Learn more

MOTOREN TURBINEN UNION

Overview
  • Total Patents
    206
About

MOTOREN TURBINEN UNION has a total of 206 patent applications. Its first patent ever was published in 1967. It filed its patents most often in France, Germany and United Kingdom. Its main competitors in its focus markets engines, pumps and turbines, mechanical elements and environmental technology are ROLLS ROYCE, ARMSTRONG SIDDELEY MOTORS LTD and ROLLS ROYCE 1971 LTD.

Patent filings in countries

World map showing MOTOREN TURBINEN UNIONs patent filings in countries
# Country Total Patents
#1 France 98
#2 Germany 30
#3 United Kingdom 21
#4 United States 21
#5 Italy 16
#6 Japan 13
#7 China 5
#8 Sweden 1
#9 Taiwan 1

Patent filings per year

Chart showing MOTOREN TURBINEN UNIONs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Herrmann Bruno 4
#2 Hagemeister Klaus 2
#3 Riemerschmid Fritz 2
#4 Geruharuto Herupuringu 2
#5 Armin Doelker 2
#6 Maier K 2
#7 Hainritsuhi Furantsu Baueru 2
#8 Manfureeto Shuraupitsutsu 2
#9 Greune C 2
#10 Hackl F 2

Latest patents

Publication Filing date Title
JPS53134107A Inspection device of touching process of rotative member and fixed member of fluid machinery
GB1539302A Helicopter propulsion systems
GB1509488A Air-cooled radiator assembly
DE2642044B1 DEVICE FOR DETERMINING THE STATIC AND / OR DYNAMIC AXIAL THRUST OF A FIXED BEARING
GB1535247A Engine ventilation system
US4043883A Electrolytic precision drilling process
DE2620762B1 GAP SEAL FOR FLOW MACHINERY, IN PARTICULAR GAS TURBINE JET ENGINES
DE2554685A1 CONTAINER FOR GAS TURBINE ENGINES, IN PARTICULAR GAS TURBINE JETS
DE2543813B1 ROTATING DEVICE FOR A BLADE RUNNER OF A FLOW MACHINE
DE2540537B1 GAS TURBINE JET ENGINE FOR DRIVING AND CONTROLLING AN AIRPLANE
GB1510196A Rotor wheel for high-speed turbo-machines
DE2457231B1 IMPELLER FOR A FAST RUNNING TURBO MACHINE
FR2118716A6 Crack detector for highly stressed components
US3748854A Lift engine
US3751909A Turbojet aero engines having means for engine component cooling and compressor control
US3760590A Device for metering ignition fuel to the ignition unit of an afterburner associated with a turbojet engine
FR2083846A5 Gas turbine rotors and blades assembled by electron bombardment - welding - with efficient assembly cooling means
FR2095451A5 Gas centrifuge molecular pump mfr - on thread cutting lathe with die plate angled relative opposed roller tool
FR2095450A5 Assembly of two articles - using a connecting wire
DE2028966A1 VEHICLE DRIVE