Assignee
WIEBE DAVID J
US·17 granted patents·1 pending application·196 citations·filing 2008–2013
Top patents by PatentIndex Score
18 records- 0198US9016066B2Combustor assembly in a gas turbine engineWIEBE DAVID J·Filed 2012·Granted Apr 28, 2015·29 cites·19 claims
- 0298US8281594B2Fuel injector for use in a gas turbine engineWIEBE DAVID J·Filed 2009·Granted Oct 9, 2012·59 cites·20 claims
- 0393US8668454B2Turbine airfoil fillet cooling systemWIEBE DAVID J·Filed 2010·Granted Mar 11, 2014·19 cites·7 claims
- 0492US9399926B2Belly band seal with circumferential spacerWIEBE DAVID J·Filed 2013·Granted Jul 26, 2016·15 cites·17 claims
- 0584US9091180B2Airfoil assembly including vortex reducing at an airfoil leading edgeWIEBE DAVID J·Filed 2012·Granted Jul 28, 2015·8 cites·17 claims
- 0684US8978389B2Radial inflow gas turbine engine with advanced transition ductWIEBE DAVID J·Filed 2011·Granted Mar 17, 2015·8 cites·19 claims
- 0783US8210819B2Airfoil structure shimWIEBE DAVID J·Filed 2008·Granted Jul 3, 2012·22 cites·20 claims
- 0876US8622016B2Wear indication system for compressor diaphragms of gas turbine enginesWIEBE DAVID J·Filed 2011·Granted Jan 7, 2014·5 cites·20 claims
- 0975US8585356B2Control of blade tip-to-shroud leakage in a turbine engine by directed plasma flowWIEBE DAVID J·Filed 2010·Granted Nov 19, 2013·5 cites·12 claims
- 1074US8920116B2Wear prevention system for securing compressor airfoils within a turbine engineWIEBE DAVID J·Filed 2011·Granted Dec 30, 2014·6 cites·6 claims
- 1171US8757981B2Locking spacer assembly for a turbine engineWIEBE DAVID J·Filed 2011·Granted Jun 24, 2014·4 cites·20 claims
- 1268US9267689B2Combustor apparatus in a gas turbine engineWIEBE DAVID J·Filed 2013·Granted Feb 23, 2016·4 cites·20 claims
- 1367US8991192B2Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engineWIEBE DAVID J·Filed 2009·Granted Mar 31, 2015·9 cites·17 claims
- 1462US9115600B2Insulated wall sectionWIEBE DAVID J·Filed 2011·Granted Aug 25, 2015·2 cites·20 claims
- 1558US9470422B2Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrierWIEBE DAVID J·Filed 2013·Granted Oct 18, 2016·1 cites·12 claims
- 1649US9206699B2Mid-section of a can-annular gas turbine engine with a cooling system for the transitionWIEBE DAVID J·Filed 2012·Granted Dec 8, 2015·0 cites·19 claims
- 1747US2013081407A1Aero-derivative gas turbine engine with an advanced transition duct combustion assemblyWIEBE DAVID J·Filed 2011·Application pending·0 cites
- 1845US9388738B2Casing for a gas turbine engineWIEBE DAVID J·Filed 2011·Granted Jul 12, 2016·0 cites·9 claims
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