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ROLLS-ROYCE DEUTSCHLAND LTD & CO KG

Overview
  • Total Patents
    341
  • GoodIP Patent Rank
    5,610
  • Filing trend
    ⇩ 73.0%
About

ROLLS-ROYCE DEUTSCHLAND LTD & CO KG has a total of 341 patent applications. It decreased the IP activity by 73.0%. Its first patent ever was published in 2005. It filed its patents most often in Germany, EPO (European Patent Office) and United States. Its main competitors in its focus markets engines, pumps and turbines, environmental technology and transport are ROLLS ROYCE DEUTSCHLAND LTD & CO KG, SAFRAN AIRCRAFT ENGINES and ROLLS ROYCE PLC.

Patent filings per year

Chart showing ROLLS-ROYCE DEUTSCHLAND LTD & CO KGs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Clemen Carsten 28
#2 Todorovic Predrag 25
#3 Venter Gideon 16
#4 Beier Jürgen 16
#5 Weinert Markus 11
#6 Schreiber Karl 11
#7 Thies Robert 10
#8 Leymann Tobias 9
#9 Heinze Kay 9
#10 Beier Juergen 8

Latest patents

Publication Filing date Title
US2020263553A1 Cooled turbine rotor blade
DE102019203125A1 Electrical contact arrangement, power converter and aircraft
DE102019105442A1 Method for producing an engine component with a cooling duct arrangement and engine component
DE102019105233A1 Method and device for calibrating strain gauges
DE102019202760A1 Sealing sleeve for a stator of an electrical machine
DE102019202466A1 Combustion chamber assembly with shingle component and base bodies aligned with one another, each carrying a fastening element, as well as manufacturing process
DE102019104143A1 Device, planetary gear with a device and method for producing a rotationally fixed connection between two components
DE102019104194A1 Gas turbine engine and aircraft with a gas turbine engine
DE102019202072A1 Engine assembly with cover part
GB201616759D0 Accessory gearbox for a gas turbine engine
WO2017046250A2 Structural element of an aircraft part and method for manufacturing a structural element
DE102016215030A1 Turbofan engine with a lying in the secondary flow channel and a separate end element panel
DE102016114930A1 Device of a turbomachine for actuating an adjusting device and turbomachine with such a device
DE102016215036A1 Turbofan engine with overpressure flap on a fairing located in the secondary flow channel
DE102016114394A1 Device of a turbomachine for separating oil from an air-oil volume flow
DE102016113568A1 Method for producing a tandem vane segment
DE102016113030A1 Gas turbine and method for protecting a gas turbine during shaft breakage
GB201612099D0 A geared gas turbine engine
DE102016212649A1 Burner seal of a gas turbine and method for its production
DE102016112604A1 Engine nacelle and method for influencing flows in an engine nacelle