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PUBLICHNOE AKTSIONERNOE OBSHCHESTVO UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE PAO UMPO

Overview
  • Total Patents
    28
  • GoodIP Patent Rank
    57,528
About

PUBLICHNOE AKTSIONERNOE OBSHCHESTVO UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE PAO UMPO has a total of 28 patent applications. Its first patent ever was published in 2016. It filed its patents most often in Russian Federation. Its main competitors in its focus markets engines, pumps and turbines and measurement are TURBEC AB, ALM DEV INC and HANS HOLZWARTH.

Patent filings in countries

World map showing PUBLICHNOE AKTSIONERNOE OBSHCHESTVO UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE PAO UMPOs patent filings in countries
# Country Total Patents
#1 Russian Federation 28

Patent filings per year

Chart showing PUBLICHNOE AKTSIONERNOE OBSHCHESTVO UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE PAO UMPOs patent filings per year from 1900 to 2020

Focus industries

Top inventors

# Name Total Patents
#1 Kuprik Viktor Viktorovich 6
#2 Uzbekov Andrej Valerevich 5
#3 Kikot Nikolaj Vladimirovich 4
#4 Dontsov Sergej Nikolaevich 4
#5 Kiselev Andrej Leonidovich 4
#6 Chepkin Viktor Mikhajlovich 4
#7 Privalov Vitalij Nikolaevich 4
#8 Zelikin Yurij Markovich 3
#9 Tereshko Anton Geroldovich 3
#10 German Georgij Konstantinovich 3

Latest patents

Publication Filing date Title
RU2623616C1 Method of turbojet engine testing
RU2623631C1 Axial flow compressor stage guide vanes
RU2623605C1 Control method of aircraft jet turbine bypass engine
RU2623675C1 Resilient damping support of turbomachine rotor
RU2623703C1 Elasticity-damper support with adjustable stiffness
RU2627627C1 Aero bypass turbofan engine control method
RU2627750C1 Method of determining dynamic disbalance of aeronautical gas turbine engine rotor
RU2623849C1 Aeronautic bypass turbofan engine control method
RU2623674C1 Gas-turbine engine rotor support angular contact
RU2623627C1 Axial flow compressor stage guide vanes
RU2623618C1 Joint of compressor rotors and gas turbine engine turbine
RU2627748C1 Bypass gas turbine engine cooled turbine
RU2620737C1 Control method of aircraft jet turbine engine
RU2623704C1 Fan valve unit
RU2623705C1 All-track nozzle
RU2623609C1 Turbojet engine rotating nozzle
RU2634490C1 Quasi-distributed fiber-optical information-measuring system
RU2623622C1 Cooled high-pressure turbine
RU2614456C1 Adjustable guide device of axial compressor of turbomachine
RU2620735C1 Method of determining gasifier capacity