AIRBUS IND has a total of 27 patent applications. Its first patent ever was published in 1980. It filed its patents most often in France, United States and EPO (European Patent Office). Its main competitors in its focus markets transport, computer technology and environmental technology are AERION CORP, DZYNE TECH INCORPORATED and ZHOU LIANGYONG.
# | Country | Total Patents | |
---|---|---|---|
#1 | France | 7 | |
#2 | United States | 5 | |
#3 | EPO (European Patent Office) | 4 | |
#4 | Canada | 3 | |
#5 | WIPO (World Intellectual Property Organization) | 3 | |
#6 | Australia | 2 | |
#7 | United Kingdom | 1 | |
#8 | Russian Federation | 1 | |
#9 | Ukraine | 1 |
# | Industry | |
---|---|---|
#1 | Transport | |
#2 | Computer technology | |
#3 | Environmental technology | |
#4 | Control | |
#5 | IT methods for management |
# | Technology | |
---|---|---|
#1 | Aeroplanes | |
#2 | Parachutes | |
#3 | Electric digital data processing | |
#4 | Climate change mitigation in transportation | |
#5 | Teaching materials | |
#6 | Data processing systems |
# | Name | Total Patents |
---|---|---|
#1 | Roeder Jean | 8 |
#2 | Eilts Torsten | 5 |
#3 | Emsters Peter | 5 |
#4 | Blomberg Richard D | 4 |
#5 | Fouillot Jean-Pierre | 4 |
#6 | Geering Leslie James | 3 |
#7 | Speyer Jean-Jacques | 3 |
#8 | Beteille Roger H | 2 |
#9 | Geering Leslie J | 2 |
#10 | Sallier Daniel | 2 |
Publication | Filing date | Title |
---|---|---|
FR2827055A1 | Method for struturing and managing the configuration of industrial products, in particular aircraft | |
FR2745260A1 | System and method for fast and reversible conversion of an aircraft between a passenger configuration and a freight configuration | |
FR2733335A1 | Method, device and system for estimating and predicting the evolution of a size as a function of time and of another reference size itself as a function of time | |
FR2698068A1 | Airplane and other powered aircraft with wings. | |
FR2649665A1 | LARGE CAPACITY FUSELAGE FOR AIRCRAFT | |
FR2615641A1 | Method for developing a statistical model for determining the workload of an aircraft pilot, resulting model, device for carrying out said method and applications of the model | |
CA1148522A | Fixed-wing aircraft with tandem supporting surfaces |