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OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OBEDINENIE SATURN

Overview
  • Total Patents
    11
  • GoodIP Patent Rank
    161,555
About

OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OBEDINENIE SATURN has a total of 11 patent applications. Its first patent ever was published in 2014. It filed its patents most often in Russian Federation. Its main competitors in its focus markets engines, pumps and turbines, measurement and materials and metallurgy are PUBLICHNOE AKTSIONERNOE OBSHCHESTVO ODK SATURN, ZHIYUE TENGFENG TECH INVEST GROUP CO LTD and ZOLLERN BHW GLEITLAGER GMBH & CO KG.

Patent filings in countries

World map showing OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OBEDINENIE SATURNs patent filings in countries
# Country Total Patents
#1 Russian Federation 11

Patent filings per year

Chart showing OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OBEDINENIE SATURNs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Shmotin Yurij Nikolaevich 4
#2 Danilov Denis Viktorovich 3
#3 Leshchenko Igor Alekseevich 3
#4 Zavodov Sergej Aleksandrovich 3
#5 Porter Aleksandr Markovich 3
#6 Logunov Aleksandr Vyacheslavovich 3
#7 Berestevich Artur Ivanovich 2
#8 Khryashchev Ilya Igorevich 2
#9 Mikhajlov Aleksandr Mikhajlovich 2
#10 Kochetkov Vladimir Andreevich 2

Latest patents

Publication Filing date Title
RU2623938C1 Method of circular electrochemical processing compressor blades of gas turbine engine
RU2618602C1 Method for x-ray control parts of gas turbine engine
RU2626783C2 Combined radial support
RU2612687C1 Mulimode multifuel engine control method
RU2626180C2 Remote combustion chamber
RU2623838C2 Method for x-ray diffraction controlling parts of gas turbine engine
RU2623941C2 Method of obtaining large-dimensional castings from heat-resistant alloys by directed crystalization
RU2626118C2 Casting heat resistant nickel-based alloy
RU2623940C2 Casting nickel alloy with increased heat strength and resistance to sulfide corrosion
RU2603883C1 Joint assembly between transmission shaft and rotor shaft of power turbine
RU2618145C2 Method for inspection intervals determination for aero-derivative gas turbine engine parts in case of operation according to its technical condition