Inventor · disambiguated record
David J. Wiebe
Also filed as: WIEBE DAVID · WIEBE DAVID J · WIEBE DAVID JAMES
49 granted patents·5 pending applications·956 citations·filing 1976–2018
98Inventor score
Files withWIEBE DAVID J18SIEMENS ENERGY INC13SIEMENS WESTINGHOUSE POWER3FOX TIMOTHY A2UNIFY GMBH & CO KG2
Top patents by PatentIndex Score
54 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
- 0397US8375726B2Combustor assembly in a gas turbine engineSIEMENS ENERGY INC·Filed 2009·Granted Feb 19, 2013·53 cites·16 claims
- 0494US6698207B1Flame-holding, single-mode nozzle assembly with tip coolingSIEMENS WESTINGHOUSE POWER·Filed 2002·Granted Mar 2, 2004·72 cites·17 claims
- 0593US8668454B2Turbine airfoil fillet cooling systemWIEBE DAVID J·Filed 2010·Granted Mar 11, 2014·19 cites·7 claims
- 0693US6672073B2System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plateSIEMENS WESTINGHOUSE POWER·Filed 2002·Granted Jan 6, 2004·85 cites·10 claims
- 0792US9399926B2Belly band seal with circumferential spacerWIEBE DAVID J·Filed 2013·Granted Jul 26, 2016·15 cites·17 claims
- 0892US7082380B2Refrigeration monitorWIEBE DAVID·Filed 2003·Granted Jul 25, 2006·112 cites·14 claims
- 0991US9759073B1Turbine airfoil having near-wall cooling insertSIEMENS ENERGY INC·Filed 2016·Granted Sep 12, 2017·6 cites·10 claims
- 1090US9316153B2Purge and cooling air for an exhaust section of a gas turbine assemblyPATAT HARRY·Filed 2013·Granted Apr 19, 2016·31 cites·20 claims
- 1190US5314304AAbradeable labyrinth stator sealUS ARMY·Filed 1991·Granted May 24, 1994·65 cites·14 claims
- 1287US8376697B2Gas turbine sealing apparatusSIEMENS ENERGY INC·Filed 2009·Granted Feb 19, 2013·27 cites·20 claims
- 1386US4380896AAnnular combustor having ceramic linerUS ARMY·Filed 1980·Granted Apr 26, 1983·42 cites·8 claims
- 1484US9957818B2Removably attachable snubber assemblySIEMENS ENERGY INC·Filed 2015·Granted May 1, 2018·4 cites·16 claims
- 1584US9650904B1Transition duct system with straight ceramic liner for delivering hot-temperature gases in a combustion turbine engineSIEMENS ENERGY INC·Filed 2016·Granted May 16, 2017·4 cites·17 claims
- 1684US9091180B2Airfoil assembly including vortex reducing at an airfoil leading edgeWIEBE DAVID J·Filed 2012·Granted Jul 28, 2015·8 cites·17 claims
- 1784US8978389B2Radial inflow gas turbine engine with advanced transition ductWIEBE DAVID J·Filed 2011·Granted Mar 17, 2015·8 cites·19 claims
- 1884US6786046B2Dual-mode nozzle assembly with passive tip coolingSIEMENS WESTINGHOUSE POWER·Filed 2002·Granted Sep 7, 2004·29 cites·17 claims
- 1983US8210819B2Airfoil structure shimWIEBE DAVID J·Filed 2008·Granted Jul 3, 2012·22 cites·20 claims
- 2081US5165860ADamped airfoil bladeUNITED TECHNOLOGIES CORP·Filed 1991·Granted Nov 24, 1992·71 cites·12 claims
- 2179US4043147AIntershaft balance weightUS AIR FORCE·Filed 1976·Granted Aug 23, 1977·36 cites·2 claims
- 2276US8959888B2Device to lower NOx in a gas turbine engine combustion systemLASTER WALTER R·Filed 2011·Granted Feb 24, 2015·5 cites·19 claims
- 2376US8622016B2Wear indication system for compressor diaphragms of gas turbine enginesWIEBE DAVID J·Filed 2011·Granted Jan 7, 2014·5 cites·20 claims
- 2475US9618207B1Transition duct system with metal liners for delivering hot-temperature gases in a combustion turbine engineSIEMENS ENERGY INC·Filed 2016·Granted Apr 11, 2017·2 cites·15 claims
- 2575US8585356B2Control 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
- 2675US5803710ATurbine engine rotor blade platform sealing and vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 1996·Granted Sep 8, 1998·41 cites·8 claims
- 2774US10133644B2Method and apparatus for indirectly assessing a status of an active entityUNIFY GMBH & CO KG·Filed 2016·Granted Nov 20, 2018·2 cites·21 claims
- 2874US8920116B2Wear prevention system for securing compressor airfoils within a turbine engineWIEBE DAVID J·Filed 2011·Granted Dec 30, 2014·6 cites·6 claims
- 2973US9810434B2Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engineSIEMENS ENERGY INC·Filed 2016·Granted Nov 7, 2017·2 cites·14 claims
- 3073US8770924B2Gas turbine engine with angled and radial supportsBEECK ALEXANDER·Filed 2011·Granted Jul 8, 2014·6 cites·20 claims
- 3171US8757981B2Locking spacer assembly for a turbine engineWIEBE DAVID J·Filed 2011·Granted Jun 24, 2014·4 cites·20 claims
- 3271US8721278B2Exhaust manifold flange connectionSHTEYMAN YEVGENIY·Filed 2011·Granted May 13, 2014·6 cites·17 claims
- 3369US10767504B2Flexible damper for turbine bladesSIEMENS AG·Filed 2016·Granted Sep 8, 2020·1 cites·13 claims
- 3469US10649866B2Method and apparatus for indirectly assessing a status of an active entityUNIFY GMBH & CO KG·Filed 2018·Granted May 12, 2020·1 cites·21 claims
- 3569US9822669B2Turbine assembly with detachable strutsSIEMENS ENERGY INC·Filed 2014·Granted Nov 21, 2017·4 cites·13 claims
- 3668US9322558B2Combustor apparatus in a gas turbine engineRAMIER STEPHEN A·Filed 2013·Granted Apr 26, 2016·4 cites·16 claims
- 3768US9267689B2Combustor apparatus in a gas turbine engineWIEBE DAVID J·Filed 2013·Granted Feb 23, 2016·4 cites·20 claims
- 3867US8991192B2Fuel 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
- 3964US6698738B2Multi-direction swivel viseFiled 2003·Granted Mar 2, 2004·8 cites·9 claims
- 4062US9115600B2Insulated wall sectionWIEBE DAVID J·Filed 2011·Granted Aug 25, 2015·2 cites·20 claims
- 4159US7272930B2Exhaust diffuser assembly with tunable velocity profileSIEMENS POWER GENERATION·Filed 2003·Granted Sep 25, 2007·20 cites·10 claims
- 4258US9885482B1Method of making an aero-derivative gas turbine engineSIEMENS ENERGY INC·Filed 2016·Granted Feb 6, 2018·0 cites·5 claims
- 4358US9470422B2Gas 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
- 4458US8549859B2Combustor apparatus in a gas turbine engineFOX TIMOTHY A·Filed 2008·Granted Oct 8, 2013·6 cites·20 claims
- 4556US9803487B2Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engineSIEMENS ENERGY INC·Filed 2014·Granted Oct 31, 2017·2 cites·14 claims
- 4650US4539864AAdjustable balance weight for rotating shaftUS AIR FORCE·Filed 1982·Granted Sep 10, 1985·13 cites·4 claims
- 4749US9206699B2Mid-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
- 4847US2013081407A1Aero-derivative gas turbine engine with an advanced transition duct combustion assemblyWIEBE DAVID J·Filed 2011·Application pending·0 cites
- 4945US9388738B2Casing for a gas turbine engineWIEBE DAVID J·Filed 2011·Granted Jul 12, 2016·0 cites·9 claims
- 5043US2010071377A1Combustor Apparatus for Use in a Gas Turbine EngineFOX TIMOTHY A·Filed 2009·Application pending·0 cites
Showing the top 50 of 54 patent records by PatentIndex Score.
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