new TOP 200 Companies filing patents this week

new Companies with the Most Patent Filings (2010+)




  

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 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Airbus Operations Sas-related inventors




Date Airbus Operations Sas patents (updated weekly) - BOOKMARK this page
03/09/17Aircraft rear portion comprising a vertical stabilizer having a box-section structure including a lower portion accommodated in the fuselage
03/09/17High assurance segregated gateway interconnecting different domains
03/02/17Aircraft engine unit comprising an improved front engine attachment
03/02/17Aircraft attitude indicator device
02/09/17Interface device for the connection and the passage of an electric route through an airtight wall of an aircraft
02/02/17Method for repairing a composite-material panel of an aircraft and tool for implementing said method
01/26/17Rear door of a landing gear box comprising an air passage orifice and a closure member of the latter
01/19/17Methods and control systems for controlling a drive system of an aircraft
01/12/17Braking control system for an aircraft
01/12/17Aircraft steering system controller
01/12/17Data processing unit for aircraft undercarriage performance monitoring
01/05/17System for electrically connecting cabin equipment of an aircraft to a control system and to at least one electrical power supply source of the aircraft
01/05/17Systems and methods for providing optimized taxiing path operation for an aircraft
12/29/16Method for eddy current testing
12/29/16System and locating impacts on an external surface
12/22/16Device and moving cargo
12/08/16Aircraft landing gear longitudinal force control
11/03/16Aircraft steering system
09/22/16Method and device for assisting the piloting of an aircraft during a parabolic flight
09/08/16Tool-holder fixed to a workpiece
08/11/16Method and control of a steerable landing gear
08/04/16Propulsion assembly incorporating a turbojet and a mounting pylon enabling a new distribution of the forces between the turbojet and the wing
06/23/16Removable auxiliary power device for aircraft and aircraft adapted to use at least one such device
06/16/16Control an aircraft when taxiing
06/16/16Systems and methods for providing optimized taxiing path operation for an aircraft
06/09/16Device for checking a pressurized testing tool for a fluid circuit of an aircraft
06/02/16Aircraft fuselage frame
06/02/16Avionics networks
05/26/16An aircraft including an engine attachment with a control surface
05/05/16Safety device for an extension socket
04/07/16Device for managing the storage of data
02/18/16Methods, device and evaluating electrical current threat effects at joints
01/28/16Method and device for determining an operational distance of an unspecified termination segment of an aircraft flight plan
01/21/16Differential braking of aircraft landing gear wheels
12/31/15Aeroplane equipped with an internal escape hatch having a double opening controller
12/31/15Aeroplane equipped with an internal escape hatch incorporating a pressure regulating system
12/24/15Aircraft propulsion assembly comprising at least one brush seal resistant to high-temperature
10/29/15Assembly for an aircraft comprising a moveable access panel
10/22/15Latching system for securing two components
10/22/15Landing gear force and moment distributor
09/10/15Device for determining navigation parameters of an aircraft during a landing phase
07/23/15Method and system for automatically modifying a lateral flight plan of an aircraft
07/09/15Method and device for guiding an aircraft during a low level flight
06/25/15Method for producing a central wing box
05/14/15Connection device for means of airplane
05/14/15Electrical energy distribution network in a transport vehicle, such as an aircraft, and an electrical installation in an aircraft
04/30/15Method and device for automatically detecting an incorrect measurement of a total temperature on an aircraft
04/23/15Method and device for revising a low-altitude flight phase of a flight path of an aircraft
03/19/15Electric flight control an aircraft
08/14/14Method for machining a through-hole in a component and machining device for implementing the said method
07/31/14Aircraft cockpit, in particular the front portion of an aircraft cockpit
07/17/14Mounting device for aircraft supply systems
06/26/14Flight data recorder
06/19/14Fibre laying machine comprising a roller with pivoting rings
06/19/14Electronics structure comprising at least one barrier impermeable to fine particles
05/29/14Aircraft nacelle comprising a reinforced connection between an air intake and a means of propulsion
05/22/14Passive device for generating a film of cold air in contact with an outer surface of an aircraft
05/01/14Connector for securing double skin pipework and assembly obtained
03/13/14Method for producing a profile that has a re-entrant angle in a composite material from a stack of layers of fibres
03/06/14Assembly of two parts made of composite material
02/13/14Unknown
02/06/14Assembly comprising a device for locking a fastening
01/30/14Method for monitoring the coordinated execution of sequenced tasks by an electronic card comprising at least two processors synchronized to one and the same clock
01/30/14Method for monitoring the coordinated execution of sequenced tasks by an electronic card comprising at least two processors synchronized to two different clocks
01/02/14Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber
Patent Packs
12/19/13Heat exchanger incorporated into a wall of an aircraft
11/07/13Overpressure door for an aircraft
09/26/13Machining tool for an aircraft fuselage frame
09/19/13Sealing device and method
09/19/13Method and device for optimizing data updates in operationally approved software applications of aircraft
09/12/13Method for obtaining a composite material part incorporating a tensioning step of the filaments and tool for its implementation
09/12/13Method of manufacturing a curved profile made of composite material from a rectilinear preform of fiber plies
09/12/13Method of manufacturing a part made of composite material and tool for the implementation thereof
09/12/13System and end-of-life processing of an airframe
08/29/13Aircraft engine pylon aft aerodynamic fairing
08/22/13Method and device for stiffener protection, and corresponding composite panel
08/01/13Device for carrying out tests on at least one fluid circuit of an aircraft
08/01/13Method for disassembly of two elements welded by ultrasound and element able to be welded by ultrasound to another element to the implementation of said method
07/25/13Method of calculating dynamic pressure at the level of an aircraft surface
07/18/13Wall made from a composite material reinforced so as to limit the spread of a crack in a direction
Patent Packs
07/11/13Bleeding system
07/11/13Method and device for driving at least one landing gear wheel of an aircraft by means of a wheel motor
06/27/13Method, apparatus and computer program product for determining the strain induced at a selected point in a stiffened panel structure in response to a load, taking into account one or more out of plane (oop) effects
06/13/13Substitution device for aircraft engine
06/13/13Method for producing an acoustic treatment panel
06/13/13Headrest for an aircraft pilot's seat and seat comprising a such headrest
06/13/13Method and device for automatically monitoring on an aircraft an identification code of a ground station of a navigation system
06/06/13Device and assembling two shell elements made from a composite material
05/30/13Cabling of an aircraft circuit breaker panel
05/30/13Interactive dialog device between an operator of an aircraft and a guidance system of said aircraft
05/02/13Electrical harness equipped with a device to space its electrical conductors at the level of a partition passage
05/02/13Energy protection device for an aircraft
05/02/13Method and device for controlling engine speed of an aircraft during a take-off
04/25/13Aircraft nacelle comprising a hot air supply device for a panel combining acoustic and frost treatments
04/25/13Method for adjusting the doors of a landing gear bay, and associated door
04/18/13Nacelle for a power plant with a variable-area fan nozzle
04/04/13Process for the destruction of a blind fastener and device for its implementation
04/04/13Ventilation system, air blowing and extraction circuits of such a system, as well as an aircraft avionics bay
03/28/13Conversion method and system
03/07/13Connection system and simulator using such a connection system
02/07/13Fastening device particularly suitable for the fastening between an air intake and an engine of an aircraft nacelle
02/07/13Fastening device particularly suitable for the fastening between an air intake and an engine of an aircraft nacelle
01/17/13Pressurised hot air duct of an aircraft equipped with a device for detecting air leakage
01/17/13Process for the production of a double-curved panel
01/03/13Spacer adjustable in length
12/20/12Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air
12/20/12Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structure
12/20/12Air intake of an aircraft nacelle that incorporates a reinforced lip with a defrost system by joule-effect
11/29/12Method for pointing a plurality of predetermined locations inside a structure and corresponding pointing system
11/15/12Method for manufacturing a part of a composite material and part thus obtained
Social Network Patent Pack
11/15/12Method and device for aiding the piloting of an aircraft during an intermediate approach phase of a descent
11/08/12Connecting device particularly adapted for the connection between an air intake and an engine of an aircraft nacelle
10/18/12Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together
10/04/12Device for connecting an air leak detection system to a sleeve that envelops a pressurized air hose of an aircraft
10/04/12Air inlet of an aircraft nacelle including optimized frost treatment
10/04/12Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means
09/27/12Panel for the acoustic treatment with a progressive thickness
09/20/12Process for manufacturing a part made of composite material that comprises at least one radius of curvature
09/20/12Process for the production of a profile made of composite material fibers that has a half-nail-head or nail-head cross-section
08/23/12Frame for an opening provided in an aircraft fuselage
Patent Packs
08/16/12Panel for acoustic treatment comprising a junction between two parts and process for the reparation of a panel for acoustic treatment
08/02/12Stiffened structure integrating an opening
06/21/12Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes
04/19/12Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
04/05/12Cable securing device
03/15/12Aircraft nacelle comprising a reinforced outer wall
03/01/12Aircraft nacelle including an optimised acoustic processing system
01/12/12Method for realization of an aircraft structure and resulting structure
01/12/12Aircraft including a fuel valve and a control actuator fastened to the valve
01/05/12Expansion tool and cold expansion of holes
12/01/11Aircraft including an undercarriage motor
11/10/11Method for producing a concave-shaped in particular u-shaped piece in a composite material and device for carrying out the same
10/27/11Process for manufacturing a piece that is made of composite material and device for its implementation
09/22/11Method of making a core comprising an envelope containing granular and/or powdery products, device and core obtained
09/22/11De-icing device comprising means for detection of a leakage in a hot air supply system
07/21/11Fuse link device between a mobile part and a fixed part of an aircraft nacelle
07/14/11Device for connecting an air inlet with an aircraft nacelle actuator assembly
06/23/11Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle
06/16/11Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment
06/16/11Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle
06/09/11Aircraft nacelle incorporating a device for protecting an access flap for a locking system
06/09/11Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
06/02/11Aircraft nacelle that incorporates a thrust reversal device
05/19/11Acoustic treatment panel with integral connecting reinforcement
05/19/11Device for shrouding an aircraft nacelle
05/19/11Device for shrouding an aircraft nacelle
04/28/11Method for producing a stiffener on a surface of an element to be stiffened
03/10/11Method of preparing the connection between two fuselage sections of an aircraft
03/10/11Rest module with a first partial module with direct access to a possible second partial module
01/27/11Device for the production of a composite material piece that comprises smoothing panels with sliding junctions and process for the production of smoothing panels with sliding junctions
Patent Packs
12/30/10Air outlet system for aircraft leading edge
12/16/10Aircraft nacelle including hot air discharge means
11/25/10Method of producing a structural part made from a thermosetting resin by drawing
11/11/10Aircraft propulsion assembly comprising hot air bleed systems
10/14/10Wing mounting
10/14/10Device for the production of a composite material part integrating a drainage system
10/07/10Aircraft nacelle including an optimised ice treatment system
08/19/10Method and device for concentrating messages for the integration simulation of components
07/22/10Coating for acoustic treatment that integrates the function of hot-air treatment of frost
07/22/10Method and device for communication by address virtualization for the integration simulation of components
06/10/10Method and device for detecting non-regression of an input/output system in a simulation environment
05/06/10Sail wing aircraft which includes an engine mounted on a pylon
04/01/10Device for the manufacturing of a piece of composite materiel with complex shape
03/25/10System for managing the heat fluxes of an aircraft
02/25/10System for attaching an engine to the structure of an aircraft, such as a sail wing aircraft







ARCHIVE: New 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. Freshpatents.com is not affiliated or associated with Airbus Operations 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 Operations Sas with additional patents listed. Browse our Agent directory for other possible listings. Page by FreshPatents.com

###




';