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Airbus Operations s a s patents


Recent patent applications related to Airbus Operations s a s. Airbus Operations s a s is listed as an Agent/Assignee. Note: Airbus Operations s a s may have other listings under different names/spellings. We're not affiliated with Airbus Operations s a s, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Airbus Operations s a s-related inventors


Processor comprising a plurality of computation cores

A processor including computation groups, each computation group including computation cores, the processor being capable of simultaneously implementing a plurality of applications, each application being implemented by a computation core and possibly requiring a read-mode or write-mode access to an external memory connected to the processor. At least one core,... Airbus Operations s a s

Method and device for identification of a recipient aircraft of an audio communication

A method and device for identification of a recipient aircraft of an audio communication. The device includes at least one reception unit, for example a VHF radio or an HF radio, for receiving an audio message on board the aircraft, a transcription unit for transcribing the audio message received into... Airbus Operations s a s

Process for manufacturing an acoustic panel reinforced by at least one thermoplastic composite layer

A process for manufacturing an acoustic panel including at least one acoustically resistive layer, at least one cellular structure and a reflective wall. The process includes steps of depositing the parts of the acoustic panel made of thermosetting composite, depositing a film made of thermoplastic resin that is miscible with... Airbus Operations s a s

Processor designed for a deterministic switched ethernet network

Multiple-core processor to be connected, by way of communication ports, to a deterministic switched Ethernet network using virtual links to which items of equipment are connected, the processor including clusters each including cores, wherein at least one cluster of the processor implements a switch function that makes it possible to... Airbus Operations s a s

Generation of application codes from a formal specification

System and method to generate automatically a compact application code suitable for taking advantage of the intrinsic power of processors. The system can generate the application code executable by a processor from a formal specification associated with an application, the formal specification including operators, and the system including an analyzer... Airbus Operations s a s

Piping system with leak detection

A piping system includes a first and a second inner tube assembled end to end and a hot fluid detector. For each inner tube, a first peripheral tube into which the inner tube is introduced and fixed. For each first peripheral tube, a second peripheral tube into which the first... Airbus Operations s a s

Method for the structural analysis of panels consisting of an isotropic material and stiffened by triangular pockets

A method for dimensioning of panels stiffened by triangular pockets that make it possible to take into account aeronautical specifics and more particularly the stresses that are admissible for the different types of buckling and the calculations of adapted reserve factors is presented. The method relates to dimensioning of a... Airbus Operations s a s

Device for transferring information from an avionics system of an aircraft to an independent computer

A device and system for transferring information from an avionics system of an aircraft to an independent computer. The device can be embedded onboard an aircraft for transferring information arising from an avionics system from the aircraft to a computer independent of the avionics system. The device includes at least... Airbus Operations s a s

Support for a pipe

A support for a pipe. The support includes a body and at least one base configured so as to be in contact with and connected to a fixing surface. The support includes an orifice for receiving the pipe. Two inner members are disposed within the body. A first inner member... Airbus Operations s a s

Embedded communications network of a vehicle

An embedded communications network of a vehicle is a deterministic switched Ethernet network using virtual links, including a set of subscribers and a set of switches. A first subscriber is connected to a first switch and a third switch, and a second subscriber is connected to a second switch and... Airbus Operations s a s

Method for making an electroluminescent marking on an exterior wall of an aircraft, marking tape comprising the electroluminescent marking, and aircraft comprising the electroluminescent marking

A method for making an electroluminescent marking on an exterior wall of an aircraft, including a step of superpositioning of layers designed or configured to produce the electroluminescent marking on a first face of a flexible backing distinct from the aircraft to obtain a marking tape and a step of... Airbus Operations s a s

Method of producing a micro-channeled material at atmospheric pressure

A micro-channeled material is fabricated from a bundle of metal-plated polymer fibers by a process wherein the polymer fibers are heated to a first temperature and pyrolyzed in the presence of an inert gas at atmospheric pressure.... Airbus Operations s a s

Method and device for assisting the initiation of a flare maneuver of an aircraft during a landing of the aircraft

A method and device for assisting initiation of a flare maneuver of an aircraft during a landing. The device includes an acquisition unit for acquiring current values of flight parameters of the aircraft, including the current height of the aircraft with respect to the ground, a computation unit for computing... Airbus Operations s a s

Predicting failures in an aircraft

The disclosure herein proposes identifying precursors to all the phenomena which can have an impact on the service use of an aircraft. It relates to a system for predicting failures in an aircraft, including a processor configured to analyze a current behavior of at least one flight parameter of the... Airbus Operations s a s

Flight management system for an aircraft and securing open world data using such a system

A flight management system for an aircraft and method of securing open world data using such a system. The flight management system includes at least two flight management computers including one computer termed active forming part of an active guidance subsystem configured to supply data for guiding the aircraft. Another... Airbus Operations s a s

Method making it possible to identify the proximity of a wake turbulence and to generate a report relative to that proximity

A method to identify the proximity of a wake turbulence and to generate a report relative to that proximity. A method implemented by an aircraft comprising a processor makes it possible to identify the proximity of a wake turbulence and to generate a report relative to that proximity. The method... Airbus Operations s a s

Structure ensuring attenuation of acoustic waves and thermal exchange

A structure ensuring acoustic attenuation of a flow of a first fluid and heat exchange between a first fluid and a second fluid. The structure includes a first wall which is perforated, a second wall, and a plurality of intermediate walls extending between the first wall and the second wall.... Airbus Operations s a s

Device for reducing aerodynamic disturbances in the wake of an aerodynamic profile by variable-distribution blowing on the top side and the underside

A device for reducing aerodynamic disturbances in the wake of an aerodynamic profile. The device comprises a first air ejection nozzle arranged on the top side of the profile and a second air ejection nozzle arranged on the underside of the profile. A first blowing chamber is fluidically connected to... Airbus Operations s a s

Human machine interface for displaying information relative to the energy of an aircraft

A human machine interface linked to the throttle lever of an aircraft used to control the energy of an aircraft is disclosed. The HMI has upper part, which corresponds to the forward stroke of the lever, and a lower part, which corresponds to the rearward stroke of the lever. An... Airbus Operations s a s

Collision avoidance for an aircraft formation relative to an intrusive aircraft

Collision avoidance method and device for an aircraft formation relative to an intrusive aircraft. The device manages a collision avoidance for an aircraft formation, relative to an aircraft external to the aircraft formation, the aircraft formation comprising a lead aircraft and at least one following aircraft, the device comprising a... Airbus Operations s a s

Collision avoidance a trailer aircraft of an aircraft formation relative to an intruder aircraft

A collision avoidance method and system for a trailer aircraft of an aircraft formation relative to an intruder aircraft. The collision avoidance system is embedded in a trailer aircraft of an aircraft formation and it is intended to avoid a collision relative to at least one aircraft external to the... Airbus Operations s a s

Onboard communication network of an aircraft and communication system

An onboard communication network of an aircraft and communication system. The onboard communication network of an aircraft is a deterministic switched Ethernet network including a set of subscribers and at least one switch. It uses virtual links, each defined between a transmitting subscriber and one or more receiving subscribers. The... Airbus Operations s a s

Aircraft control comprising an improved pedal

An aircraft control of the rudder bar type, which includes a box-shaped pedal, a support, a first rotation shaft connecting the pedal to the support with a first rotation axis, a first pivot connection configured to allow the pedal to pivot about the first rotation axis relative to the support,... Airbus Operations s a s

Method and device for displaying a symbology for assisting the piloting of an aircraft during a landing phase

A method and device for displaying a symbology for assisting the piloting of an aircraft during a landing phase. The display device allows a crew to anticipate or avoid emission of a runway overrun warning, able to be emitted by a piloting assistance unit. The display device includes a display... Airbus Operations s a s

Universal joint with simplified structure

A universal joint includes a first band and a second band which are separated by a slot, are cylindrical and coaxial with one another with respect to a common axis, and further includes a first torsion bar, whose ends are joined to the first band, and a second torsion bar... Airbus Operations s a s

Universal joint with simplified structure

A universal joint includes a first band and a second band which are separated by a slot, are cylindrical and coaxial with one another with respect to a common axis, a first stiffener whose ends are joined to the first band, and a second stiffener whose ends are joined to... Airbus Operations s a s

Control system enabling comparison between two character strings and installing a new configuration in an aircraft

A control system and method enabling comparison of first and second character strings, the control system comprising a first source of information supplying the first string and a second source of information embedded in an aircraft and supplying the second string. A first processing module can model the first character... Airbus Operations s a s

Aircraft high-lift device equipped with at least one differentiated coupling system

An aircraft high-lift device comprising a kinematic chain connected to flaps, the kinematic chain comprising a plurality of shafts connected by coupling systems. This high-lift device comprises at least one differentiated coupling system different from the non-differentiated coupling systems, the differentiated coupling system being configured to be coupled to an... Airbus Operations s a s

System for assisting in the guiding of an aircraft on the ground

A system for assisting in guiding of an aircraft maneuvered by an aircraft tractor on the ground, the system including at least one projection device including a laser generating a laser beam fixed to an anchor point of the fuselage of the aircraft. A fixing mechanism is configured to fix... Airbus Operations s a s

Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box

In order to reduce congestion of attachments between an aircraft engine and its attachments, an engine assembly is provided, the primary structure of the device of which includes a structural cover surrounding the engine and connected on a central box, the cover including an outer skin interiorly delimiting a secondary... Airbus Operations s a s

Electric generator for an aircraft, comprising a ventilation device with controlled opening

An electric generator for an aircraft includes a sealed casing, a rotating shaft, and a ventilation device, which has at least one orifice configured to place a chamber positioned inside the rotating shaft in communication with the exterior of the sealed casing. For at least one orifice, an inertia sealing... Airbus Operations s a s

Method for aligning a first hole of a first part with a second hole of a second part and kit for its implementation

A method enabling two holes belonging to two parts to be aligned relies on use of a tool, comprising a body, having a first outer surface which gradually wanders from a longitudinal axis of the body as it extends from a first end of the body, and a hollow part... Airbus Operations s a s

Door of a blended body aircraft installed in the leading edge and with lateral edges parallel to the plane of symmetry of the aircraft

A flying wing or blended body aircraft comprising at least one door installed in the leading edge of the aircraft. The lateral edges of the door extend each in a plane parallel to the plane of symmetry of the aircraft, when the door is closed. It reduces the aerodynamic penalties... Airbus Operations s a s

Aircraft brace housing a fluid transfer line

An aircraft including a wing, a fuselage and at least one brace extending between the wing and the fuselage. The brace houses at least one fluid transfer line between the wing and the fuselage, such as an engine air bleed line, a hydraulic line or a fuel pipe. Use in... Airbus Operations s a s

Method and system for assisting the piloting of an aircraft in landing phase

The runway state determined on the ground by an aircraft and provided to the aircraft on approach does not make it possible to account for possible degradation of the runway occurring since the previous determination of that runway state. Updating of this runway state on the basis of a simple... Airbus Operations s a s

06/15/17 / #20170166297

Aircraft control comprising a pedal coupled to a cylinder and associated control device

An aircraft control comprises a mobile pedal and comprises a cylinder coupled to the pedal such that a displacement of the pedal according to at least a first direction reduces the volume of a first chamber of the cylinder. A control device comprises a fluid type bus system connecting two... Airbus Operations s a s

06/15/17 / #20170166300

Method and device for controlling coupled forward and aft doors of an aircraft landing gear bay

A system for the control of the door assemblies of a bay of a landing gear of an aircraft, that is retractile and is able to be deployed, the opening of the bay for the landing gear being able to be closed by a forward door assembly and an aft... Airbus Operations s a s

06/15/17 / #20170171112

Onboard communication network of a vehicle and subscriber of such a communication network

A subscriber of a deterministic Ethernet communication network using virtual links including a first receiver, a first transmitter, a first memory to record a configuration table relating to a set of virtual links that the subscriber can receive and/or retransmit. A processing unit is configured to implement at least one... Airbus Operations s a s

06/08/17 / #20170162067

System for assisting in managing the flight of an aircraft, in particular of a transport airplane, in a landing phase on a runway

A system for assisting in managing the flight of an aircraft in a landing phase. The system comprises a trajectory computation module for determining a trajectory of the aircraft, an interface module and an auxiliary computation module for computing an optimized ground slope, a display unit for allowing an operator... Airbus Operations s a s

06/08/17 / #20170162068

Method and device for estimating a lateral speed and a lateral position of an aircraft, during a phase where the aircraft is traveling on the ground

Method and device for estimating lateral speed and lateral position of an aircraft during a phase where the aircraft is traveling on the ground. The device includes a unit for determining an initial lateral position value, corresponding to lateral position with respect to axis of a runway when touching down... Airbus Operations s a s

06/01/17 / #20170152024

Device forming a trailing edge of an aerodynamic profile and comprising a blowing system

A device including a profiled member conformed to constitute an edge portion of an aircraft aerodynamic profile. The device includes a blower chamber to be pressurized and an air ejector nozzle making it possible to provide fluidic communication between the blower chamber and an external surface of the profiled member,... Airbus Operations s a s

06/01/17 / #20170152054

Method of controlling the thrust of the jets of an aircraft during the takeoff phase, control device and aircraft corresponding thereto

The disclosure herein relates to a method of controlling the thrust of the jets of a multi-jet aircraft, during the aircraft takeoff phase, which successively comprises a first step of controlling the jets to a first thrust level, until the aircraft reaches a first predetermined speed, and a second step... Airbus Operations s a s

05/18/17 / #20170137106

Structural assembly for an aircraft fuselage with double curvature including frames with an optimized orientation

In order to allow an aircraft fuselage structure to provide optimum resistance to pressurization loads in a fuselage region with a double curvature, the fuselage structure includes a circumferential frame oriented so that the web of the circumferential frame has an orientation close to the local normal to the skin... Airbus Operations s a s

05/11/17 / #20170131165

Method and device for monitoring the clamping of an assembly by a threaded fastener

A method of monitoring the clamping of an assembly by a threaded fastener. One element of the threaded fastener is rotated by a driver while the other is held stationary by a holding tool. The screwing torque and reaction torque of the holding tool are measured. Analyzing their evolution as... Airbus Operations s a s

04/20/17 / #20170107603

Friction adjustment interface between two parts made of nickel or nickel or cobalt-chromium alloy that are in relative motion against one another at high temperature

An adjustment interface inserted between a first part made of nickel or made of nickel alloy or made of cobalt-chromium alloy in relative motion with a second part made of nickel or made of nickel alloy or made of cobalt-chromium alloy. The interface includes a first adjustment layer on one... Airbus Operations s a s

04/13/17 / #20170100739

Tool and applying an anti-corrosion substance to an aircraft passenger seat rail

The disclosure herein relates to a tool for applying a corrosion-protection substance to a rail for securing seats in an aircraft. The tool comprises a component of elongate overall shape comprising a base configured to slide along the rail, and a rollers support connected to the base and comprising an... Airbus Operations s a s

04/06/17 / #20170096229

Aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other

In order to reduce the width of the attachment between the rear portion of an aircraft engine and its attachment pylon, an engine assembly attachment include an assembly of rear engine attachments comprising a first connecting rod laid out in a longitudinal and median vertical plane, a second connecting rod... Airbus Operations s a s

03/16/17 / #20170074750

Measuring air flows along a wall

A simple device for accurately measuring real-time air flows along a wall, and relating to a measuring device including an optical sensor configured to measure an illuminance distribution on a free surface of the optical sensor. A mobile member movably is mounted on the light sensor by partially covering its... Airbus Operations s a s

03/09/17 / #20170066077

Process for friction stir welding including a mobile counter-bearing

System for friction stir welding of two parts which includes a welding unit which includes at least one welding head fitted with a rotating pin and a counter-bearing unit which has a support surface to support the parts against a pressure exerted by the welding head, and wherein each welding... Airbus Operations s a s

03/09/17 / #20170066520

Integrated ribs for central wing box

A central wing box for an aircraft, including a top panel, a bottom panel, a front spar, a rear spar, and at least one secondary rib. A secondary rib includes two stiffeners, a first stiffener extending adjacent to the top panel and to one of the front spar and the... Airbus Operations s a s

03/02/17 / #20170061806

Method and device for automatically determining a runway state

An estimation unit including an element for computing an actual distance, representing the distance covered by the aircraft over at least one speed interval delimited between two speeds of the aircraft, the interval corresponding to rollout on a segment of the runway, for which the braking performance of the aircraft... Airbus Operations s a s

02/16/17 / #20170047983

Methods, systems, and computer readable media for managing aircraft radiofrequency communications

Methods, systems, and computer readable media for managing aircraft radiofrequency communications on board an aircraft are disclosed. In some aspects, a method can include determining at least one communication frequency, the at least one communication frequency corresponding to a communication center within a radio horizon of the aircraft, displaying the... Airbus Operations s a s

02/02/17 / #20170028520

Tool-support system

A tool-support system for working on holes of a surface. The tool-support system includes two rails fixed to the surface and having imprints regularly distributed over their length, and a mobile tool-support including a mobile optical system capturing an image of the surface. For each rail, at least one wheel... Airbus Operations s a s

02/02/17 / #20170032684

Method and system for assisting the guidance of an aircraft along a runway approach axis

A method and system for assisting guidance of an aircraft along a runway approach axis. The method includes acquiring a position deviation between a current position of the aircraft and the approach axis, determining an angle between a longitudinal axis of the aircraft and the approach axis, and determining a... Airbus Operations s a s

01/26/17 / #20170021939

Method and device for displaying at least one position indicator for an aircraft

A method and device for displaying at least one position indicator for an aircraft. The display device includes at least one unit for generating information for determining, during a flight of the aircraft, a control value representative of the movement by a first pilot of his joystick relative to at... Airbus Operations s a s

01/19/17 / #20170014936

Weld protecting device by gas diffusion

A weld protecting device by gas diffusion including several elements mounted one after the other and hinged to each other, and including a front element, intermediate elements mounted one after the other and behind the front element. A back element is mounted behind the last intermediate element, each element including... Airbus Operations s a s

01/19/17 / #20170018125

System, device and recording data in an aircraft

A system, device and method for recording data in an aircraft including a memory and a network interface through which it is connected to the network. This device is configured for acquiring information from the avionics communication network, and information relative to characteristic events relative to operation of the aircraft,... Airbus Operations s a s

01/12/17 / #20170008640

Flight management assembly for an aircraft and monitoring such an assembly

A flight management assembly for an aircraft and method for monitoring such an assembly. The flight management assembly includes two guidance systems each provided with a flight management system, the flight management systems being independent, each of the flight management systems carrying out at least one calculation of roll commands... Airbus Operations s a s

01/12/17 / #20170011638

Monitoring scheduled turnaround activities and alerting on time deviation of scheduled turnaround activities

A system for monitoring scheduled turnaround activities and alerting on time deviation from the scheduled turnaround activities is disclosed. The system includes a ground computing station system, an aircraft on-board system, a cloud, and user interface. The cloud is communicatively coupled to the ground station computing system and the aircraft... Airbus Operations s a s








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This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. Freshpatents.com is not affiliated or associated with Airbus Operations s a s in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for Airbus Operations s a s with additional patents listed. Browse our Agent directory for other possible listings. Page by FreshPatents.com

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