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LIANG GEORGE

Overview
  • Total Patents
    166
  • GoodIP Patent Rank
    233,679
About

LIANG GEORGE has a total of 166 patent applications. Its first patent ever was published in 2007. It filed its patents most often in United States and WIPO (World Intellectual Property Organization). Its main competitors in its focus markets engines, pumps and turbines, environmental technology and materials and metallurgy are TIBBOTT IAN, KOUKUU UCHIYUU GIJIYUTSU KENKI and SPANGLER BRANDON W.

Patent filings in countries

World map showing LIANG GEORGEs patent filings in countries

Patent filings per year

Chart showing LIANG GEORGEs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Liang George 166
#2 Gao Zhihong 4
#3 Gilliam Joseph B 2
#4 Wessell Brian J 2
#5 Ryznic John E 1
#6 Jiang Nan 1
#7 Salazar Santiago R 1

Latest patents

Publication Filing date Title
US8864469B1 Turbine rotor blade with super cooling
US2015152738A1 Turbine airfoil cooling passage with diamond turbulator
US2015152736A1 Turbine endwall with micro-circuit cooling
US2015152737A1 Turbine blade with near wall microcircuit edge cooling
US8585354B1 Turbine ring segment with riffle seal
US9447692B1 Turbine rotor blade with tip cooling
US9109451B1 Turbine blade with micro sized near wall cooling channels
US8500401B1 Turbine blade with counter flowing near wall cooling channels
US8678766B1 Turbine blade with near wall cooling channels
US8469666B1 Turbine blade tip portion with trenched cooling holes
US8876475B1 Turbine blade with radial cooling passage having continuous discrete turbulence air mixers
US8864468B1 Turbine stator vane with root turn purge air hole
US8459935B1 Turbine vane with endwall cooling
US9228437B1 Turbine airfoil with pressure side trailing edge cooling slots
US8414263B1 Turbine stator vane with near wall integrated micro cooling channels
US8851848B1 Turbine blade with showerhead film cooling slots
US8961136B1 Turbine airfoil with film cooling hole
US8864467B1 Turbine blade with serpentine flow cooling
US8261810B1 Turbine airfoil ceramic core with strain relief slot
US8858176B1 Turbine airfoil with leading edge cooling