Inventor · disambiguated record
Kevin Weston Mcmahan
Also filed as: MCMAHAN KEVIN · MCMAHAN KEVIN J · MCMAHAN KEVIN W · MCMAHAN KEVIN WESTON
65 granted patents·20 pending applications·778 citations·filing 1996–2021
99Inventor score
Files withGEN ELECTRIC42MCMAHAN KEVIN WESTON14FLANAGAN JAMES SCOTT6LEBEGUE JEFFREY SCOTT4KIM WON-WOOK3
Top patents by PatentIndex Score
85 records- 0199US6993916B2Burner tube and method for mixing air and gas in a gas turbine engineGEN ELECTRIC·Filed 2004·Granted Feb 7, 2006·216 cites·22 claims
- 0298US7082766B1One-piece can combustorGEN ELECTRIC·Filed 2005·Granted Aug 1, 2006·79 cites·19 claims
- 0394US8398090B2Spring loaded seal assembly for turbinesMCMAHAN KEVIN WESTON·Filed 2010·Granted Mar 19, 2013·23 cites·14 claims
- 0493US8459041B2Leaf seal for transition duct in turbine systemFLANAGAN JAMES SCOTT·Filed 2011·Granted Jun 11, 2013·22 cites·16 claims
- 0590US9649690B2System having layered structure and method of making the sameGEN ELECTRIC·Filed 2014·Granted May 16, 2017·6 cites·13 claims
- 0690US9133722B2Transition duct with late injection in turbine systemLEBEGUE JEFFREY SCOTT·Filed 2012·Granted Sep 15, 2015·14 cites·18 claims
- 0790US9097184B2Gas turbine system having premixed injector vanesSTRYAPUNIN SERGEY ALEKSANDROVICH·Filed 2010·Granted Aug 4, 2015·24 cites·21 claims
- 0887US8701415B2Flexible metallic seal for transition duct in turbine systemFLANAGAN JAMES SCOTT·Filed 2011·Granted Apr 22, 2014·12 cites·16 claims
- 0987US5749701AInterstage seal assembly for a turbineGEN ELECTRIC·Filed 1996·Granted May 12, 1998·94 cites·10 claims
- 1086US10690056B2Segmented annular combustion system with axial fuel stagingGEN ELECTRIC·Filed 2017·Granted Jun 23, 2020·2 cites·19 claims
- 1186US9291103B2Fuel nozzle for a combustor of a gas turbine engineGEN ELECTRIC·Filed 2012·Granted Mar 22, 2016·9 cites·12 claims
- 1285US9255484B2Aft frame and method for cooling aft frameCIHLAR DAVID WILLIAM·Filed 2011·Granted Feb 9, 2016·10 cites·12 claims
- 1385US8707673B1Articulated transition duct in turbomachineGEN ELECTRIC·Filed 2013·Granted Apr 29, 2014·9 cites·13 claims
- 1485US8418468B2Segmented annular ring-manifold quaternary fuel distributorMCMAHAN KEVIN WESTON·Filed 2010·Granted Apr 16, 2013·10 cites·29 claims
- 1584US10584880B2Mounting of integrated combustor nozzles in a segmented annular combustion systemGEN ELECTRIC·Filed 2017·Granted Mar 10, 2020·3 cites·20 claims
- 1682US11047248B2Curved seal for adjacent gas turbine componentsGEN ELECTRIC·Filed 2018·Granted Jun 29, 2021·2 cites·13 claims
- 1782US10337404B2Preferential cooling of gas turbine nozzlesMCMAHAN KEVIN WESTON·Filed 2010·Granted Jul 2, 2019·8 cites·20 claims
- 1882US8438856B2Effusion cooled one-piece can combustorCHILA RONALD JAMES·Filed 2009·Granted May 14, 2013·18 cites·13 claims
- 1980US8590314B2Combustor liner helical cooling apparatusMCMAHAN KEVIN WESTON·Filed 2010·Granted Nov 26, 2013·6 cites·20 claims
- 2079US8522555B2Multi-premixer fuel nozzle support systemBERRY JONATHAN DWIGHT·Filed 2009·Granted Sep 3, 2013·14 cites·16 claims
- 2179US7490471B2Swirler assemblyGEN ELECTRIC·Filed 2005·Granted Feb 17, 2009·16 cites·12 claims
- 2278US8353165B2Combustor assembly for use in a turbine engine and methods of fabricating sameGEN ELECTRIC·Filed 2011·Granted Jan 15, 2013·6 cites·20 claims
- 2375US9038666B2Electromagnetic flow controllerCHEN WEI·Filed 2012·Granted May 26, 2015·3 cites·20 claims
- 2474US8245515B2Transition duct aft end frame cooling and related methodDAVIS JR LEWIS B·Filed 2008·Granted Aug 21, 2012·15 cites·12 claims
- 2573US8720206B2Methods and systems for inducing combustion dynamicsMCMAHAN KEVIN WESTON·Filed 2009·Granted May 13, 2014·6 cites·29 claims
- 2673US7970570B2Methods and systems for analysis of combustion dynamics in the time domainGEN ELECTRIC·Filed 2006·Granted Jun 28, 2011·9 cites·20 claims
- 2772US9080447B2Transition duct with divided upstream and downstream portionsGEN ELECTRIC·Filed 2013·Granted Jul 14, 2015·4 cites·20 claims
- 2872US8915087B2Methods and systems for transferring heat from a transition nozzleMCMAHAN KEVIN WESTON·Filed 2011·Granted Dec 23, 2014·4 cites·20 claims
- 2972US8281601B2Systems and methods for reintroducing gas turbine combustion bypass flowMCMAHAN KEVIN WESTON·Filed 2009·Granted Oct 9, 2012·11 cites·19 claims
- 3071US9360221B2Gas turbine burnerGEN ELECTRIC·Filed 2013·Granted Jun 7, 2016·3 cites·10 claims
- 3170US9546601B2Clocked combustor can arrayGEN ELECTRIC·Filed 2012·Granted Jan 17, 2017·3 cites·8 claims
- 3270US6220815B1Inter-stage seal retainer and assemblyGEN ELECTRIC·Filed 1999·Granted Apr 24, 2001·44 cites·36 claims
- 3369US11773739B2Curved seal for adjacent gas turbine componentsGEN ELECTRIC·Filed 2021·Granted Oct 3, 2023·0 cites·20 claims
- 3469US11231175B2Integrated combustor nozzles with continuously curved liner segmentsGEN ELECTRIC·Filed 2018·Granted Jan 25, 2022·1 cites·18 claims
- 3569US10684016B2Aft frame assembly for gas turbine transition pieceGEN ELECTRIC·Filed 2017·Granted Jun 16, 2020·1 cites·17 claims
- 3669US9360220B2Micro-mixer nozzleGEN ELECTRIC·Filed 2012·Granted Jun 7, 2016·3 cites·6 claims
- 3769US8683805B2Injector seal for a gas turbomachineCHEN WEI·Filed 2012·Granted Apr 1, 2014·3 cites·30 claims
- 3868US11215072B2Aft frame assembly for gas turbine transition pieceGEN ELECTRIC·Filed 2017·Granted Jan 4, 2022·1 cites·20 claims
- 3968US10718224B2AFT frame assembly for gas turbine transition pieceGEN ELECTRIC·Filed 2017·Granted Jul 21, 2020·1 cites·23 claims
- 4067US11137143B2System having layered structure and method of making the sameGEN ELECTRIC·Filed 2017·Granted Oct 5, 2021·0 cites·16 claims
- 4167US8322976B2High temperature seal for a turbine engineCHILA RONALD JAMES·Filed 2008·Granted Dec 4, 2012·10 cites·20 claims
- 4267US8186167B2Combustor transition piece aft end cooling and related methodCHILA RONALD J·Filed 2008·Granted May 29, 2012·11 cites·13 claims
- 4366US9145778B2Combustor with non-circular head endKIM WON-WOOK·Filed 2012·Granted Sep 29, 2015·3 cites·12 claims
- 4465US8087228B2Segmented combustor capMCMAHAN KEVIN WESTON·Filed 2008·Granted Jan 3, 2012·10 cites·9 claims
- 4563US9243506B2Methods and systems for cooling a transition nozzleMCMAHAN KEVIN WESTON·Filed 2012·Granted Jan 26, 2016·2 cites·11 claims
- 4663US8650852B2Support assembly for transition duct in turbine systemLEBEGUE JEFFREY SCOTT·Filed 2011·Granted Feb 18, 2014·2 cites·12 claims
- 4761US8707705B2Impingement cooled transition piece aft frameBERRY JONATHAN DWIGHT·Filed 2009·Granted Apr 29, 2014·6 cites·18 claims
- 4860US8448450B2Support assembly for transition duct in turbine systemLEBEGUE JEFFREY SCOTT·Filed 2011·Granted May 28, 2013·2 cites·18 claims
- 4959US8966910B2Methods and systems for cooling a transition nozzleMCMAHAN KEVIN WESTON·Filed 2011·Granted Mar 3, 2015·1 cites·18 claims
- 5059US2012031097A1Multi-premixer fuel nozzleMCMAHAN KEVIN WESTON·Filed 2009·Application pending·0 cites
Showing the top 50 of 85 patent records by PatentIndex Score.
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