Inventor · disambiguated record
Gregory O. Woodcock
Also filed as: WOODCOCK GREGORY O
17 granted patents·12 pending applications·189 citations·filing 2003–2017
93Inventor score
Top patents by PatentIndex Score
29 records- 0194US10195574B2Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2017·Granted Feb 5, 2019·6 cites·9 claims
- 0286US7531048B2On-wing combustor cleaning using direct insertion nozzle, wash agent, and procedureHONEYWELL INT INC·Filed 2005·Granted May 12, 2009·35 cites·27 claims
- 0385US8388307B2Turbine nozzle assembly including radially-compliant spring member for gas turbine engineSMOKE JASON·Filed 2009·Granted Mar 5, 2013·26 cites·17 claims
- 0481US10166524B2Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2017·Granted Jan 1, 2019·1 cites·14 claims
- 0576US8534076B2Combustor-turbine seal interface for gas turbine engineWOODCOCK GREGORY O·Filed 2009·Granted Sep 17, 2013·16 cites·19 claims
- 0675US7812282B2Methods of forming fan-shaped effusion holes in combustorsHONEYWELL INT INC·Filed 2007·Granted Oct 12, 2010·18 cites·19 claims
- 0773US9707530B2Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Granted Jul 18, 2017·1 cites·10 claims
- 0873US9656229B2Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Granted May 23, 2017·1 cites·4 claims
- 0970US7984615B2Combustors for use in turbine engine assembliesHONEYWELL INT INC·Filed 2007·Granted Jul 26, 2011·13 cites·15 claims
- 1066US6912782B2Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Jul 5, 2005·11 cites·23 claims
- 1165US7007480B2Multi-axial pivoting combustor liner in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Mar 7, 2006·26 cites·26 claims
- 1257US8104288B2Effusion cooling techniques for combustors in engine assembliesWOODCOCK GREGORY O·Filed 2008·Granted Jan 31, 2012·6 cites·15 claims
- 1357US2014058173A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 1457US2017015606A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2016·Application pending·0 cites
- 1556US8127552B2Transition scrolls for use in turbine engine assembliesSCHUMACHER JURGEN C·Filed 2008·Granted Mar 6, 2012·7 cites·18 claims
- 1656US7093448B2Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Aug 22, 2006·18 cites·14 claims
- 1747US10160697B2Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2017·Granted Dec 25, 2018·0 cites·19 claims
- 1846US2014058174A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 1946US2014056771A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 2046US2014058170A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 2146US2014058172A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 2246US2014058176A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 2346US2014058169A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 2445US2014058178A1Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2013·Application pending·0 cites
- 2544US10029957B2Methane conversion apparatus and process using a supersonic flow reactorUOP LLC·Filed 2017·Granted Jul 24, 2018·0 cites·15 claims
- 2643US2006016191A1Combined effusion and thick TBC cooling methodHONEYWELL INT INC·Filed 2004·Application pending·0 cites
- 2739US6962480B2Thermally stabilized turbine scroll retention ring for uniform loading applicationHONEYWELL INT INC·Filed 2003·Granted Nov 8, 2005·4 cites·19 claims
- 2838US2009188256A1Effusion cooling for gas turbine combustorsHONEYWELL INT INC·Filed 2008·Application pending·0 cites
- 2933US2005241316A1Uniform effusion cooling method for a can combustion chamberHONEYWELL INT INC·Filed 2004·Application pending·0 cites
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