Learn more

WIEBE DAVID J

Overview
  • Total Patents
    18
About

WIEBE DAVID J has a total of 18 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, machines and thermal processes are ANSALDO ENERDZHIA SVITZERLEND AG, BMW ROLLS ROYCE GMBH and SOLAR TURBINES INC.

Patent filings in countries

World map showing WIEBE DAVID Js patent filings in countries
# Country Total Patents
#1 United States 18

Patent filings per year

Chart showing WIEBE DAVID Js patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Wiebe David J 18
#2 Charron Richard C 3
#3 Montgomery Matthew D 2
#4 Fox Timothy A 2
#5 Little David A 1
#6 Garan Daniel W 1
#7 Morrison Jay A 1
#8 Deane Erick J 1
#9 Pela Adam C 1
#10 Finneran John W 1

Latest patents

Publication Filing date Title
US2015107264A1 Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier
US2015056068A1 Belly band seal with circumferential spacer
US2014245740A1 Combustor apparatus in a gas turbine engine
US2014023483A1 Airfoil assembly including vortex reducing at an airfoil leading edge
US2013219921A1 Mid-section of a can-annular gas turbine engine with a cooling system for the transition
US2013152543A1 Radial inflow gas turbine engine with advanced transition duct
US2013089417A1 Wear prevention system for securing compressor airfoils within a turbine engine
US2013081399A1 Casing for a gas turbine engine
US2013084163A1 Wear indication system for compressor diaphragms of gas turbine engines
US2013081407A1 Aero-derivative gas turbine engine with an advanced transition duct combustion assembly
US2013051995A1 Insulated wall section
US2012275918A1 Locking spacer assembly for a turbine engine
US2011236182A1 Control of blade tip-to-shroud leakage in a turbine engine by directed plasma flow
US2011217179A1 Turbine airfoil fillet cooling system
US2011067402A1 Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine
US2011056206A1 Fuel injector for use in a gas turbine engine
US2009214349A1 Airfoil structure shim