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Airbus Operations Sas patents


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

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


System for actuating a control surface of an aircraft

An actuating system comprising a hydraulic actuator provided with a cylindrical cavity containing a piston configured to slide within the cylindrical cavity and a rod. The piston separates the cylindrical cavity into a first actuating chamber and a second actuating chamber. A first servo valve comprises a sheath including a... Airbus Operations Sas

Method and device for determining the position of an aircraft in an approach for a landing

A device comprising a radar for taking at least one radar image of the terrain in front of the aircraft in a zone containing at least one characteristic pattern, the position of the characteristic pattern being known, an image processing unit for detecting, on the radar image taken by the... Airbus Operations Sas

Crocodile-type flight control surface for aircraft

A crocodile-type flight control surface comprising an upper foil flap, a lower foil flap, an actuating mechanism which guarantees the rotational displacement of each foil flap about a joint axis, either in the same direction or in different directions, and a locking mechanism alternatively adopting a locking position in which... Airbus Operations Sas

Method of automatic positioning of a seat

A method of automatic positioning a seat in an apparatus comprising two cameras located on either side of the seat, each one in a position able to acquire images of a face of a user seated on the seat. The seat comprises at least one motor, each motor acting on... Airbus Operations Sas

Aircraft engine mount comprising at least one transverse nut and aircraft comprising the said engine mount

An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house... Airbus Operations Sas

Method and system for aiding the ground rolling of an aircraft

In an aircraft comprising a cockpit comprising a display screen, a camera configured to acquire images of the environment of the aircraft, as well as a display management system, a ground rolling aid system configured so as to a) acquire several successive images of the environment of the aircraft via... Airbus Operations Sas

Method for repairing a radome using the radome as a heating chamber and tool for implementing same

A method and tool for repairing a damaged zone of an aircraft radome, using the actual radome itself as a heating chamber to avoid resorting to an autoclave and the removal of certain parts of the radome which cannot withstand the curing temperature needed for the repair. The method for... Airbus Operations Sas

Assembly for aircraft comprising engines with boundary layer propulsion by injection

In order to further benefit from the principle of boundary layer ingestion by engines of an aircraft assembly, the rear portion of the fuselage of this aircraft assembly includes a front portion which splits up into at least two distinct rear portions, spaced apart from each other, and each integrating... Airbus Operations Sas

Aircraft brake temperature measurement

A brake temperature sensing system for an aircraft including a sensor apparatus and an interrogation apparatus. The sensor apparatus includes a temperature sensor for attachment to a brake disc of an aircraft brake, and a relay for attachment to the brake. The temperature sensor is configured to wirelessly transmit a... Airbus Operations Sas

Method for monitoring the engines of an aircraft

A monitoring method, the purpose of which is, when a loss of power is detected in an aircraft engine, to generate an alarm in the form of a single message displayed on a display screen in the cockpit, in order to indicate if the level of damage suffered by the... Airbus Operations Sas

Method for adjusting the position of elements of a structure of an aircraft, and device for implementing same

A device for adjusting the position of structural elements of a structure of an aircraft, comprising a measurement tool for determining a value for the actual position of each structural element, a processing and calculation system for comparing each value of the actual position determined by the analysis system with... Airbus Operations Sas

Method and device for verifying a guidance signal

A verification method comprising a first step of measuring at least one position parameter of an aircraft and a first set of steps implemented after the flight of at least one aircraft, in an automatic and repetitive manner, comprising computing a geographical height of an aircraft with respect to the... Airbus Operations Sas

Display an aircraft

A display system for an aircraft cockpit comprises a display device configured to be secured to a user's head, a sensor to determine an orientation of the user's head, and a display computer. The computer is configured to control the display of information relating to the flight of the aircraft... Airbus Operations Sas

Method for optimizing the take-off parameters of an aircraft

A method for optimizing the take-off parameters of an aircraft. The aircraft comprises a system for automatically controlling the high lift devices at the moment when the wheels of the aircraft leave the ground. The method comprises a step of selecting a first configuration of the high lift devices at... Airbus Operations Sas

System and evaluating action capacities of an individual

A system for evaluating the action capacities of an individual comprising at least one measurement module, each measurement module being configured to produce at least one measurement point of a physiological parameter of the individual; a computation module configured to determine at least one set of measurement points representative of... Airbus Operations Sas

On-board system for evaluating the severity of a lightning strike

An on-board system for evaluating the severity of a lightning strike, intended to be installed in the interior of an airplane and connected to an avionic system of the airplane. The system comprises four devices, a master device and three slave devices, each device comprising a magnetic-field sensor. The devices... Airbus Operations Sas

Propeller for an aircraft turbo engine, including safety means for controlling blade angle of attack

In order to simplify the design of an aircraft turbo engine propeller while enhancing the safety function thereof related to control of the blade angle of attack, a propeller is provided comprising a secondary rotational coupling to couple in rotation, along the radial axis of the blade, the inner radial... Airbus Operations Sas

Aircraft engine assembly comprising a pylon leading edge incorporated with an annular row of unfaired after-guide vanes

To reduce the overall mass of an engine assembly for aircraft, this assembly comprises a part of the fuselage of an aircraft, a turbomachine comprising an unfaired propeller, together with an annular row of unfaired after-guide vanes located aft of the propeller and rotationally fixed in relation to a longitudinal... Airbus Operations Sas

Method for testing a structural component of a vehicle

A method for structural component crack testing comprising: a) identifying a structural component hole and inserting a probe thereinto; b) for different emission directions, automatically performing the following: b1) controlling a probe ultrasound beam emission; b2) measuring a probe signal; b3) if the measured signal amplitude is above a predetermined... Airbus Operations Sas

System and controlling the thrust of the engines of an aircraft

A system for controlling the thrust of the engines of an aircraft comprises a processing unit configured to receive an aircraft speed setting, to determine a control setting for at least one engine of the aircraft as a function of the speed setting and to transmit a setting to a... Airbus Operations Sas

Ground unit, aircraft and transmitting flight instructions from a ground unit to an aircraft

The transmission of flight instructions from a ground unit to an aircraft comprising an onboard system. The ground unit is configured to generate, on the basis of flight data intended for the aircraft, at least one optical symbol containing a flight instruction. The onboard system comprises an optical reader and... Airbus Operations Sas

Center for assisting the flight management of a plurality of aircraft

A center to assist flight management of a plurality of an entity's aircraft comprising a control unit and at least two stations and communication equipment configured to receive data signals and to transmit/receive audio signals to/from each aircraft. The control unit comprises a man-machine interface connected to a central unit,... Airbus Operations Sas

Communication the transmission of audio data signals from an aircraft cockpit to a ground station

A communication system installed in an aircraft, the system comprising a transmitter configured to transmit audio data signals to a ground recording station provided with memories for the recording of the data, at least one audio assembly per pilot of the aircraft for transmitting and receiving audio data signals, a... Airbus Operations Sas

Doors for an easy access to the pressurized housing of a flying wing, from the trailing edge

An aircraft of flying wing or blended wing body type comprising, for access to a pressurized housing, a non-pressurized door in the trailing edge of the aircraft and a pressurized door on the pressurized housing. The distance between the center of the pressurized door and a plane of symmetry of... Airbus Operations Sas

Unified floor and aircraft nose including such a floor, and incorporating such a nose

An aircraft nose floor comprising a grid structure formed by an interlacing of crosspieces and longitudinal elements. The crosspieces are parallel to one another and the longitudinal elements are parallel to one another and fastened to the crosspieces. The floor forms a unified module configured to be transported in one... Airbus Operations Sas

Unknown

A tooling making it possible to mount a module directly in an aircraft without making any modifications to the module. This tooling is made up of upper beams connected to the structure of the aircraft, lower beams secured to the module, lift elements connecting the lower beams to the upper... Airbus Operations Sas

Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box

In order to reduce the size of the attachment arrangement between an aircraft engine and its attachment device, an engine assembly is provided for which the primary structure of the attachment device includes a central box and two movable structural cowls. Further the arrangement for attaching the engine on the... Airbus Operations Sas

System and starting the engines of a twin-engine aircraft

A system and a method for the automatic starting of the engines of a twin-engine aircraft. When a first engine is made by the pilots of the aircraft to follow an automatic starting procedure, this engine follows the conventional four-phase starting cycle. The rotor of the high-pressure stage of the... Airbus Operations Sas

Control device of a communication system of an aircraft

The control device of a communication system of an aircraft having a predefined number of communication channels comprises a processing unit and one or more sets of buttons each associated with a communication channel. The number of sets of buttons is less than the predefined number of communication channels of... Airbus Operations Sas

Control device of a communication system of an aircraft

The control device of a communication system of an aircraft having a predefined number of communication channels comprises a processing unit and sets of buttons each associated with a communication channel and comprising a button for setting sound volume, a reception button and a transmission button. The number of sets... Airbus Operations Sas

Aircraft cell comprising a door opening in rectilinear translation

In order to simplify the connection of a door to the outer envelope of an aircraft cell, it is provided to dispose the door into a portion of the outer envelope having tilted sides, as is the case at the nose cones and the tail cones of conventional airplanes, and... Airbus Operations Sas

System for holding a forward pressure bulkhead via non-parallel rods attached to the floor

A zone provided between the forward pressure bulkhead in an aircraft and the floor. The nose section of the aircraft in which the flat surface pressure bulkhead including at least one transverse frame comprises at least two rods, of which one of the front ends is attached to the bulkhead... Airbus Operations Sas

Windshield with support rod

An aircraft windshield that improves pilot and co-pilot's perception of the outside world. The windshield includes a transparent panel held inside a structure of the aircraft, in which the upper part and the lower part are bridged so that the loads applied to the panel are (at least partially) diverted.... Airbus Operations Sas

Curvilinear rudder bar for an aircraft and aircraft comprising such a curvilinear rudder bar

The rudder bar includes two actuation arrangements, each provided with two pedals, each actuation arrangement having a frame provided with two rails arranged on either side of said frame and being in the form of a concave curve, and, associated with each one of said rails, a movable carriage, each... Airbus Operations Sas

Support pylon for a turbomachine, provided with a thermal protection element

A support pylon for an aircraft turbomachine having the overall shape of a box defined by lateral walls, at least one of the lateral walls having an external surface comprising a thermal protection element, the element being mobile as a result of a rise in temperature between a first, retracted... Airbus Operations Sas

06/15/17 / #20170167437

Jet engines and their arrangement in the rear section of an aircraft

A jet engine comprises at least three zones including an air intake zone and an exhaust zone. The axis of the air intake zone is not coincident with the axis of the exhaust zone of the engine, the engine as a result, having at least two intersecting axes and being... Airbus Operations Sas

06/08/17 / #20170158349

Method and system for aiding landing of an aircraft

A method for aiding the landing of an aircraft on a landing runway comprising the following steps implemented in an automatic manner by a processing unit: a) acquiring information relating to the landing runway; b) acquiring information relating to a current situation of the aircraft; f) determining a maximum roll... Airbus Operations Sas

06/08/17 / #20170162065

Method and system for aiding landing of an aircraft

A method for aiding the landing of an aircraft on a landing runway comprises the following steps implemented in an automatic manner by a processing unit: a) acquiring information relating to the landing runway; b) acquiring information relating to a current situation of the aircraft; c) determining, as a function... Airbus Operations Sas

06/08/17 / #20170162066

Method and system for aiding landing of an aircraft

A method for aiding the landing of an aircraft on a landing runway comprises the following steps implemented automatically by a processing unit: a) acquiring information relating to the runway; b) acquiring information relating to a current situation of the aircraft; i) determining a landing position of the aircraft on... Airbus Operations Sas

06/01/17 / #20170152052

Aircraft engine assembly comprising rear engine attachments in the form of shackles

An aircraft engine assembly including a set of rear engine attachments comprising a first shackle hinged on a bracket secured to the engine and on a bracket made as one piece with one of the two side panels, the shackle being oriented along a vertical direction, a second shackle hinged... Airbus Operations Sas

05/25/17 / #20170144175

System for applying a fluid to a surface

An application system for depositing a fluid product on a surface. The application system comprises a frame mounted on a locomotive system ensuring the displacement of the frame over the surface, a tank mounted on the frame and receiving the fluid product to be applied, and an application head fluidically... Airbus Operations Sas

05/11/17 / #20170129140

Forming tool of a preform in composite material and manufacturing a part in composite material using said tool

A forming tool of a preform made of composite material, the tool comprising at least one flexible element and at least a first and a second rigid plate connected to the flexible element and disposed on either side of the flexible element. The first and second rigid plates and the... Airbus Operations Sas

05/11/17 / #20170132942

Method and device for generating an optimum vertical path intended to be followed by an aircraft

A method and device for generating an optimum vertical path intended to be followed by an aircraft. The device comprises at least one database relating to fixed and moving obstacles, a data entering unit, a data processing unit implementing iterative processing to generate an optimum vertical path between an initial... Airbus Operations Sas

04/27/17 / #20170113425

Method for repairing an aircraft structure using deformable sheets

A method for repairing an aircraft structure made of composite material which comprises a damaged zone having at least one bend. The method comprises the stacking of at least two sheets of composite material, which each have a thickness allowing manual deformation thereof, a first sheet being applied to the... Airbus Operations Sas

04/20/17 / #20170106967

System for moving loads and cargo hold

A system for moving loads comprises a cargo hold floor, at least one row of rollers integrated into the floor, at least one guide rail in the floor and extending parallel to the at least one row of rollers, and a least one transport vehicle. The vehicle is received in... Airbus Operations Sas

04/20/17 / #20170108145

Support for a conduit

A support for a pipe which comprises a body which comprises a through-orifice for the pipe. The through-orifice has a diameter which is greater than an external diameter of the pipe. At least one base of the support is configured so as to be in contact with and connected to... Airbus Operations Sas

04/20/17 / #20170109946

Method and device for detecting oscillatory failures in an automatic position control chain of an aircraft control surface

A detection device comprising a first data processing unit configured to determine a first trend of the control surface control order as a function of time, the first trend being defined according to a reference parameter, a second data processing unit configured to determine at least one second trend of... Airbus Operations Sas

04/13/17 / #20170101195

Method for predicting temperatures which are tolerable by a component, a piece of equipment or an airplane structure

A method for predicting temperatures tolerable by a component, a piece of equipment or a vehicle structure. This method includes the steps of determining, for each piece of equipment, component or structure of the vehicle, such as an airplane, a temperature spectrum depending on a plurality of extrinsic parameters measured... Airbus Operations Sas

04/06/17 / #20170096230

Compartmentalized structure for the acoustic treatment and the de-icing of an aircraft nacelle and aircraft nacelle incorporating said structure

An acoustic structure for an aircraft nacelle which comprises an acoustically resistive substructure, at least one layer of cells and a reflective layer. The acoustic structure comprises at least one single-piece substructure which divides up the layer of cells and which incorporates elongated elements of a de-icing system.... Airbus Operations Sas

04/06/17 / #20170096238

Aircraft propulsion system having at least one anti-fire tank

A propulsion system comprising a nacelle substantially tubular around a longitudinal axis, having an inner wall extending from a front to a rear of the nacelle and by an outer wall, external of the inner wall, extending from the front to the rear of the nacelle, a turbojet comprising a... Airbus Operations Sas

03/30/17 / #20170092391

Method for mounting a sheath on a wire harness and a set comprising a sheath and a wire harness

The method for fitting a sheath on a cable harness includes a series of steps including determining the length of sheath to be used, mounting the sheath on a mounting tool of tubular shape, inserting the cable harness into the mounting tool, removing the mounting tool and arranging the sheath... Airbus Operations Sas

03/09/17 / #20170066518

Aircraft rear portion comprising a vertical stabilizer having a box-section structure including a lower portion accommodated in the fuselage

To optimize the structure of an aircraft tail section, an aircraft rear section comprises a fuselage section, a tail section, and a vertical stabilizer comprising a box-section structure which comprises a box-section upper part extending on the outside of the tail section, and a box-section lower part housed inside the... Airbus Operations Sas

03/09/17 / #20170070507

High assurance segregated gateway interconnecting different domains

A gateway having an architecture authorizing bidirectional communication between applications located in different domains and presenting a high assurance level of protection. The gateway interconnects a first and second domain. The gateway comprises an internal protocol, first and second protocol adapters hosted within the first and second domains and configured... Airbus Operations Sas

03/02/17 / #20170057652

Aircraft engine unit comprising an improved front engine attachment

An aircraft engine unit comprising an engine, a mast and an engine connection connecting the engine and the mast. The aircraft engine unit includes a front engine attachment of the engine connection which comprises at least one front rod connecting the primary structure of the mast and the core of... Airbus Operations Sas

03/02/17 / #20170057656

Aircraft attitude indicator device

An aeroplane attitude indicator device includes a mobile rod which includes a first end connected by a link to a support fastened to the aeroplane and a second end to which is connected a moving body, at least one actuator for controlling the motions of the rod, and a system... Airbus Operations Sas

02/09/17 / #20170040764

Interface device for the connection and the passage of an electric route through an airtight wall of an aircraft

An interface device that includes a plastic part including at least one through-opening in a longitudinal direction, the plastic part being adapted to be fixed in an airtight manner into an opening in the wall. At least one metal shaft is arranged and fixed in the through-opening. The metal shaft... Airbus Operations Sas

02/02/17 / #20170028655

Method for repairing a composite-material panel of an aircraft and tool for implementing said method

A method and a tool for repairing a composite-material panel of an aircraft with at least one repair part made of composite material without using an autoclave. The repair method includes the steps of preparing the panel, placing at least one repair part made of composite material on the second... Airbus Operations Sas

01/26/17 / #20170021919

Rear door of a landing gear box comprising an air passage orifice and a closure member of the latter

A landing gear box of an aircraft comprising a front door with independent opening and a rear door with opening mechanically connected to the landing gear, including an orifice in the rear door provided with a closure member and a drive mechanism allowing movement of this closure member independently of... Airbus Operations Sas

01/19/17 / #20170015410

Methods and control systems for controlling a drive system of an aircraft

A method of controlling a drive system of an aircraft. The drive system comprised a drive motor arranged to drive at least one wheel of an aircraft landing gear. A power signal indicative of a power level for the drive motor and a speed signal indicative of a rotation speed... Airbus Operations Sas

01/12/17 / #20170008503

Braking control system for an aircraft

A braking control system for an aircraft having braking wheels, the braking control system being configured to receive input of signals from sensors representative of a plurality of measured aircraft parameters, and to output a plurality of brake commands to brakes associated with the braking wheels, wherein the braking control... Airbus Operations Sas

01/12/17 / #20170008619

Aircraft steering system controller

A controller for an aircraft steering system, the controller being configured to receive a steering input representative of a desired direction of travel of a steerable nose landing gear, and to receive one or more force-based inputs representative of lateral forces acting upon the nose landing gear, wherein the controller... Airbus Operations Sas

01/12/17 / #20170011568

Data processing unit for aircraft undercarriage performance monitoring

A data processing unit for monitoring the performance of at least one undercarriage which is used for braking and/or steering an aircraft, wherein the data processing unit is configured to: receive data representative of operating characteristics of the undercarriage(s) and use that data to calculate a maximum achievable braking force... Airbus Operations Sas

01/05/17 / #20170001583

System for electrically connecting cabin equipment of an aircraft to a control system and to at least one electrical power supply source of the aircraft

A system for electrically connecting a piece of cabin equipment of an aircraft to a control system and to at least one electrical power supply source of the aircraft. The connection system comprises a host interface module to which the control system and the at least one electrical power supply... Airbus Operations Sas

01/05/17 / #20170004715

Systems and methods for providing optimized taxiing path operation for an aircraft

A taxiing path optimization system is provided for computing a taxi path of an aircraft using available taxi routes of a corresponding airport. An interaction means management unit manages interactions between a user and the taxiing path optimization system using an interactive device for inputting a taxi clearance. An aircraft... Airbus Operations Sas








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