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FEDERAL NOE GUP TSENTRAL NYJ INST AVIAT MOTOROSTROENIJA IM P I BARANOVA

Overview
  • Total Patents
    109
  • GoodIP Patent Rank
    96,442
About

FEDERAL NOE GUP TSENTRAL NYJ INST AVIAT MOTOROSTROENIJA IM P I BARANOVA has a total of 109 patent applications. Its first patent ever was published in 2008. It filed its patents most often in Russian Federation. Its main competitors in its focus markets environmental technology and engines, pumps and turbines are G OBRAZOVATEL NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL NOGO OBRAZOVANIJA JUZHNO ROSSIJSKIJ GU EHKONOMI, SHANGHAI TONGYUN AUTOMOBILE TE and SUZHOU HAIGE NEW ENERGY AUTO ELECTRIC CONTROL SYSTEM TECHNOLOGY CO LTD.

Patent filings in countries

World map showing FEDERAL NOE GUP TSENTRAL NYJ INST AVIAT MOTOROSTROENIJA IM P I BARANOVAs patent filings in countries
# Country Total Patents
#1 Russian Federation 109

Patent filings per year

Chart showing FEDERAL NOE GUP TSENTRAL NYJ INST AVIAT MOTOROSTROENIJA IM P I BARANOVAs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Starik Aleksandr Mikhajlovich 16
#2 Titova Natalija Sergeevna 10
#3 Aleksandrov Vadim Jur Evich 8
#4 Serikov Rostislav Ivanovich 8
#5 Shershakov Sergej Mikhajlovich 8
#6 Kuleshov Pavel Sergeevich 8
#7 Bychkov Nikolaj Grigor Evich 7
#8 Kulakov Vjacheslav Vasil Evich 7
#9 Savel Ev Aleksandr Mikhajlovich 7
#10 Khamidullin Artem Shamilevich 6

Latest patents

Publication Filing date Title
RU2557137C1 Liquefied gas supply system
RU2573438C1 Method of aircraft engine augmentation
RU2573425C1 Combustion in hypersonic air jet engine
RU2567689C1 Tooth-wheel
RU2565131C1 Ramjet engine running on solid propellant and method of its operation
RU2562926C1 Air-fluid device to throw birds' carcasses and other articles at aircraft tests
RU2563079C1 Low-sized gas turbine engine with heat recovery
RU2573331C2 Method of characteristics determination of non-synchronous oscillations of impeller of turbine machine
RU2562361C1 Cooling method of turbine work blade of gas-turbine engine
RU2559566C1 Measurement of pulsating flow parameters
RU2556304C1 Stand for testing gas-dynamic bearings
RU2555601C1 Gas dynamic ignitor of basic fuel mixture in flow channel
RU2547353C1 Liquid oxygen feed system and method of its feed from tank to consumer
RU2573427C2 Fuel-air mix combustion and ramjet engine with spin detonation wave
RU2563092C2 Method of detonation-deflagration combustion and detonation-deflagration ramjet engine
RU2551410C1 Gas generator clutch
RU2563641C2 Hybrid aerospace rocket ramjet
RU2548933C1 Method of spectrometric measurement of average temperature of gas layer of specified thickness
RU2548378C1 Procedure for evaluation of adhesion shear strength of heat shielding coating and device for its implementation
RU2558170C2 Method for determining frequency of forced oscillations of impeller as part of turbo-machine stage