Patents Assigned to Airbus (SA)
  • Aircraft galley
    Patent number: 12077300
    Abstract: An aircraft galley has a plurality of galley inserts and a master aircraft galley control unit. The galley inserts are connected to the master aircraft galley control unit via an aircraft galley data bus, and at least one panel, wherein the galley inserts each have a status selected from the following group: initialization, standby ON, ON, waiting, interrupted, ended maintenance fault, standby OFF, or stopped/ended. The galley also collects the respective statuses of the galley inserts. The data collector stores information which can be displayed on the panel in accordance with the respective statuses.
    Type: Grant
    Filed: June 29, 2020
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations GmbH
    Inventor: Thomas Taddey
  • Processes for offsetting a carbon footprint of a multistage trip and for the lifecycle of a vehicle
    Patent number: 12080109
    Abstract: Processes for determining carbon dioxide emission impact. In one process, a carbon dioxide emission impact is determined for each stage of a multi-stage trip. A traveler may make adjustments to the trip to offset the carbon dioxide emission impact of the entire trip and achieve a desired sustainability level for the trip. In another process, that may be used in the first process, the carbon dioxide emission impact for a vehicle is determined based on the entire life span of the vehicle, including a carbon dioxide emission impact for a production stage, a carbon dioxide emission impact for a usage stage, and a carbon dioxide emission impact for an end of life stage.
    Type: Grant
    Filed: February 18, 2020
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations GmbH
    Inventors: Paul Jörn, Markus Müller
  • Aircraft having a dihydrogen transport pipe and an embedding channel for said transport pipe
    Patent number: 12077312
    Abstract: An aircraft having at least one transport pipe in which dihydrogen flows and, for each transport pipe, an embedding channel in which the transport pipe is housed. The embedding channel has a gutter that has a bottom and an opening opposite the bottom and a cover that covers the opening of the gutter. The cover constitutes an outer wall of the aircraft in direct contact with external air surrounding the aircraft. The cover has ventilation windows passing through it that allow the passage of the dihydrogen towards the outside. With such an arrangement, even in the event of dihydrogen leaking into the embedding channel, the dihydrogen is automatically evacuated towards the outside of the aircraft.
    Type: Grant
    Filed: September 20, 2022
    Date of Patent: September 3, 2024
    Assignees: Airbus SAS, Airbus Operations SAS
    Inventors: Jérôme Milliere, Romain Joubert, Lionel Teyssedre, Alistair Forbes
  • System for providing a pressurized liquid
    Patent number: 12076672
    Abstract: A system for providing a pressurized liquid, having a reservoir for the liquid, which has a discharge and a feed, having a pump, having a first valve, having a separate filter chamber, having an inlet and at least one outlet, and a compressible, closed buffer body. The pump is between the discharge of the reservoir and the filter chamber and configured to increase pressure of the liquid within the filter chamber, the first valve between the feed of the reservoir and the filter chamber and configured to open in the direction of the reservoir upon attainment or exceedance of a minimum pressure of the liquid in the filter chamber. The buffer body is in the filter chamber such that it can be surrounded by liquid.
    Type: Grant
    Filed: January 28, 2022
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations GmbH
    Inventors: Jana Caspari, Torsten Trümper, Christopher Warsch
  • Tank comprising inner and outer chambers and at least one link system with flexible radial blades linking said chambers
    Patent number: 12078293
    Abstract: A double-walled tank including at least one link system linking the outer and inner chambers of the tank and including a central part linked to the inner chamber and at least three blades distributed around the central part, each blade extending between a first end linked to the central part and a second end which has a head linked to the outer chamber, each blade being sufficiently flexible to be deformed elastically between its first and second ends in a direction of displacement.
    Type: Grant
    Filed: February 21, 2023
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations SAS
    Inventor: Julien Gallardo
  • System of morphing control surface for aircraft wing
    Patent number: 12077291
    Abstract: A system includes at least one upper flexible skin intended to be fixed in the extension of an upper plane of the wing, a lower flexible skin intended to be movable in the extension of a lower plane of the wing and fixed along a trailing edge of the control surface, an actuator for generating a displacement of the lower flexible skin with respect to the lower plane. The displacement causes a curvature of the first, upper flexible skin and a curvature of the second, lower flexible skin having a concavity oriented in a same direction. The control surface system makes it possible to reduce the quantity of energy supplied by the actuator.
    Type: Grant
    Filed: November 22, 2022
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Cristobal Calatayud, Benjamin Trarieux, Brice Albert
  • Aircraft comprising at least one systems cabinet connected to a landing gear compartment by at least one sliding connection sliding in a longitudinal direction
    Patent number: 12077274
    Abstract: An aircraft having a systems cabinet positioned in an avionics bay to the rear of a landing gear compartment and connected to the fuselage by at least one lower connecting system. The systems cabinet and/or the lower connecting system comprises at least one longitudinal beam, which has a front end connected by a front connection to a wall separating the avionics bay and the landing gear compartment, the front connection comprising a sliding connection sliding in a direction substantially parallel to the longitudinal axis.
    Type: Grant
    Filed: March 17, 2023
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations SAS
    Inventors: Damien Aguera, Salim Chalqi, Yannick Lampure
  • Avionics network having synchronization domains, and method for synchronizing network subscribers in an avionics network
    Patent number: 12081364
    Abstract: An avionics network comprises at least one data bus system, a multiplicity of network subscribers connected to one or more of the data bus systems via network interfaces, a central configuration server configured to configure each of the multiplicity of network subscribers individually according to a predefined functionality, and a synchronization note configured to stipulate a work-cycle for the multiplicity of network subscribers via the at least one data bus system according to a stipulated synchronization protocol.
    Type: Grant
    Filed: September 24, 2020
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations GmbH
    Inventors: Stéphane Poulain, Hartmut Hintze
  • Diversity control for multi-access wireless networks
    Patent number: 12081492
    Abstract: A network system includes access points and wireless devices. Each wireless device can exchange data with at least one access point that includes a diversity matrix defining at least two data exchange connections between a first wireless device and at least one access point for exchanging data between the first wireless device and the at least one access point. The diversity matrix indicates a space domain with at least one access point, a frequency domain with at least one data transmission frequency value, and a time domain with at least one data transmission time. Each data exchange connection is defined by an access point, a data transmission frequency, and a data transmission time, selected from the diversity matrix. The at least two data exchange connections between the first wireless device and the at least one access point are configured to transmit the same information.
    Type: Grant
    Filed: May 17, 2022
    Date of Patent: September 3, 2024
    Assignee: Airbus (S.A.S.)
    Inventors: Paulo Mendes, Thomas Meyerhoff
  • Aircraft comprising at least one system rack connected to a floor rail by at least one connecting system
    Patent number: 12077275
    Abstract: An aircraft including at least one system rack positioned under a floor and including a series of vertical first uprights, distributed in a direction parallel to the longitudinal axis of the aircraft. The aircraft includes at least a first upper connecting system connecting at least one of the first uprights and a rail of the floor oriented parallel to the longitudinal axis. In so far as the first uprights of the system rack are not connected to the crossbeams of the floor, they can be positioned irrespective of the position of the crossbeams, and this contributes to simplifying the design of the system racks and allows these to be standardized.
    Type: Grant
    Filed: December 15, 2022
    Date of Patent: September 3, 2024
    Assignee: Airbus Operations SAS
    Inventors: Damien Aguera, Matthieu De Kergommeaux, Salim Chalqi, Gaspard Supan
  • Methods, systems, and computer readable media for utilizing a linear sequence coding scheme
    Patent number: 12074681
    Abstract: Methods, systems, and computer readable media for utilizing a linear sequence coding scheme. In some embodiments, a method for utilizing a linear sequence coding scheme includes at a first computing device generating, using a linear sequence coding scheme and a source message, coded network packets, wherein each of the coded network packets indicates coded symbols, wherein each of the coded symbols is linear independent, and sending, via a lossy channel or a wireless channel, the coded network packets.
    Type: Grant
    Filed: August 20, 2021
    Date of Patent: August 27, 2024
    Assignee: Airbus (S.A.S.)
    Inventors: Klaus-Werner Rueger, Romain Desautard, Zhongren Cao, Anders Nilsson Plymoth
  • Actively dried equipment unit with a movable mechanical element in an aircraft
    Patent number: 12071248
    Abstract: An equipment unit for installation in an aircraft includes an enclosure, in which at least one movable mechanical element is arranged, a supply duct, and a non-return valve, wherein the enclosure includes an inflow port and an outflow port, wherein the supply duct is connected to the inflow port, wherein the non-return valve is connected to the outflow port, wherein the supply duct is connectable to a source of heated air providable in the respective aircraft, and wherein the enclosure is designed that air supplied through the supply duct enters the enclosure through the inflow port, picks up moisture from inside the enclosure and exits through the outflow port.
    Type: Grant
    Filed: July 11, 2022
    Date of Patent: August 27, 2024
    Assignee: Airbus Operations GmbH
    Inventors: Jan Haserodt, Christoph Winkelmann
  • Spoiler actuation apparatus for moving an aircraft spoiler
    Patent number: 12071221
    Abstract: A spoiler actuation apparatus for moving an aircraft spoiler. The spoiler is moveable between a stowed configuration and a deployed configuration. The spoiler actuation apparatus includes a guide member, a rack mounted on the guide member and slideable along a longitudinal axis of the guide member, and a gear coupled to the rack, the gear arranged to move the spoiler in response to sliding of the rack. The rack is held at a first position when the spoiler is in the stowed configuration. An actuator moves the rack from the first position to a second position along the longitudinal axis. When the rack is at the second position, the rack is operable to accelerate relative to the guide member away from the second position by an aerodynamic force acting on the spoiler.
    Type: Grant
    Filed: June 13, 2022
    Date of Patent: August 27, 2024
    Assignee: Airbus Operations Limited
    Inventor: Benjamin Bishop
  • Aircraft wing with trailing edge panel
    Patent number: 12071239
    Abstract: An aircraft wing including a wingbox with an upper cover, a lower cover, and a rear spar. A lower trailing edge panel is provided with a leading edge attached to the wingbox. The wing includes a flap, a flap deployment mechanism which is configured to deploy the flap, and a fairing which covers the flap deployment mechanism. A first end of a link is pivotally attached to the lower trailing edge panel at a first pivot joint, and a second end of the link is pivotally attached to the fairing at a second pivot joint. The second pivot joint is lower than the first pivot joint.
    Type: Grant
    Filed: March 24, 2022
    Date of Patent: August 27, 2024
    Assignee: Airbus Operations Limited
    Inventor: William Tulloch
  • Methods, systems and devices for free-space optical communications
    Patent number: 12074639
    Abstract: Methods, systems, and devices for free-space optical communications. An aircraft includes a flat optical communication terminal on an external surface of the aircraft, the flat optical communication terminal being configured to communicate with a ground station via a free-space optical communication link.
    Type: Grant
    Filed: June 8, 2022
    Date of Patent: August 27, 2024
    Assignee: Airbus (S.A.S.)
    Inventors: Alberto Comin, Thomas Multerer, Andrew A. Anderson, Jan Tepper, Bernd Schleicher, Andreas Drexler, Alejandro Gimeno Martín, Kevin Shortt
  • Method for Optimizing a Modification of an Ad-Hoc-Edge Network with a Resource-Aware Service Allocation Strategy and a System for Executing Such a Method
    Publication number: 20240284153
    Abstract: A method for optimizing a modification of an ad-hoc-edge network with a resource-aware service allocation strategy is described for deployment of a multitude of correlated microservices, which define a service, on an ad-hoc-edge network topology including a multitude of edge devices and a multitude of mobile computational devices with limited resources, interconnected in an ad-hoc manner. The services are thereby not deployed as a monolithic element in a single computational device, but as a set of correlated microservices, each of which can be deployed and executed in a different mobile computational device. Hence, an efficient allocation and scheduling of computational tasks among the set of resource constrained devices, for example energy consumption, ensure the proper execution of the overall service.
    Type: Application
    Filed: February 20, 2024
    Publication date: August 22, 2024
    Applicant: Airbus S.A.S.
    Inventor: Paulo Jorge Milheiro Mendes
  • Aircraft comprising at least one hydrogen supply device and at least one sealed container, in which at least one item of equipment of said hydrogen supply device is positioned
    Patent number: 12065260
    Abstract: An aircraft including at least one hydrogen engine, at least one hydrogen supply device including at least one hydrogen tank and at least one item of equipment through which the hydrogen flows and which is positioned between the hydrogen tank and the hydrogen engine. The aircraft includes at least one sealed container sealed from the outside air, in which sealed container the equipment of the hydrogen supply device is positioned. This solution allows a safe hydrogen installation to be obtained using existing equipment.
    Type: Grant
    Filed: August 1, 2022
    Date of Patent: August 20, 2024
    Assignees: Airbus SAS, Airbus Operations SAS
    Inventors: Alexis Pissavin, Lionel Czapla, Alistair Forbes
  • Fluid circuit comprising a connecting fitting for pipes, comprising a guide member for a heater duct
    Patent number: 12066136
    Abstract: A fluid circuit, in particular for an aircraft, having at least a first pipe, a second pipe and a connecting fitting, each pipe having a connection end and extending along an axis X, the connecting fitting, movably mounted between the two pipes, being configured to mechanically connect the two connection ends, the connecting fitting having a connecting sleeve and a guide member formed on an outer surface of the connecting sleeve and configured to cooperate with a heater duct so as to guide it between the two pipes, the heater duct being configured to transmit heat to the pipes and to the connecting fitting so as to prevent them from icing up.
    Type: Grant
    Filed: November 24, 2020
    Date of Patent: August 20, 2024
    Assignee: Airbus Atlantic
    Inventor: Daniel Perherin
  • Seat assembly for a cabin of a means of transportation
    Patent number: 12065248
    Abstract: The invention relates to a seat assembly for a cabin of a means of transportation, having an aisle which is arranged in the longitudinal direction of the cabin, two mutually spaced cabin walls which are oriented parallel to the aisle at least in some regions and laterally delimit the cabin, two outer passenger seat regions which are separated from one another by the aisle and each of which adjoins one of the two cabin walls, wherein the outer passenger seat regions have at least one row of seats with a respective inner first seat module which faces the aisle, a central second seat module adjoining the first module, and an outer third seat module adjoining the respective cabin wall.
    Type: Grant
    Filed: August 27, 2020
    Date of Patent: August 20, 2024
    Assignee: Airbus Operations GmbH
    Inventor: Tobias Schmidt-Schäffer
  • Fluid tank for integration into a structure of an unmanned aircraft
    Patent number: 12065259
    Abstract: A fluid tank for integration into a structure of an unmanned aircraft includes a shell having a first axial wall, an oppositely arranged second axial wall, an upper side, a lower side, and an enclosed interior, at least one receiving chamber in the interior for storing fluid, and a collection chamber, which is arranged on the lower side and which is fluidically connected to the at least one receiving chamber. The collection chamber includes a bottom surface, through which there extends a drain, wherein a covering surface is arranged above the bottom surface and covers at least a portion of the collection chamber. At least one flow opening could be arranged on an upper side of the collection chamber, which flow opening allows gas bubbles to escape in the direction of the upper side of the fluid tank.
    Type: Grant
    Filed: September 30, 2020
    Date of Patent: August 20, 2024
    Assignee: Airbus Defence and Space GmbH
    Inventors: Borja Sanz Lopez, Clemens Brand, Michael Jost, Winfried Lohmiller, Georg Söllinger, Dieter Grebner, Oliver Motlik