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INST TECHNICZNY WOJSK LOTNICZYCH

Overview
  • Total Patents
    39
  • GoodIP Patent Rank
    64,961
  • Filing trend
    0.0%
About

INST TECHNICZNY WOJSK LOTNICZYCH has a total of 39 patent applications. It increased the IP activity by 0.0%. Its first patent ever was published in 2005. It filed its patents most often in Poland. Its main competitors in its focus markets machines and environmental technology are OGURTSOV VLADIMIR M, UNIV TEHNICĂ GHEORGHE ASACHI DIN IAŞI and CAMPUS CREATE CO LTD.

Patent filings in countries

World map showing INST TECHNICZNY WOJSK LOTNICZYCHs patent filings in countries
# Country Total Patents
#1 Poland 39

Patent filings per year

Chart showing INST TECHNICZNY WOJSK LOTNICZYCHs patent filings per year from 1900 to 2020

Focus industries

Top inventors

# Name Total Patents
#1 Lisiecki Janusz 8
#2 Szczepanik Ryszard 7
#3 Spychała Jarosław 7
#4 Dragan Krzysztof 6
#5 Kurnyta Artur 5
#6 Rokicki Edward 5
#7 Błażejewicz Teresa 4
#8 Dziendzikowski Michał 4
#9 Buler Wiesław 4
#10 Sałaciński Michał 3

Latest patents

Publication Filing date Title
PL430838A1 System for measuring the position of DC generator brushes in relation to the neutral zone
PL430742A1 Air-cooled inductive sensor for measuring the vibrations of rotating blades of rotor turbomachines at high temperature
PL429172A1 Sensor for measuring the content of microparticles from ferromagnetic materials in an aircraft engine oil system under operating conditions
PL429039A1 Device for continuous, autonomous measurement of the load-bearing capacity of the natural airport pavement and pavement layers made of an unbound mixture
PL425752A1 Electronic circuit for measuring a distance between the turbomachine blade tip and the sensor front end
PL424635A1 System for pyrotechnical releasing of utility loads from a no-pilot aircraft board
PL424167A1 Analog system for detection and monitoring of development of the structure elements damages, preferably of an aircraft structure
PL423479A1 Digital circuit for detection and monitoring of a structure elements cracking, preferably of the aircraft
PL421899A1 Dual-piston engine with central feeding with working fluid
PL420474A1 Method for regeneration of a highly stressed element
PL419670A1 Piezoelectric seismic transducer with the ability for remote testing of it efficiency
PL418311A1 System for determination of weight and position of centre of an aircraft mass
PL416960A1 Magnetorheological mixture with improved lubricating properties
PL414461A1 Laminar seat cushion with polyurethane auxetic foam
PL414277A1 Method for detection and monitoring of a composite structure damages, preferably with the non-conducting core
PL413613A1 Method for detection and monitoring of development of the structure elements damages, preferably of the aircraft structure
PL413582A1 Method for producing polyurethane auxetic foam with elongated return time
PL412871A1 Method for the assessment of air pore structure on the airfield pavement
PL411458A1 System for comparative tests of aviation fuels
PL409558A1 System for monitoring of loading of the aircraft structure in the airplane with variable wing geometry