALBET ,  Alain PORTE

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.

公开(公告)号：US20210078718A1

公开(公告)日：2021-03-18

申请号：US17017482

申请日：2020-09-10

Applicant: Airbus Operations SAS

Inventor： Arnaud BOURHIS ,  Gregory ALBET ,  François PONS

IPC: B64D33/02 ,  B64D15/04

Abstract: An air inlet for an aircraft nacelle, including a lip and a front frame, which together form a duct with D-shaped section receiving hot air. The front frame is arranged in an advanced position inside the lip. The lip has de-icing grooves, which communicate with the duct and extend essentially downstream of the front frame. Downstream of the front frame, outside of the de-icing grooves, the lip has perforated zones provided with sound absorption holes. The air inlet includes a foil, which hermetically seals the de-icing grooves and is provided with sound absorption holes facing the perforated zones. The air inlet comprises acoustic panels inside the lip downstream of the front frame. The advanced position of the front frame, due to the de-icing grooves which ensure the de-icing of the lip downstream of the front frame, allows the acoustic treatment surface of the air inlet to be increased.

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

IPC: B64D15/16 ,  B64D15/12

CPC classification number: B64D15/16 ,  B64D15/12

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.

公开(公告)号：US20230286234A1

公开(公告)日：2023-09-14

申请号：US18180283

申请日：2023-03-08

Applicant: Airbus Operations SAS

Inventor： Laurent CALIMAN ,  Florian RAVISE ,  Arnaud BOURHIS

IPC: B29D24/00 ,  B29C70/08 ,  B29C70/88 ,  B29C65/00

CPC classification number: B29D24/005 ,  B29C70/083 ,  B29C70/88 ,  B29C66/438 ,  B29L2031/608

Abstract: A honeycomb structure having a core made up of a plurality of corrugated sheets which are superposed and adhesively bonded together is described. The corrugated sheets are made from a thermally insulating material. Bear filaments are made up of thermally conductive filaments. The honeycomb structure can be used when the ambient temperature exceeds, for example, 120° C.

公开(公告)号：US20230138228A1

公开(公告)日：2023-05-04

申请号：US17979023

申请日：2022-11-02

Applicant: Airbus Operations SAS

Inventor： Arnaud BOURHIS ,  Florian RAVISE ,  Maxime ZEBIAN

IPC: F02C7/045

Abstract: A module ensuring an acoustic attenuation of a flow of a first fluid and a heat exchange between the first fluid and a second fluid. The module comprises a perforated first wall with a cutout, a second wall, a cellular structure extending from the second wall to the first wall, a recess provided in the cellular structure between a perforated bottom and a perforated top, and a heat exchanger which is fixed inside the recess between the bottom and the top and in which the second fluid circulates. Such a module ensures an attenuation of sound waves and a heat exchange without limiting the attenuation surface.