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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

Component configurator for generating variants of a component to be installed

Disclosed here is a component configurator that generates variants of an aircraft component to be installed. The component configurator includes a detection unit that detects a characteristic of the component, and that determines an available free space for an installation of the component in an installation environment. ... Airbus Sas

Jet engine nacelle having a reverser flap

A nacelle comprising a fixed cowl and a movable cowl movable in translation, a window delimited by the fixed cowl and the movable cowl, a reverser flap movable in rotation and a drive mechanism coordinating the movements of the reverser flap with those of the movable cowl. The drive mechanism comprises two bearings fixed to the nacelle, for each bearing, a lever arm with one end movable in rotation on the bearing and one end articulated on the reverser flap, for each lever arm, a rail comprising a straight portion and a curved portion, for each lever arm, a rod with one end articulated on the lever arm, and for each rail, a slider that is movable in translation on the rail and is articulated to one end of the rod.. ... Airbus Sas

Air input structure for an aircraft nacelle

An air input structure includes an air input lip and a front reinforcement frame placed inside the air input lip. The front part of the air input lip has a plurality of segments distributed angularly along the leading edge of the air input lip, two adjacent segments being separated by an intermediate part having an excess thickness. ... Airbus Sas

Machine tool with an assembly configuration with a cantilevered tool

A machine tool for carrying out operations on a part includes a longitudinal rail, a transverse arm, a module for connection between the transverse arm and the longitudinal rail, the module being fitted in translation on the longitudinal rail, a tool which is supported by the transverse arm, and a retention unit which is arranged at one end of the transverse arm, and includes at least one sucker. The machine tool has an assembly configuration—in which the retention unit and the tool are positioned respectively on both sides of the longitudinal rail, such that the tool is fitted cantilevered relative to the longitudinal rail. ... Airbus Sas

Safeguarding arrangement

A safeguarding arrangement for restricting the movability of at least one transport container storable or stored in a support structure receptacle. The transport container may be used for transporting goods, for example, in an aircraft, and may be stowed in the aircraft's galley area as a trolley. ... Airbus Sas

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

02/16/17 / #20170045394

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

02/02/17 / #20170029136

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

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009


This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. is not affiliated or associated with Airbus Sas 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 Sas with additional patents listed. Browse our Agent directory for other possible listings. Page by