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1. 发明公开

EP4386936A1 COOLING ARRANGEMENT FOR THERMAL RUNAWAY EVENTS 审中-公开
公开(公告)号：EP4386936A1
公开(公告)日：2024-06-19
申请号：EP22213100.5
申请日：2022-12-13
申请人： Airbus S.A.S.
发明人： FRIEDBERGER, Alois , FRIEDL, Stephan
IPC分类号： H01M10/613 , H01M10/625 , H01M10/6561 , H01M50/30 , H01M50/342 , H01M50/383
CPC分类号： H01M50/30 , H01M50/3425 , H01M50/383 , H01M10/613 , H01M10/625 , H01M10/6561
摘要： The present invention relates to a cooling for thermal runaway events in battery arrangements of vehicles. In order to provide an improved cooling, an arrangement (10) for a vehicle (14) is provided. The arrangement comprises a conduit (16). The conduit comprises: a primary inlet (18), a secondary inlet (20), an outlet (22) and an air flow passage (24). The air flow passage is provided between the primary inlet and the outlet. The primary inlet is configured to be fluid-dynamically connected to an enclosed volume (26) accommodating a battery arrangement (28), in order to direct a decompressing fluid stream (30) originating from the battery arrangement in a thermal runaway event via the air flow passage. The outlet is configured to discharge the decompressing fluid stream to an outboard environment (32) of the vehicle. The secondary inlet is configured to provide a supply fluid (34) cooling the decompressing fluid stream.

2. 发明公开

EP4351042A1 PHOTON SOURCE AND METHOD FOR QUANTUM COMMUNICATION 审中-公开
公开(公告)号：EP4351042A1
公开(公告)日：2024-04-10
申请号：EP22199971.7
申请日：2022-10-06
申请人： Airbus S.A.S.
发明人： Comin, Alberto
IPC分类号： H04B10/70 , H04J14/04
摘要： The present invention provides a photon source for quantum communication. The photon source comprises a plurality of optical channels, each comprising: a light emitter configured to emit optical pulses, and a phase mask optically connected to the respective light emitter and configured to encode an orbital angular momentum into incident light, wherein each of the phase masks of each optical channel is configured to encode a mutually orthogonal orbital angular momentum to the optical pulses emitted by the light emitter of each optical channel to provide an encoded optical output; a controller electrically coupled to each light emitter in each optical channel and configured to control parameters of the optical pulses; and combining optics configured to combine the encoded optical output of each of the optical channels to form a single encoded optical signal. Furthermore, the present invention provides an optical quantum communication system comprising the inventive photon source. Furthermore, the present invention provides a method for quantum communication.

3. 发明公开

EP4344997A1 MULITFUNCTIONAL THERMAL AND ACOUSTIC INSULATION SYSTEM FOR AN AIRCRAFT 审中-实审
公开(公告)号：EP4344997A1
公开(公告)日：2024-04-03
申请号：EP22198874.4
申请日：2022-09-29
申请人： Airbus Operations GmbH , Airbus S.A.S.
发明人： Bonaccurso, Elmar , Thomas, Christian , Friedberger, Alois , Machunze, Wolfgang , Helwig, Andreas , Witte, Tassilo
IPC分类号： B64C1/40
摘要： A multifunctional thermal and acoustic insulation system (3) to be received between an inner surface (8) of an aircraft primary structure, such as an aircraft fuselage structure (2, 9), and a surface (11) of a panel arrangement (10) delimiting an aircraft cabin, the surface (11) facing away from the aircraft cabin, comprises a multilayer structure (7) and a plurality of functional components (12) formed integrally and non-exchangeably with the multilayer structure (7). The multilayer structure (7) has a thermal and acoustic damping performance and comprises, in a stacked arrangement, a continuous first outer layer (5), a core layer (4) and a continuous second outer layer (6). The core layer (4) is received between the first and second outer layers (5, 6) so that the first and second outer layers (5, 6) cover the core layer (4) at least on opposite sides thereof. Functions of the functional components (12) are related to at least one of the thermal and the acoustic damping performance of the multilayer structure (7) and the functional components (12) are provided on a first outer layer side of the core layer (4) and/or on a second outer layer side of the core layer (4).

4. 发明公开

EP4344993A1 THERMAL AND ACOUSTIC INSULATION SYSTEM FOR AN AIRCRAFT 审中-实审
公开(公告)号：EP4344993A1
公开(公告)日：2024-04-03
申请号：EP22198876.9
申请日：2022-09-29
申请人： Airbus Operations GmbH , Airbus S.A.S.
发明人： Thomas, Christian , Friedberger, Alois , Machunze, Wolfgang , Helwig, Andreas , Witte, Tassilo , Bonaccurso, Elmar
IPC分类号： B64C1/06 , B64C1/40
摘要： A thermal and acoustic insulation system (3) for an aircraft (1), the system (3) adapted to be received between an inner surface (11) of an aircraft primary structure, such as an aircraft fuselage structure (2, 12), and a surface (14) of a panel arrangement (13) delimiting an aircraft cabin, the surface (14) facing away from the aircraft cabin, comprises an insulation package (6) and at least one sensor (17) adapted to measure a level of humidity present in the insulation package (6). The insulation package (6) comprises a core layer (4) having a thermal and acoustic damping performance, and a packing layer (5) enclosing the core layer (4). The packing layer (5) is provided with a plurality of normally closed and selectively openable drainage openings (7) which are actuatable to change between their normally closed state and an open state to allow for selective dehumidification of the insulation package (6) on demand.

5. 发明公开

EP4336552A1 COMPOSANT ÉLECTRONIQUE COMPRENANT UN FLUIDE DIPHASIQUE POUR ÉVACUER LES CALORIES THERMIQUES DES SEMI-CONDUCTEURS DUDIT COMPOSANT ÉLECTRONIQUE 审中-实审
公开(公告)号：EP4336552A1
公开(公告)日：2024-03-13
申请号：EP23187170.8
申请日：2023-07-24
申请人： Airbus (S.A.S.)
发明人： LOEHRMANN, Antoine , CREPEL, Olivier
IPC分类号： H01L23/427 , H01L23/373
摘要： Composant électronique comprenant un fluide diphasique pour évacuer les calories thermiques des semi-conducteurs dudit composant électronique.
L'invention a pour objet un composant électronique (30) comprenant un empilement de couches (32a-d) de matériau conducteur électrique et de couches (34a-c) de matériau non-conducteur électrique, un volume étant défini entre deux couches adjacentes, et un semi-conducteur (36) étant disposé dans ledit volume. Le composant électronique (30) comprend également des moyens de refroidissement prenant la forme d'un fluide diphasique remplissant ledit volume (38).
Ce composant électronique présente un poids et un volume réduits, ainsi que des performances améliorées.

6. 发明公开

EP4269662A1 METHODS FOR ANODIZING A PART SURFACE AND SUBSEQUENTLY COATING THE ANODIZED PART SURFACE FOR CORROSION PROTECTION PURPOSES 审中-实审
公开(公告)号：EP4269662A1
公开(公告)日：2023-11-01
申请号：EP22170800.1
申请日：2022-04-29
申请人： Airbus Operations GmbH , Airbus S.A.S.
发明人： Paz Martinez-Viademonte, Mariana , Hack, Theodor , Burchardt, Malte , Beneke, Martin
IPC分类号： C25D11/08 , C25D11/10 , C25D11/16
摘要： In order to improve adhesion of Cr(VI)-free primers and suitable topcoats on aircraft parts, a method for anodising part surface of the aircraft part that includes aluminium or an aluminium alloy is proposed. The part is cleaned and exposed to an anodising electrolyte. During anodising it is essential that the temperature of the anodising electrolyte is maintained at a constant temperature chosen from a range from 42 °C to 60 °C. This results in a surprising surface morphology that improves adhesion of primers and/or topcoats on the aircraft part.

7. 发明公开

EP4203231A1 MODULAR ENERGY SOURCE WITH BYPASS AND RECONFIGURATION FUNCTIONALITY AND METHOD OF OPERATING A MODULAR ENERGY SOURCE 无效
公开(公告)号：EP4203231A1
公开(公告)日：2023-06-28
申请号：EP21216596.3
申请日：2021-12-21
申请人： Airbus (S.A.S.)
发明人： Kapaun, Florian , Steiner, Gerhard
IPC分类号： H02J7/00 , B60L3/00 , B60L50/64 , B60L58/12 , B60L58/18
摘要： A modular energy source (10) with bypass and reconfiguration functionality, comprises an arrangement of energy source modules (12, 13) connected in series for providing electrical energy to an electric network (11), and a number of bypass and balancing units (14, 15), each being configured for bypassing an assigned energy source module (12, 13). Each bypass and balancing unit (14, 15) comprises a first switch (16, 17) connected in series with its assigned energy source module (12, 13) for isolating it in case of a failure of that module, and a second switch (18, 19) connected in parallel to the first switch (16, 17) and to its assigned energy source module (12, 13) for bypassing that module when it is isolated. A method of operating the modular energy source (10) comprises isolating at least one of the energy source modules (12, 13) in case of a failure of that module, and bypassing that module (12, 13) when it is isolated.

8. 发明公开

EP4199285A1 CIRCUIT BREAKER WITH PRE-CHARGING AND CURRENT LIMITING FUNCTIONS, METHOD OF OPERATING SAME, POWER SUPPLY CIRCUIT AND AIRCRAFT 审中-实审
公开(公告)号：EP4199285A1
公开(公告)日：2023-06-21
申请号：EP21215954.5
申请日：2021-12-20
申请人： Airbus S.A.S.
发明人： Kapaun, Florian , Steiner, Gerhard
IPC分类号： H02H3/08 , H02H9/00 , H02H9/02
摘要： A circuit breaker (13) with pre-charging and current limiting functions, wherein the circuit breaker (13) is configured for being provided in a power line (14) connecting an electrical energy source (11) and an electric network (12). The circuit breaker (13) comprises a short circuit protection unit (15) comprising a first semiconductor switch (16), a precharge unit (17) connected in parallel to the short circuit protection unit (15) and comprising a second semiconductor switch (18), and a current limit unit (19) connected in parallel to the short circuit protection unit (15) and to the precharge unit (17), the current limit unit (19) comprising a third semiconductor switch (20).

9. 发明公开

EP4198326A1 ROTARY JOINT WITH ANGULAR LOCKING MECHANISM 审中-实审
公开(公告)号：EP4198326A1
公开(公告)日：2023-06-21
申请号：EP21214937.1
申请日：2021-12-15
申请人： AIRBUS S.A.S.
发明人： Bürger, Thomas
IPC分类号： F16C11/06 , F16C11/10
摘要： A rotary joint with angular locking mechanism comprises a socket rod having an at least partly spheroid concave bearing surface; a ball rod having an at least partly spheroid convex bearing surface slidingly engaging the concave bearing surface of the socket rod, wherein the curvature of the concave bearing surface of the socket rod corresponds substantially to the curvature of the convex bearing surface of the ball rod; wherein a locking element is embedded in the socket rod or the ball rod at the respective bearing surface and configured to be actuated to press against the respective opposite bearing surface to lock the socket rod with respect to the ball rod at a current relative position thereby setting a respective inclination angle between the socket rod and the ball rod.

10. 发明公开

EP4166307A1 FIBRE COMPOSITE STRUCTURE AND METHOD FOR MANUFACTURING A FIBRE COMPOSITE STRUCTURE 审中-实审
公开(公告)号：EP4166307A1
公开(公告)日：2023-04-19
申请号：EP21202628.0
申请日：2021-10-14
申请人： Airbus Defence and Space GmbH , Airbus (S.A.S.)
发明人： Karch, Christian , Friedberger, Alois
IPC分类号： B29C70/08 , B29C70/20 , B29C70/88 , B29C70/02 , B29C70/76 , B29C70/72 , B32B27/12 , H01Q1/42 , B29C70/68 , B65D5/42 , B65D25/54 , B29L31/00
摘要： A fibre composite structure includes a base structure being formed of a first fibre composite material that includes a plurality of first fibre bundles embedded in a first matrix material, wherein the base structure comprises an opening defined by first fibre bundles which include first sections and a second section that continuously or uninterruptedly interconnects the first sections, wherein the second section forms a bay that defines a part of the circumference of the opening. The fibre composite structure further includes a functional structure positioned in the opening of the base structure and joined with the first fibre composite material of the base structure.

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