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NPOB SATURN AOOT

Overview
  • Total Patents
    92
  • GoodIP Patent Rank
    183,720
About

NPOB SATURN AOOT has a total of 92 patent applications. Its first patent ever was published in 2004. It filed its patents most often in Russian Federation. Its main competitors in its focus markets engines, pumps and turbines and environmental technology are CARDARELLA L JAMES JR, SPANGLER BRANDON W and SEDLACEK VLASTIMIL.

Patent filings in countries

World map showing NPOB SATURN AOOTs patent filings in countries
# Country Total Patents
#1 Russian Federation 92

Patent filings per year

Chart showing NPOB SATURN AOOTs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Posadov Vladimir Valentinovich 12
#2 Matveev Anatolij Sergeevich 11
#3 Firsov Andrej Vladimirovich 9
#4 Porter Aleksandr Markovich 7
#5 Pajusov Valentin Izosimovich 6
#6 Andreev Vladimir Viktorovich 6
#7 Kuzmenko Mikhail Leonidovich 6
#8 Berestevich Artur Ivanovich 5
#9 Mikhajlov Aleksandr Leonidovic 5
#10 Popov German Mikhajlovich 5

Latest patents

Publication Filing date Title
RU2557821C1 Device for twisting blade feather of gas-turbine engine
RU2564655C1 Device for gas-static moulding of hollow workpieces
RU2561649C1 Method for gearbox fabrication
RU2564773C1 Dimensional electrochemical treatment method of parts from titanium and titanium alloys
RU2572690C2 Method of single stage diffusion chrome aluminising of parts out of heat-resistant alloys
RU2550072C1 Device for plastic structure formation of metals
RU2548221C1 Adjustment method of impeller of gas-turbine engine (gte)
RU2540226C1 Gear reverse reducer
RU2532089C1 Differential speed reduction gear of turbo-propeller engine
RU2542215C1 Detail screwing device
RU2528236C1 Planetary differential reduction gearbox
RU2533526C1 Method to provide resistance of turbomachine working blades to self-excited vibrations
RU2536645C1 Bench-type reduction gear unit for testing of engines
RU2527414C1 Marine power transmission
RU2552601C2 Part state estimation method
RU2525961C1 Fording of blades from two-phase titanium alloy
RU2535717C1 Composition of easy-to-remove protective coating
RU2536853C2 Casting gas turbine blade with directed and monocrystalline structure
RU2520934C1 Heat-resistant nickel alloy with higher resistance to sulphide corrosion combined with high heat resistance
RU2511773C1 Method of diagnostics of oscillations of turbomachine impeller