The report contains ten-year analysis with the following sections
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airbus operations | 25284 |
airbus france | 2458 |
airbus deutschland | 1752 |
airbus | 996 |
airbus uk | 656 |
airbus espana, s.l. | 340 |
eads deutschland | 195 |
ehjrbas dojchland | 135 |
airbus (s.a.s.) | 126 |
airbus defence and space | 121 |
airbus france | 972 |
airbus deutschland | 722 |
airbus operations | 460 |
airbus uk | 246 |
airbus | 178 |
airbus espana, s.l. | 132 |
ehjrbas dojchland | 23 |
eads deutschland | 17 |
airbus espana | 11 |
evonik roehm | 5 |
airbus operations | 2268 |
airbus | 72 |
airbus defence and space | 40 |
airbus (s.a.s.) | 38 |
airbus france | 18 |
hydac technology | 8 |
airbus group india private | 8 |
eads deutschland | 7 |
airbusgroup | 5 |
airbus military | 3 |
Title of patent family (most common patent title) |
Family members |
Filing year |
---|---|---|
landing gear drive systems | 37 | 2012 |
wing tip device | 37 | 2010 |
braided composite spar | 32 | 2013 |
aircraft nacelle including hot air discharge means | 31 | 2007 |
electronic card able to execute a command originating from a simulation system and a com… 🛈 | 26 | 2007 |
lining shell carrying a main load and structural component having at least one lining sh… 🛈 | 26 | 2010 |
system and method for controlling an aircraft cooling system | 24 | 2009 |
flight management system of an aircraft | 24 | 2013 |
landing gear drive system flexible interface | 23 | 2013 |
aircraft having a force transmission element between a cabin structural element and a pr… 🛈 | 23 | 2006 |