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UHM JONG HO

Overview
  • Total Patents
    25
About

UHM JONG HO has a total of 25 patent applications. Its first patent ever was published in 2008. It filed its patents most often in United States. Its main competitors in its focus markets engines, pumps and turbines, thermal processes and machines are JOHNSON THOMAS EDWARD, BATHINA MAHESH and KHAN ABDUL RAFEY.

Patent filings in countries

World map showing UHM JONG HOs patent filings in countries
# Country Total Patents
#1 United States 25

Patent filings per year

Chart showing UHM JONG HOs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Uhm Jong Ho 25
#2 Johnson Thomas Edward 20
#3 York William David 5
#4 Ziminsky Willy Steve 4
#5 Zuo Baifang 4
#6 Kim Kwanwoo 3
#7 Kraemer Gilbert Otto 2
#8 Felling David 2
#9 Wu Chunyang 2
#10 Yilmaz Ertan 2

Latest patents

Publication Filing date Title
US2013227953A1 System and method for reducing combustion dynamics in a combustor
US2013227928A1 Fuel nozzle assembly for use in turbine engines and method of assembling same
US8511086B1 System and method for reducing combustion dynamics in a combustor
US2013219899A1 Annular premixed pilot in fuel nozzle
US2013199190A1 Fuel injection assembly for use in turbine engines and method of assembling same
US2013199189A1 Fuel injection assembly for use in turbine engines and method of assembling same
US2013174568A1 Combustor and method for distributing fuel in the combustor
US8438851B1 Combustor assembly for use in a turbine engine and methods of assembling same
US2013104551A1 Fuel injection assembly for use in turbine engines and method of assembling same
US2013104556A1 System and method for reducing combustion dynamics and NOx in a combustor
US2013104552A1 Fuel nozzle assembly for use in turbine engines and methods of assembling same
US2013101943A1 Combustor and method for conditioning flow through a combustor
US2013045450A1 System and method for reducing combustion dynamics in a combustor
US2012198856A1 Turbine combustor configured for high-frequency dynamics mitigation and related method
US2012198812A1 Apparatus for mixing fuel in a gas turbine
US2012192566A1 Fuel injection assembly for use in turbine engines and method of assembling same
US2012180487A1 System for flow control in multi-tube fuel nozzle
US2012180495A1 System and method for injecting fuel
US2012058437A1 Apparatus and method for mixing fuel in a gas turbine nozzle
US2012055163A1 Fuel injection assembly for use in turbine engines and method of assembling same