AIRBUS OPERATIONS SAS

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Technologies

Intl Class Technology # of Patents Rank
 
 
 
B64C AEROPLANES; HELICOPTERS 2183
 
 
 
B64D EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS1622
 
 
 
G06F ELECTRIC DIGITAL DATA PROCESSING 146188
 
 
 
G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES 746
 
 
 
G01C MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY 6925
 
 
 
G08B SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS 4336
 
 
 
F02K JET-PROPULSION PLANTS 318
 
 
 
1207 AIRCRAFT AND SPACE VEHICLES264
 
 
 
H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION 23153
 
 
 
G06G ANALOGUE COMPUTERS 2221

Top Patents (by citation)

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Recent Publications

Publication # Title Filing Date Pub Date Intl Class
2014/0081,482 METHOD AND DEVICE FOR AUTOMATICALLY MANAGING THE SPACING OF AT LEAST ONE FOLLOWING AIRCRAFT BEHIND AT LEAST ONE TARGET AIRCRAFTSep 11, 13Mar 20, 14[G05D]
2014/0072,775 METHOD FOR PRODUCING A PROFILE THAT HAS A RE-ENTRANT ANGLE IN A COMPOSITE MATERIAL FROM A STACK OF LAYERS OF FIBRESAug 29, 13Mar 13, 14[B32B]
2014/0064,877 ASSEMBLY OF TWO PARTS MADE OF COMPOSITE MATERIALAug 28, 13Mar 06, 14[F16B]
2014/0042,803 UnknownNov 16, 12Feb 13, 14[H02J]
2014/0037,400 Assembly Comprising A Device For Locking A FasteningAug 06, 13Feb 06, 14[F16B]
2014/0033,224 METHOD FOR MONITORING THE COORDINATED EXECUTION OF SEQUENCED TASKS BY AN ELECTRONIC CARD COMPRISING AT LEAST TWO PROCESSORS SYNCHRONIZED TO ONE AND THE SAME CLOCKJul 24, 13Jan 30, 14[G06F]
2014/0033,225 METHOD FOR MONITORING THE COORDINATED EXECUTION OF SEQUENCED TASKS BY AN ELECTRONIC CARD COMPRISING AT LEAST TWO PROCESSORS SYNCHRONIZED TO TWO DIFFERENT CLOCKSJul 24, 13Jan 30, 14[G06F]
2014/0001,284 Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamberOct 03, 12Jan 02, 14[F02K]
2013/0333,857 HEAT EXCHANGER INCORPORATED INTO A WALL OF AN AIRCRAFTAug 20, 13Dec 19, 13[B64D]
2013/0334,365 AIRCRAFT WITH REDUCED ENVIRONMENTAL IMPACTAug 22, 13Dec 19, 13[B64C]

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Recent Patents

Patent # Title Filing Date Issue Date Intl Class
8,689,644 Device for detecting shocks on a structureMar 15, 12Apr 08, 14[H01H, G01B, G01N, G01L]
8,694,234 System onboard an aircraft connected with a flight planJan 27, 11Apr 08, 14[G08G]
8,694,747 Method and device for loading and executing instructions with deterministic cycles in a multicore avionic system having a bus of which the access time is not predictableJun 02, 10Apr 08, 14[G06F]
8,684,301 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelleApr 28, 09Apr 01, 14[B64D]
8,684,312 Method and system for checking the formation of ice on an aircraft in flightApr 08, 11Apr 01, 14[B64F, B64D]
8,688,419 Method for predicting the operational reliability of an aircraft systemJan 02, 08Apr 01, 14[G06G]
8,677,625 Process for repairing a damaged area of an aircraft fuselageMay 10, 07Mar 25, 14[B21D]
8,677,755 Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said methodNov 12, 08Mar 25, 14[F02C]
8,677,764 Aircraft propulsion assembly comprising hot air bleed systemsDec 22, 08Mar 25, 14[F02C]
8,678,314 Impact resistant and damage tolerant aircraft fuselageDec 29, 11Mar 25, 14[B64C]
8,678,317 Installation assembly including a fixation rail for attaching devices in an aircraftJun 21, 11Mar 25, 14[B64C]
8,682,507 Method and system for determining flight parameters of an aircraftJul 31, 12Mar 25, 14[G06F]
8,683,266 Methods and devices for configuration validation of a complex multi-element systemMar 02, 11Mar 25, 14[G06F]

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Expired/Abandoned/Withdrawn Patents

Patent # Title Filing Date Issue/Pub Date Intl Class
2011/0117,773 AIRCRAFT CONNECTOR ASSEMBLYOct 13, 05May 19, 11[H01R]
2010/0301,163 STAIRWAY FOR AN AIRCRAFTMay 30, 08Dec 02, 10[B64D, B64C]
2010/0289,671 AIRCRAFT VIEWING SYSTEMNov 15, 07Nov 18, 10[G08B]
2010/0060,636 METHOD AND DEVICES FOR MODELING TEMPLATES OR STENCILS FOR THREE-DIMENSIONAL OBJECTS WITH NON-DEVELOPABLE SURFACES AND FOR ASSISTING THE TRANSFER OF TWO-DIMENSIONAL MOTIFS ONTO THOSE OBJECTSApr 23, 08Mar 11, 10[G06T]
2010/0047,985 METHOD FOR FABRICATING A SEMICONDUCTOR DEVICE WITH SELF-ALIGNED STRESSOR AND EXTENSION REGIONSAug 19, 08Feb 25, 10[H01L]
2010/0026,988 ONLINE SENSOR FOR MONITORING CHEMICAL CONTAMINATIONS IN HYDRAULIC FLUIDSDec 15, 07Feb 04, 10[G01J]
2009/0326,738 DEVICE FOR AIDING TO TAKE A DECISION CONCERNING THE ABILITY OF AN AIRCRAFT TO START A FLIGHTMay 19, 08Dec 31, 09[G06F]
2009/0314,899 STRUCTURAL ELEMENT OF AN AIRCRAFTJul 30, 07Dec 24, 09[B64D]
2009/0294,577 DEVICE FOR AUTONOMOUS MOVEMENT OF AN AIRCRAFT ON THE GROUNDJun 28, 07Dec 03, 09[B64C]
2009/0245,968 NUT ATTACHING AN AIRCRAFT WINDSHIELD AND DEVICE FOR ATTACHING AN AIRCRAFT WINDSHIELD INCORPORATING SAID NUTFeb 26, 07Oct 01, 09[F16B]
2009/0246,531 PROCESS FOR THE PRODUCTION OF A STIFFENER THAT IS SCOOPED OUT IN THE SHAPE OF AN OMEGA AND CORE FOR THE PRODUCTION OF A STIFFENER THAT IS SCOOPED OUT IN THE SHAPE OF AN OMEGAMar 30, 09Oct 01, 09[B32B]
2009/0217,868 DEVICE FOR SUPPLYING PASTY MATERIALOct 25, 05Sep 03, 09[B08B, B05C]
2009/0199,536 PROCESS FOR REVERSING THE THRUST PRODUCED BY A PROPULSION UNIT OF AN AIRCRAFT, DEVICE FOR ITS IMPLEMENTATION, NACELLE EQUIPPED WITH SAID DEVICEJun 28, 07Aug 13, 09[F02K]
2009/0113,979 EXPANSION TOOL FOR COLD EXPANSION OF HOLESApr 20, 07May 07, 09[B21D]
2009/0084,039 COMMUNICATION FLAP AND AIRCRAFT PROVIDED WITH ONE SUCH FLAPJun 06, 06Apr 02, 09[E06B]
2008/0283,172 Method for Repairing a Composite Structural Outer SkinSep 27, 06Nov 20, 08[B29C]
2008/0226,818 Method for Through Repair of a Composite Structure Comprising Three Skins and Two Core LayersSep 27, 06Sep 18, 08[B32B]
2008/0228,454 Method and Device for Simulating Bending of a TubeJul 18, 06Sep 18, 08[B21D, G06G]
2008/0217,468 MAST FOR AN AIRCRAFT NACELLE INCORPORATING MEANS FOR LIMITING THE APPEARANCE OF VIBRATIONS, IN PARTICULAR IN CERTAIN FLIGHT REGIMES, AT A HIGH MACH NUMBER AND LOW LIFTMar 06, 08Sep 11, 08[B64D]
2008/0210,811 Aircraft Engine UnitMay 23, 06Sep 04, 08[B64D]

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