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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


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

A device includes a database including data related to obstacles, a first determination module for determining at least one obstacle intercepted by a direct flight path connecting an initial point to the target point, a second determination module for determining at least one lateral extreme apex of at least one... Airbus Operations S a s

Device, assisting the taxiing of an aircraft

In an aircraft including a cockpit, a unit for monitoring the situation of the aircraft and a radio communication unit, the device for aiding the ground rolling is configured to: acquire, from the monitoring unit, information the situation of the aircraft and determine predicted positions of the aircraft for a... Airbus Operations S a s

Method for manufacturing a component from composite material

A method for manufacturing a composite component from a plurality of plies of fibres embedded in a resin includes the following steps: forming a preliminary composite component by draping the plurality of fibre plies in a mould; laying up the preliminary composite component by stacking layers comprising at least one... Airbus Operations S a s

Method for masking a sound signal generated by an element of the skin of an aircraft

A masking method includes: a step of choosing a generating element which is part of the skin of an aircraft, a first step of measuring a fundamental frequency of a sound signal emitted by the generating element, a step of selecting a masking element which is part of the skin,... Airbus Operations S a s

Effector comprising a contact surface having an interface made of a ductile material

An effector includes at least one contact surface configured to bear against a face of a workpiece near a zone of the workpiece that is impacted by a tool supported by the effector. The contact surface includes at least one interface made of a ductile material interposed between the contact... Airbus Operations S a s

Waste separation device with separation magnetic filter

A device for separating waste includes a tank having a closed internal chamber, the device being provided with an inlet opening and an outlet opening that can be connected to a suction system. The internal chamber of the tank is provided with a magnetic filter making it possible to attract... Airbus Operations S a s

Aircraft comprising a clearance between an opening and a door which comprises an upstream edge with a sharp edge

An aircraft includes a clearance between an opening and a door. The clearance communicates with a cavity and is oriented in a direction intersecting a flow direction of an air flow to the outside of the aircraft in flight. The aircraft further includes an upstream edge and an upstream outer... Airbus Operations S a s

Aircraft exhibiting independent elevators

An aircraft includes a structure exhibiting a median plane XZ and including a fuselage, a fixed vertical stabilizer at the rear of the fuselage, an adjustable horizontal stabilizer rotatably mounted about a horizontal axis on a first section of the structure, and extending on either side of the median plane... Airbus Operations S a s

Aircraft strut comprising at least one lateral frame in lattice form and aircraft comprising said strut

An aircraft strut includes a primary structure which includes: a top stringer, a bottom stringer, at least one transverse frame which links the top stringer to the bottom stringer, a front end wall which links a front end of the top stringer to a front end of the bottom stringer,... Airbus Operations S a s

Method and device for assisting in the piloting of an aircraft in the approach to a landing runway with a view to a landing

A device includes a unit for defining evaluation criteria relating to the aircraft and to its flight, a unit for predicting an energy status of the aircraft at the end of a given segment of a flight trajectory, a unit for verifying whether at least one event will occur on... Airbus Operations S a s

Aircraft cockpit side console with articulated single-piece components

A side console for an aircraft cockpit includes a structure for mounting of an item of aircraft equipment and a complementary structure. The mounting structure and the complementary structure are formed of single-piece components articulated about an axis of articulation between a storage position in which the single-piece components are... Airbus Operations S a s

Acoustic panel for aircraft nacelle, and manufacturing the acoustic panel

An acoustic panel for an aircraft nacelle includes a cellular layer configured to trap noise, a backplate fixed to one surface of the cellular layer and a facesheet fixed to another, opposite, surface of the cellular layer. The facesheet includes a layer of a preimpregnated woven material containing weft yarns... Airbus Operations S a s

Aircraft flight management unit and monitoring such a unit

A flight management unit includes two guidance subsystems each including a flight management system, each of the flight management systems being configured at least to extract a flight plan from at least one navigation database, to construct a flight trajectory, and to compute guidance commands for the aircraft. The flight... Airbus Operations S a s

Method and device for assisting the piloting of an aircraft for energy management during an approach phase

The device includes a reception unit for receiving a target energy including a target altitude and a target speed, a computation unit for computing a target energy state relative to the target energy, a computation unit for computing an energy difference between a final energy state at a final position,... Airbus Operations S a s

Aircraft engine pylon

An aircraft engine pylon includes two side panels and an upper stringer and a lower stringer assembled to form a strut assembly extending in a longitudinal direction (AX) corresponding to the direction in which the aircraft is moving and an internal reinforcement structure including a plurality of reinforcements. The pylon... Airbus Operations S a s

Method for controlling an offset between two stops and tool for controlling an offset between two stops

A tool for controlling an offset between two stops, includes: a body which includes an extension with an end configured to abut against one of the stops, a sliding rule that is configured to slide in a longitudinal direction in relation to the body and which has an end configured... Airbus Operations S a s

Shutter capable of obscuring light

A shutter for masking a surface allowing radiation, to pass at least partially. includes a panel and a skirt forming, with the panel, an enclosure which, when applied to the surface, prevents the passage of at least a determined radiation, and at least one partial vacuum-based fixing system for temporarily... Airbus Operations S a s

Measurement device with single control circuit

A measurement device can be attached to an outer wall of a movable object or of a stationary object arranged in a flow of air in order to measure physical quantities. The measurement device includes a mounting which has recesses having an opening leading to the outside in which sensors... Airbus Operations S a s

Actuator system for aircraft control surface

An actuator system includes an actuator which is configured to generate a loading on a control surface, as a function of an actuation order received, a command unit of the actuator, which is configured to compute an actuation order of the actuator, a reception element for receiving a current value... Airbus Operations S a s

Method and device for automatic management of an actuator controlled by a servo-valve

The device for automatic management of an actuator controlled by a servo-valve, includes a sensor for measuring the actual value of a parameter at the output of the actuator for a given control command, a computation unit for computing a theoretical value of said parameter, by applying the control command... Airbus Operations S a s








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