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BERRY JONATHAN DWIGHT

Overview
  • Total Patents
    22
About

BERRY JONATHAN DWIGHT has a total of 22 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 environmental technology are MELTON PATRICK BENEDICT, BAILEY DONALD MARK and BATHINA MAHESH.

Patent filings in countries

World map showing BERRY JONATHAN DWIGHTs patent filings in countries
# Country Total Patents
#1 United States 22

Patent filings per year

Chart showing BERRY JONATHAN DWIGHTs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Berry Jonathan Dwight 22
#2 Ostebee Heath Michael 3
#3 Hughes Michael John 2
#4 Wu Chunyang 2
#5 Mcmahan Kevin Weston 2
#6 Stewart Jason Thurman 2
#7 Edwards Kara Johnston 1
#8 Repikov Timur Rustemovich 1
#9 Johnson Thomas Edward 1
#10 Lipinski John Joseph 1

Latest patents

Publication Filing date Title
US2013318977A1 Fuel injection assembly for use in turbine engines and method of assembling same
US2013305725A1 Fuel nozzle cap
US2013305739A1 Fuel nozzle cap
US2013219912A1 Combustor and method for purging a combustor
US2013167539A1 Fuel nozzles with mixing tubes surrounding a liquid fuel cartridge for injecting fuel in a gas turbine combustor
US2013086912A1 System for cooling a multi-tube fuel nozzle
US2013074510A1 Combustor and method for supplying fuel to a combustor
US2013032643A1 Combustor leaf seal arrangement
US2013025283A1 Sector nozzle mounting systems
US2012167578A1 Flame holding inhibitor for a lean pre-nozzle fuel injection diffuser and related method
US2012079829A1 Turbomachine including a mixing tube element having a vortex generator
US2012055168A1 System and method for producing hydrogen rich fuel
US2011252805A1 Combustor liner cooling at transition duct interface and related method
US2011243805A1 Fluid cooled reformer and method for cooling a reformer
US2011048030A1 Impingement cooled transition piece aft frame
US2011016878A1 System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
US2010293955A1 Multi-premixer fuel nozzle support system
US2010275601A1 Turbine air flow conditioner
US2010199628A1 Interlocking retention strip
US2010101204A1 Diluent shroud for combustor