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Airbus Sas patents


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

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


Revised speed advisory for an aircraft during flight based on holding time

A method including obtaining real-time data, wherein the real-time data is at least one of data associated with aircrafts in and around an airport, real-time weather information, and runway unavailability at the airport. The real-time data is analyzed. ... Airbus Sas

Flight parameter measuring device with optical deformation sensors carried by the radome of an aircraft

A device for measuring at least one flight parameter such as the airspeed, the sideslip angle or the angle of attack, or any other parameter dependent thereon, of an aircraft including a radome, including systems for measuring the deformation of the radome wall due to forces exerted by the air on the radome and a computer for computing from deformation measurements obtained by the systems the required flight parameter or parameters. The systems include at least one optical fiber carried by the radome provided with bragg gratings, each fiber including a plurality of bragg gratings distributed over a length of the fiber so as to distribute the bragg gratings over the radome when the fiber is installed.. ... Airbus 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 repairing a radome, wherein the radome comprises a composite panel exhibiting a double curvature forming a dome, the panel comprising at least one damaged zone, comprises the steps of closing an interior space of the panel using a cap to form a repair chamber. ... Airbus Sas

Weighing device and system for determining the weight and the center of gravity of an aircraft

A device for weighing aircraft includes a weighing platform configured to receive a undercarriage leg of the aircraft and to generate weighing signals, a first calculation unit configured to calculate weighing information from the weighing signals generated by the weighing platform, a communication unit configured to transmit to a central device and to receive signals including at least one signal representing the weighing information calculated by the calculation unit, and a ground rolling unit configured to move the weighing platform over a surface.. . ... Airbus 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 threshold: determining a distance between the probe and a structural component discontinuity point; recording a data set comprising at least the distance between the probe and the discontinuity point, together with a data element corresponding to the probe emission angular direction, c) automatically searching for data sets corresponding to characteristic discontinuity points, and consequently establishing a correspondence between the probe emission angular directions and an angular reference frame linked to the component; d) based on the recorded data sets, automatically determining the discontinuity point positions; e) determining a dimensional characteristic of a crack based on the discontinuity point positions.. . ... Airbus Sas

System and method for 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. ... Airbus Sas

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 the guide rail and movable along the guide rail and comprises at least one connecting element which is movable between first and second operating positions wherein the connecting element, in its first operating position, is arranged such that the vehicle is positionable under a load deposited onto the at least one row of rollers and, in its second operating position, is arranged such that it interacts with the load so as to connect the load to the vehicle such that the load is entrained by the vehicle when the vehicle is moved along the guide rail.. ... Airbus Sas

Device for locking a moving element such as an aircraft door and aircraft equipped with said locking device

A locking device which includes a hook and a dual control for locking the hook. The dual control includes a first shaft and a second shaft. ... Airbus Sas

Aircraft air conditioning system with a reduced process air demand

An aircraft air conditioning system comprising an air conditioning unit adapted and configured to be supplied with compressed process air and to generate cold fresh air, a mixer adapted and configured to mix the cold fresh air from the air conditioning unit with recirculation air recirculated from an aircraft region to be air conditioned, an air outlet adapted and configured to direct mixed air from the mixer into the aircraft region, a first sensor adapted and configured to detect an actual temperature in the aircraft region, a second sensor adapted and configured to detect a temperature of the mixed air directed into the aircraft region, and a control unit adapted and configured to control an operation of the air conditioning unit in dependence on a difference between the temperature of the mixed air directed into the aircraft region and the actual temperature in the aircraft region.. . ... Airbus Sas

System and method for determining weight of freight units and baggage

This relates to a system and a method for determining weight of freight units and baggage. Such a system comprises a unit load device (uld), an internal system of the unit load device (uld) and a digital memory unit, wherein the internal system is configured for retrieving individual identification and weight data of items within the unit load device (uld), for calculating a gross weight of the unit load device (uld) by summing the individual weight data of the items together with empty weight data of the unit load device (uld) and for storing a list of all identified items based on the identification data as well as the calculated gross weight of the unit load device (uld) in the digital memory unit.. ... Airbus Sas

Towing vehicle for maneuvering an aircraft and for supplying pressurized air to an aircraft during the taxiing phase before takeoff

A mobile vehicle for supplying pressurized air to an aircraft, the vehicle being configured to tow the aircraft during its movements on the ground and including a pneumatic supply system configured to supply pressurized air to the aircraft, the pneumatic supply system being manually connectable to a high-pressure connector of the aircraft and remotely disconnectable from the connector.. . ... Airbus Sas








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