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AKTSIONERNOE OBSHCHESTVO ODK AVIADVIGATEL

Overview
  • Total Patents
    32
  • GoodIP Patent Rank
    48,233
  • Filing trend
    ⇩ 60.0%
About

AKTSIONERNOE OBSHCHESTVO ODK AVIADVIGATEL has a total of 32 patent applications. It decreased the IP activity by 60.0%. Its first patent ever was published in 2016. It filed its patents most often in Russian Federation and China. Its main competitors in its focus markets engines, pumps and turbines, materials and metallurgy and machine tools are BACHL HERBERT, TALALMANYKIFEJLESZTOE ES ERTEK and FABRICATION DES MOTEURS ET TUR.

Patent filings in countries

World map showing AKTSIONERNOE OBSHCHESTVO ODK AVIADVIGATELs patent filings in countries
# Country Total Patents
#1 Russian Federation 29
#2 China 3

Patent filings per year

Chart showing AKTSIONERNOE OBSHCHESTVO ODK AVIADVIGATELs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Kuznetsov Valerij Alekseevich 11
#2 Sychev Vladimir Konstantinovich 10
#3 Yazev Vladimir Mikhajlovich 9
#4 Shilov Aleksandr Vladimirovich 5
#5 Ordin Dmitrij Alekseevich 5
#6 Fadeev Sergej Ivanovich 4
#7 Zvezdin Vladimir Leonidovich 4
#8 Uglev Nikolaj Pavlovich 3
#9 Cherepanov Sergej Evgenevich 3
#10 Pojlov Vladimir Zotovich 3

Latest patents

Publication Filing date Title
RU2722944C1 Three-dimensional printing method with thermoplastic composite material
RU2721974C1 Method of producing ceramic mixture and ceramic mixture
RU2696614C1 Method of wetting wax patterns
RU2693338C1 Method for determination of gas turbine engine combustion chamber extinction
RU2696067C1 Control method of cooling system of turbine blades of gas-turbine engine
RU2696173C1 Rotor of compressor of gas turbine engine
RU2705051C1 Method of adjusting cnc machine for processing complex contours of surfaces
RU2686499C1 Method of repairing a cooled blade from a heat-resistant superalloy of a turbine of a gas turbine engine
RU2674106C1 Main gearbox helicopter
RU2665602C1 Method of regulating fuel supply to gas turbine engine
RU2670469C1 Method for protecting a gas turbine engine from multiple compressor surgings
RU2670116C1 Binder for manufacture of ceramic forms used for equalaxial casting of heat-resistant alloys by welded models
RU2676937C1 Gas turbine engine part with the thin-walled element restoration method
RU2670115C1 Binder for manufacture of ceramic forms used for casting of heat-resistant alloys by welded models, and method for manufacture of ceramic forms binder for manufacture of used for casting of heat-resistant alloys by welded models
RU2673924C1 Stator of gas turbine
RU2656194C1 Melted model composition cleaning method and installation
RU2648174C1 Method of treatment of a radial end groove on the parts of a gas turbine engine (options)
RU2644207C1 Method for verification of positioning accuracy of five-coordinate machine with cnc
RU2644660C1 Gas turbine engine
RU2647944C1 Gas turbine engine with birotate fan