Patents Assigned to Airbus (SA)
  • Accommodation system for rollable containers in a vehicle, and a vehicle having such a system
    Patent number: 11597518
    Abstract: An accommodation system for an accommodation space for storing rollable containers in a vehicle. After a front container, which is arranged at the insertion opening, has been removed in the conventional manner, it is possible, through the use of the accommodation system, to remove the rear container which is arranged considerably spaced apart from the insertion opening in the interior of the accommodation space. For this purpose, a rail system is provided in the floor region of the accommodation space. A transfer plate is movable on the rail system in the floor region of the accommodation space and can assume a storage position and a removal position for the rear container.
    Type: Grant
    Filed: April 2, 2020
    Date of Patent: March 7, 2023
    Assignee: Airbus Operations GmbH
    Inventors: Michael Bauer, Hans-Gerhard Giesa, Roland Lange, Andreas Wietzke
  • Aircraft joint with a curable composite bushing
    Patent number: 11598373
    Abstract: An aircraft structural joint comprising a first structural component provided with an attachment hole that is configured to receive an corresponding attachment fastener provided by a second structural component; a curable composite bush compressed and cured between an outer diameter of the attachment fastener and the attachment hole when the first component is mounted to the second component, wherein the curable composite bush, when cured, prevents radial displacement of the attachment fastener within the attachment hole.
    Type: Grant
    Filed: September 24, 2018
    Date of Patent: March 7, 2023
    Assignee: Airbus Operations GmbH
    Inventors: Florian Lorenz, Dustin Shapi
  • Leading edge for an airfoil
    Patent number: 11597496
    Abstract: A leading edge for an airfoil of an aircraft includes a leading plate with a convex side and a concave side, and at least one container filled with a non-Newtonian fluid. The leading edge is configured to be secured to the torsion box of the airfoil. The at least one container is arranged between the concave side of the leading plate and the torsion box of the airfoil. An airfoil is also provided including such a leading edge. A method is provided for assembling such a leading edge.
    Type: Grant
    Filed: December 16, 2020
    Date of Patent: March 7, 2023
    Assignee: Airbus Operations S.L.
    Inventors: Javier Carlos Gomez del Valle, Alberto Balsa-Gonzalez
  • Semi-active system for providing a required fluid flow
    Patent number: 11597503
    Abstract: A semi-active system for providing a required fluid flow, the system comprising an outlet configured to protrude into the main flow direction of an external fluid flow external to the semi-active system, an exhaust channel provided, in relation to the main flow direction of the external fluid flow, beneath the outlet, the exhaust channel being configured to inject an exhaust fluid flow into the external fluid flow, a device configured to produce a jet fluid flow and a pipe provided within the exhaust channel, the pipe being configured to fluid-communicatively couple to the device, and entrain, by the produced jet fluid flow, the exhaust fluid flow.
    Type: Grant
    Filed: October 30, 2018
    Date of Patent: March 7, 2023
    Assignee: Airbus Operations GmbH
    Inventors: Peter Kreuzer, Hubert Stuke, Udo Krause
  • COMMUNICATION DEVICE, COMMUNICATION SYSTEM, AND METHOD FOR COMMUNICATION
    Publication number: 20230069277
    Abstract: An airborne communication device installed in a vehicle, wherein the airborne communication device is configured to receive navigation information from a ground-based communication device installed outside the vehicle via a datalink protocol. A ground-based communication device, a communication system, and a method for communication are described.
    Type: Application
    Filed: August 29, 2022
    Publication date: March 2, 2023
    Applicants: Airbus Operations GmbH, Airbus Operations (S.A.S.)
    Inventors: Francois TRANCHET, Timo WARNS
  • Method for calibration of a device for measuring a mass of fuel in a tank
    Patent number: 11579007
    Abstract: A method for calibrating a device for measuring a mass of fuel carried by an aircraft by: receiving a message containing a reference permittivity, a reference density and a reference volume, determining a first calibration coefficient as a function of the reference permittivity, determining a second calibration coefficient as a function of the reference volume, determining a third coefficient of calibration as a function of the reference density, determining a calibrated mass of fuel as a function of a determined height of fuel corrected as a function of the first calibration coefficient, a volume of fuel determined as a function of the corrected height and corrected as a function of the second calibration coefficient, and a mass of fuel determined as a function of the corrected volume and corrected as a function of the third calibration coefficient.
    Type: Grant
    Filed: December 17, 2019
    Date of Patent: February 14, 2023
    Assignee: Airbus Operations SAS
    Inventors: Emre Kanyilmaz, Alvaro Ruiz Gallardo
  • Method and device for managing the offtake of power produced by an auxiliary power unit of an aircraft and aircraft equipped with said power offtake management device
    Patent number: 11578700
    Abstract: A method for managing the offtake of power produced by an auxiliary power unit of an aircraft. The method comprises a step of calculating a maximum capacity for offtake of mechanical power that the auxiliary power unit can provide to the aircraft, a step of determining an actual offtake of mechanical power taken off by a first mechanical power offtake system of the auxiliary power unit, a step of comparing the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, a step of optimizing the offtake of mechanical power which step, based on the comparison of the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, determines at least one corrective action. A device for managing the offtake of power produced by an auxiliary power unit of an aircraft and an aircraft including such a device are provided.
    Type: Grant
    Filed: August 2, 2021
    Date of Patent: February 14, 2023
    Assignees: Airbus Operations SAS, Airbus SAS, Airbus Operations S.L.
    Inventors: Didier Poirier, Etienne Foch, Guillaume Alix, Nicolas Chauvet, Paul-Emile Roux, Souhaib Boukaya, Marcos Javier Chibrando
  • Bumper with an integrated marking cell
    Patent number: 11577795
    Abstract: A vehicle bumper comprising at least one part made of resilient material, in the interior of which there is provided at least one marking fluid cell with an opening to the exterior. The opening is closed by a closure device which, under the effect of a pressure applied with a determined intensity, can open up the opening, allowing the marking fluid to access the exterior of the cell through which the marking fluid can flow, and also comprising a securing element configured to secure the at least one part on the vehicle.
    Type: Grant
    Filed: May 1, 2019
    Date of Patent: February 14, 2023
    Assignee: Airbus SAS
    Inventors: Julien Charles, Guillaume Ferrer
  • Method and system for optimizing the arrangement of a set of aircraft parts on a plate
    Patent number: 11579585
    Abstract: Method and system for optimizing the arrangement of a set of aircraft parts on a plate. The system includes a selection module which selects, from a set of data on the material of the set of parts and a set of geometric data associated with the set of parts, part grouping criteria including at least one optimized plate thickness value, an optimization module for optimizing the arrangement of the set of parts on a plate as a function of the part grouping criteria, cutting criteria and optimization criteria and a transmission module generating and transmitting, to a user system, optimization data representative of the optimization of the arrangement of the set of parts. The system makes it possible to take account of the parameters linked to the dimensions of the plate to optimize the arrangement of the set of parts.
    Type: Grant
    Filed: October 20, 2020
    Date of Patent: February 14, 2023
    Assignees: Airbus (S.A.S.), Airbus Operations (S.A.S.)
    Inventors: Laurent Huquet, Perrine Dupuy, Samuel Drouvroy, Christophe Louat
  • Aircraft passenger seat oxygen system
    Patent number: 11572178
    Abstract: An onboard oxygen system for aircraft includes an oxygen source, a regulator connected to the oxygen source, and an oxygen mask connected to the regulator. The oxygen source is stored in a cavity in a passenger seat armrest. The oxygen mask is stored in a mask storage compartment attached to the armrest. The oxygen mask is deployed for use through an opening in the mask storage compartment.
    Type: Grant
    Filed: September 23, 2021
    Date of Patent: February 7, 2023
    Assignee: Airbus Americas, Inc.
    Inventors: Mark Griffin, Jonathan Adiong, Joyce Tan
  • Controlling aircraft wheel brakes
    Patent number: 11572045
    Abstract: A method for controlling the application of aircraft wheel brakes including: controlling the application of a first wheel brake of an aircraft and a second wheel brake of the aircraft in dependence upon a determined relationship to control the time taken for the first wheel brake and the second wheel brake to reach respective specified temperatures. The relationship is determined between a first cooling characteristic of the first wheel brake, according to which the first wheel brake cools when in a first retracted position within the aircraft, and a second cooling characteristic of the second wheel brake, according to which the second wheel brake cools when in a second retracted position within the aircraft.
    Type: Grant
    Filed: September 5, 2019
    Date of Patent: February 7, 2023
    Assignee: Airbus Operations Limited
    Inventors: Matthew Gadd, David Reid
  • Front engine attachment system for an aircraft engine, having rod systems with two rods
    Patent number: 11572184
    Abstract: A front engine attachment system for an engine of an aircraft, the front engine attachment system having an engine pylon having, in its front part, a frontal part having an attachment wall that has a front face, and a front engine attachment having a beam that is fixed against the front face and to which is fixed, on either side of a median plane, a rod system, wherein each rod system is fixed to the beam in an articulated manner by at least one first connection point, and is configured to be fixed to a front part of the engine in an articulated manner by at least one second connection point. Such a front engine attachment system thus has rod systems having two rods, allowing the shape of the rods and the shape of the beam to be simplified.
    Type: Grant
    Filed: May 19, 2020
    Date of Patent: February 7, 2023
    Assignee: Airbus Operations SAS
    Inventors: Thomas Deforet, Rémi Lansiaux, Olivier Dubois, Jacky Puech
  • Method And Apparatus For The Additive Manufacture Of A Component Within A Receiving Unit Using A Powdery Material
    Publication number: 20230035834
    Abstract: A method for the additive manufacture of a component within a receiving unit using a powdery material wherein, in one step, the powdery material is introduced into the receiving unit via a feed unit. In a further step, an oscillation is applied to the powdery material introduced into the receiving unit. In a further step, the oscillation is applied over a period of time to the powdery material introduced into the receiving unit until a predetermined distribution of the powdery material within the receiving unit is achieved. In a further step, at least a part of the powdery material within the receiving unit is solidified after the predetermined distribution of the powdery material has been achieved. An apparatus for the additive manufacture of a component within a receiving unit using a powdery material is also described.
    Type: Application
    Filed: July 19, 2022
    Publication date: February 2, 2023
    Applicant: Airbus Operations GmbH
    Inventors: Konstantin Schubert, Johannes Born
  • Tank, In Particular For A Liquid Hydrogen Reservoir, Provided With Internal Rails For Putting An Equipment Module In Place
    Publication number: 20230036429
    Abstract: A tank, in particular for a liquid hydrogen reservoir, provided with internal rails for putting an equipment module in place, includes a central portion provided with a wall, and at least one rail and preferably a plurality of rails, each of the rails being integrated in the wall of the central portion of the tank so as to be accessible from inside the tank, such rails allowing easier integration and fastening of a module comprising equipment inside the tank, so as to simplify the manufacture and assembly of the tank.
    Type: Application
    Filed: July 25, 2022
    Publication date: February 2, 2023
    Applicant: Airbus Operations SAS
    Inventor: Damien Guilloteau
  • Tank, In Particular For A Liquid Hydrogen Reservoir, Provided With At Least One Dome Fixed By Way Of An Outer Welded Joint
    Publication number: 20230036707
    Abstract: A tank, in particular for a liquid hydrogen reservoir, provided with at least one dome fixed by way of an outer welded joint and having a central portion provided with at least one free end including a first connecting element and at least one dome provided with an open end including a second connecting element, the dome and the central portion being able to be joined together, the first connecting element and the second connecting element being configured to form, when the central portion and the dome are joined together, a protruding tab extending toward the outside of the tank and able to be welded to a protruding end, such a protruding tab making it possible in particular to join together the tank, this being done entirely from the outside of said tank, and to easily mount and dismount the dome, in particular without accessibility issues.
    Type: Application
    Filed: July 25, 2022
    Publication date: February 2, 2023
    Applicant: Airbus Operations SAS
    Inventor: Damien Guilloteau
  • Wing for an aircraft
    Patent number: 11565789
    Abstract: A wing for an aircraft includes a main wing, slat, and connection assembly movably connecting the slat to the main wing, wherein the slat is movable between a retracted position and an extended position. The connection assembly includes a guide rail and an elongate slat track extending along a track longitudinal axis between front and rear ends, the front end of the slat track fixedly mounted to the slat. A first roller unit is mounted to the rear end of the slat track engaging the guide rail. A roller bearing includes a second roller unit mounted to the main wing and engaging an engagement surface of the slat track. The slat track includes a slot extending through the slat track along the track longitudinal axis. The second roller unit includes a first roller element and a second roller element mounted on one common shaft for common rotation, and the common shaft proceeds through the slot.
    Type: Grant
    Filed: November 23, 2021
    Date of Patent: January 31, 2023
    Assignee: Airbus Operations GmbH
    Inventors: Bernhard Schlipf, Florian Lorenz, Stefan Bensmann, Dustin Shapi
  • Aircraft seat, aircraft seat arrangement having an aircraft seat, and aircraft having an aircraft seat arrangement
    Patent number: 11565817
    Abstract: An aircraft seat having a voltage supply connection assigned only to the aircraft seat and/or at least one data connection assigned only to the aircraft seat, a voltage supply unit assigned to the aircraft seat and having a voltage input for connection to an on-board voltage network of an aircraft and at least one voltage output, each connected to another of the voltage supply connections. A switching arrangement is assigned only to the aircraft seat and connected between the voltage output and the voltage supply connection and/or between the data connection and a data network. A control unit is assigned only to the aircraft seat and connected to the switching arrangement. An infrared reading device is connected to the control unit and assigned only to the aircraft seat to wirelessly receive infrared signals from an external infrared transmitting device.
    Type: Grant
    Filed: March 27, 2020
    Date of Patent: January 31, 2023
    Assignee: Airbus Operations GmbH
    Inventor: Uwe Donnig
  • Aircraft door sealing system and aircraft door arrangement
    Patent number: 11565786
    Abstract: An aircraft door sealing system comprises a resilient sealing element secured to an aircraft door arrangement first element and comprising a sealing lip extending from a sealing member. A rigid counter-bearing element is secured to an aircraft door arrangement second element and cooperates with the sealing element to seal a gap between the first and second elements. The counter-bearing element comprises a first portion cooperating with the sealing member and a second portion cooperating with the sealing lip. The sealing lip and the second portion are positioned relative to each other, and the sealing lip can be resiliently deformed, so that the sealing lip is applied to the second portion and a contact face between the sealing lip and the second portion is formed or increases, when an external pressure acting on an outer face of the sealing lip via the gap, exceeds a threshold value.
    Type: Grant
    Filed: October 23, 2019
    Date of Patent: January 31, 2023
    Assignee: Airbus Operations GmbH
    Inventor: Jens Heeren
  • Vertical tail unit for flow control
    Patent number: 11565795
    Abstract: A vertical tail unit (7) for flow control including: an outer skin (13) in contact with an ambient air flow (21), wherein the outer skin (13) extends between a leading edge (23) and a trailing edge (25), and surrounds an interior space (29), and wherein the outer skin (13) includes a porous section (31) in the area of the leading edge (23), a pressure chamber (15) arranged in the interior space (29), wherein the pressure chamber (15) is fluidly connected to the porous section (31), an air inlet (17) provided in the outer skin (13), wherein the air inlet (17) is fluidly connected to the pressure chamber (15), wherein the air outlet (19) is fluidly connected to the pressure chamber (15). The vertical tail unit (7) has reduced drag and an increased efficiency because the air inlet (17) is formed as an opening (35) in the outer skin (13) at the leading edge (23).
    Type: Grant
    Filed: March 25, 2021
    Date of Patent: January 31, 2023
    Assignee: Airbus Operations GmbH
    Inventor: Thomas Heuer
  • SYSTEMS AND METHODS FOR DETECTING SURFACE CONDITIONS
    Publication number: 20230023670
    Abstract: The present disclosure generally pertains to systems and methods for detecting surface conditions using multiple images of different polarizations. A system in accordance with the present disclosure captures images having different polarizations and compares the images to evaluate surface conditions of an area, such as a runway, landing pad, roadway, or taxiway on which a vehicle is expected to land or otherwise travel. In some cases, a surface hazard, such as water, ice, or snow covering a surface of the area, may be detected and identified. Information indicative of the surface conditions may be used to make control decisions for operation of the vehicle.
    Type: Application
    Filed: December 23, 2019
    Publication date: January 26, 2023
    Applicant: A^3 by Airbus, LLC
    Inventors: Arne Stoschek, Cedric Cocaud