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PUBLICHNOE AKTSIONERNOE OBSHCHESTVO ODK UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE

Overview
  • Total Patents
    12
  • GoodIP Patent Rank
    145,596
  • Filing trend
    ⇧ 500.0%
About

PUBLICHNOE AKTSIONERNOE OBSHCHESTVO ODK UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE has a total of 12 patent applications. It increased the IP activity by 500.0%. Its first patent ever was published in 2017. It filed its patents most often in Russian Federation. Its main competitors in its focus markets engines, pumps and turbines and mechanical elements are PUBLICHNOE AKTSIONERNOE OBSHCHESTVO ODK UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIE PAO O, RATEAU SOC and BARBEZAT ALFRED.

Patent filings in countries

World map showing PUBLICHNOE AKTSIONERNOE OBSHCHESTVO ODK UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIEs patent filings in countries
# Country Total Patents
#1 Russian Federation 12

Patent filings per year

Chart showing PUBLICHNOE AKTSIONERNOE OBSHCHESTVO ODK UFIMSKOE MOTOROSTROITELNOE PROIZVODSTVENNOE OBEDINENIEs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Skiba Vladimir Vasilevich 9
#2 Grebenyuk Gennadij Petrovich 2
#3 Rakhmatullin Valerij Renatovich 2
#4 Sereda Boris Anatolevich 1
#5 Egorushkov Mikhail Yurevich 1
#6 Yalalov Ildar Irekovich 1
#7 Miftakhov Izfat Izfatovich 1

Latest patents

Publication Filing date Title
RU2730557C1 Gas turbine engine rotor support
RU2730558C1 Double-flow turbine jet engine
RU2731978C1 Method of breathing gas turbine engine rotor support oil cavity and oil ring vacuum pump for implementation thereof
RU2730565C1 Double-flow turbine jet engine
RU2732278C1 Device for turbojet engine broken turbine blade localization
RU2695872C1 Blade machine of stator of axial compressor
RU2702325C1 Device for turbojet jet nozzle rotation
RU2708279C1 Interval contact sealing
RU2702778C1 Gas turbine engine rotor support
RU2702324C1 Operating method of gas turbine engine with protective mesh at inlet and anti-icing system
RU2705023C1 Method of gas turbine engine operation
RU2711895C2 Double-flow jet turbine engine