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DAIMLER BENZ AEROSPACE AIRBUS

Overview
  • Total Patents
    279
About

DAIMLER BENZ AEROSPACE AIRBUS has a total of 279 patent applications. Its first patent ever was published in 1987. It filed its patents most often in Germany, EPO (European Patent Office) and United States. Its main competitors in its focus markets transport, environmental technology and electrical machinery and energy are EADS AIRBUS GMBH, JAMES PARK ASSOCIATES LTD and LIAONING TONGXINYUAN TECH CO LTD.

Patent filings per year

Chart showing DAIMLER BENZ AEROSPACE AIRBUSs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Kirma Safa 21
#2 Schumacher Markus 16
#3 Scherer Thomas Dr Ing 12
#4 Muin Andrew 9
#5 Lutzer Wilhelm Dipl Ing 8
#6 Roessner Bernd 8
#7 Vogg Guenter 8
#8 Schliwa Ralf 6
#9 Kallies Guenter 6
#10 Sprenger Wilfried 6

Latest patents

Publication Filing date Title
WO9916638A1 Adjustable seat, especially for transport systems
US5875998A Method and apparatus for optimizing the aerodynamic effect of an airfoil
DE19745621C1 Method for de-icing of aircraft
DE19743907C1 Wing mounting for aircraft gas turbine
DE19743909A1 Aircraft seat
DE19733934C1 Installation for reusing exhaust heat from cooker-cooler appliance in passenger aircraft
JPH1133308A Apparatus for purifying working fluid
DE19728595C1 Air injector for aircraft air conditioning gas monitoring
DE19726418A1 Heating conductor connection system
DE19726419A1 Heating conductor connection system in an aircraft
DE19721461A1 Process for drying paints on metallic or non-metallic individual parts or assembled assemblies of any structure
DE19719922C1 Device for influencing a root flow
DE19719915A1 Fork link for an empennage connection
DE19718610C1 Composite aircraft wing member manufacture incorporating suction holes to enhance laminar flow
DE19716181C1 Perforated carbon fibre reinforced plastic sheet esp. for laminar flow aircraft wings
DE19716182C1 Perforated carbon fibre reinforced plastic sheet esp. for laminar flow aircraft wings
DE19715597A1 Inflatable emergency slide to overcome the height difference between an aircraft exit and a standing area
DE19715529C1 Composite sandwich structure for use in structural components of aircraft
DE19713373C1 System for supporting manoeuvring of aircraft on ground
DE19712180A1 Connection element for plastic components