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1. 发明公开

EP4420756A1 ARRANGEMENT FOR REMOVING CO2 FROM AIR, METHOD OF MAKING SAME, AND METHOD FOR REMOVING CO2 FROM AIR 审中-公开
公开(公告)号：EP4420756A1
公开(公告)日：2024-08-28
申请号：EP23158848.4
申请日：2023-02-27
申请人： Airbus Operations GmbH , Airbus S.A.S.
发明人： Bulmann, Antje , Matthias, Carsten , Schleifenbaum, Christiane , Ketscher, Leon , Horn, Tobias , Fetter, Viktor
IPC分类号： B01D53/04
CPC分类号： B01D53/0462 , B01D2257/50420130101 , B01D2258/0620130101 , B01D2259/4009620130101 , B01D2253/2520130101 , B01D2253/20620130101 , B01D2253/20220130101 , B01D2259/457520130101 , B01D53/0438
摘要： An arrangement (10) for removing CO2 from air comprises an air permeable, electrically conductive mesh (11) coated with an adsorption material (12), in particular amine, which is configured for adsorbing CO2 from an air flow (13) through the mesh (11), and electric contact elements (14, 15) connected to a power supply (16) and contacting the electrically conductive mesh (11) to provide an electric current through the mesh (11) for electric resistance heating of the mesh (11) to remove the adsorbed CO2 from adsorption material (12). In a method, an air flow 13 is directed through the mesh (11) for adsorbing CO2, and the mesh (11) is heated by resistance heating, preferably but not exclusively, in a negative pressure environment for a desorption process to remove the CO2 from the adsorption material.

3. 发明公开

EP4411541A1 COMPUTER-IMPLEMENTED TASK SCHEDULING METHOD 审中-公开
公开(公告)号：EP4411541A1
公开(公告)日：2024-08-07
申请号：EP23154382.8
申请日：2023-02-01
申请人： Airbus S.A.S.
发明人： Klügel, Markus
IPC分类号： G06F9/48
CPC分类号： G06F9/4887
摘要： A computer-implemented task scheduling method for use in a data processing device (10) with a plurality of computational hardware components (12) and for scheduling a set R[t] of computational tasks (14) at a given time t ∈ Tact, Tact being a set of discrete time intervals each of length Δt, among a set A[t] of said computational hardware components (12) each available at the given time t ∈ Tact and configured for executing any one of the computational tasks (14), each computational task (14) being associated with a corresponding task quality class c ∈ C, C being a set of task quality classes, each task quality class c ∈ C and each computational hardware component (12) being associated with a corresponding processing time value Tproc in terms of Δt, the associated processing time value Tproc being indicative of a duration for processing any one computational task (14) of the corresponding class c ∈ C by means of the corresponding computational hardware component (12), each task quality class c ∈ C and each computational hardware component (12) being further associated with a corresponding utility value Uproc, the associated utility value Uproc being indicative of a cost or added value that is induced by processing any one computational task (14) of the corresponding class c ∈ C by means of the corresponding computational hardware component (12).

4. 发明公开

EP4378832A1 SIEGE DE COCKPIT D'AERONEF A AFFICHAGE INTEGRE A L' ARRIERE DU DOSSIER ET COCKPIT MUNI D'UN TEL SIEGE 审中-实审
公开(公告)号：EP4378832A1
公开(公告)日：2024-06-05
申请号：EP23209967.1
申请日：2023-11-15
申请人： Airbus (S.A.S.)
发明人： ZANEBONI, Jason
IPC分类号： B64D11/06
CPC分类号： B64D11/0689
摘要： La présente invention concerne un siège (8) de cockpit comprenant un dossier (10) présentant une face (12) arrière et une assise (11), caractérisé en ce que le dossier présente un équipement (14) intégré à la face arrière (12) du dossier et comportant au moins une commande (28) de paramètre de confort et une zone (16) d'affichage.
Ainsi les commandes de paramètre de confort sont facilement visibles et accessibles en entrant dans le cockpit et l'entrant peut directement adapter son environnement selon ses souhaits.
La présente invention concerne également le cockpit muni d'un tel siège et le procédé de contrôle de paramètre de confort à partir d'un tel siège.

5. 发明公开

EP4339010A3 DISPOSITIF DE TRANSFERT D' ENERGIE ÉLECTRIQUE COMPRENANT UN SYSTÈME DE CENTRAGE 审中-实审
公开(公告)号：EP4339010A3
公开(公告)日：2024-05-22
申请号：EP23181030.0
申请日：2023-06-22
申请人： Airbus (S.A.S.)
发明人： CHASSAIGNE, Didier , FORGET, Frédéric , REVEL, Ivan , LOEHRMANN, Antoine , CREPEL, Olivier
IPC分类号： B60L53/12 , B60L53/302 , B60L53/34 , H02J50/10 , B60L53/35
CPC分类号： B60L53/12 , B60L53/34 , H02J50/10 , B60L53/302 , B60L2200/1020130101 , B60L53/35 , H02J7/02 , H02J7/0042 , H02J50/005 , H01F38/14
摘要： L'invention a pour objet un dispositif de transfert d'énergie électrique comprenant des première et deuxième parties (32, 34) mobiles l'une par rapport à l'autre entre des états écarté et rapproché, la première partie (32) comprenant un premier logement (52), configuré pour loger au moins partiellement la deuxième partie (34), comportant au moins une première surface latérale sur laquelle est positionné au moins un premier élément de transfert d'énergie électrique, la deuxième partie (34) présentant une deuxième surface latérale pour chaque première surface latérale du logement (52), ayant une forme générale complémentaire de la forme du premier logement (52) et sur laquelle est positionné au moins un deuxième élément de transfert d'énergie électrique, les premier et deuxième éléments de transfert d'énergie électrique assurant un transfert d'énergie électrique entre eux lorsque les première et deuxième parties (32, 34) sont à l'état rapproché.

6. 发明授权

EP3866261B1 VERFAHREN ZUM HERSTELLEN EINER ELEKTRONIKANORDNUNG, DIE GEGEN RAUE UMGEBUNGSBEDINGUNGEN GESCHÜTZT IST, FÜR LUFTFAHRZEUGE, ELEKTRONIKANORDNUNG UND LUFTFAHRZEUG 有权转让
公开(公告)号：EP3866261B1
公开(公告)日：2024-04-10
申请号：EP20176490.9
申请日：2020-05-26
发明人： Friedberger, Alois
IPC分类号： H01Q1/40 , H01Q1/08 , H01Q1/28 , B32B3/08 , B32B5/02 , B32B5/26 , B32B7/03 , B32B27/08 , H01Q1/42

8. 发明公开

EP4279256A1 ARRANGEMENT INCLUDING A FIBRE-REINFORCED COMPOSITE COMPONENT OR ASSEMBLY, AIRCRAFT OR SPACECRAFT, METHOD OF PRODUCING AN ARRANGEMENT, AS WELL AS METHOD OF MONITORING STRUCTURAL INTEGRITY 审中-实审转让
公开(公告)号：EP4279256A1
公开(公告)日：2023-11-22
申请号：EP22173620.0
申请日：2022-05-16
申请人： Airbus Operations GmbH , Airbus SAS
发明人： Linde, Peter , Lenczowski, Blanka , Heltsch, Norbert
IPC分类号： B29C70/88 , B29C70/54 , B29C70/24 , B32B5/06 , D04B21/16 , G01M5/00
摘要： Arrangement including a fibre-reinforced composite component or assembly, aircraft or spacecraft, method of producing an arrangement, as well as method of monitoring structural integrity
An arrangement (1, 1a-c; 1') is proposed which includes a fibre-reinforced composite component or assembly (2, 2a-c; 2') and a monitoring device (45; 75). The composite component or assembly comprises at least first and second reinforcing fibre formation sections (3, 4; 3, 5) stitched to each other using a yarn (30; 30'; 30"; 60; 60'; 60") so as to connect the fibre formation sections along a seam (25, 25a-c; 55), the yarn being electrically conductive along a length thereof. The monitoring device is adapted and coupled to the yarn in such a manner as to be capable of sending an electrical input signal along at least a section (37; 67) of the yarn (30; 30'; 30"; 60; 60'; 60") that forms the seam (25, 25a-c; 55) or part thereof and receiving a response signal on the yarn (30; 30'; 30"; 60; 60'; 60"). Furthermore, the invention provides an aircraft or spacecraft (100) comprising at least one arrangement (1, 1a-c; 1') of this type, to a method of producing an arrangement (1, 1a-c; 1') including a fibre-reinforced composite component or composite assembly (2, 2a-c; 2'), and to a method of monitoring the structural integrity of a fibre-reinforced composite component or assembly (2, 2a-c; 2').

9. 发明授权

EP3306324B1 DISPOSITIF DE MESURE DE PARAMETRES DE VOL A CAPTEURS OPTIQUES DE DEFORMATION PORTES PAR LE RADÔME D'UN AERONEF 有权
公开(公告)号：EP3306324B1
公开(公告)日：2020-04-22
申请号：EP17194972.0
申请日：2017-10-05
申请人： Airbus Operations S.A.S. , Airbus (S.A.S.)
发明人： Bernus Christophe , Esteve, Nathalie , Redon, Jean , Poret, Cécile , Boisson, Thomas , Bulancea, Andrei , Fontaine, Alain
IPC分类号： G01P5/02 , G01P13/02

10. 发明公开

EP3530533A3 AIRCRAFT BRAKING 有权
公开(公告)号：EP3530533A3
公开(公告)日：2019-12-18
申请号：EP19159658.4
申请日：2019-02-27
申请人： Airbus Operations Limited , AIRBUS OPERATIONS (S.A.S) , Airbus S.A.S.
发明人： BILL, Andrew , OZA, Utsav , RAMIREZ-PAYA, Esther , CLARKE, David
IPC分类号： B60T17/22 , B60T8/17
摘要： Disclosed is a braking system and a method for applying one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions. The method comprises: receiving an indication of an aircraft speed from an aircraft speed indicator; controlling a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; and controlling the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold. Also disclosed is an aircraft comprising one or more aircraft wheel brakes and the disclosed braking system.

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