Assignee
LACY BENJAMIN PAUL
US·20 granted patents·9 pending applications·305 citations·filing 2007–2012
Top patents by PatentIndex Score
29 records- 0198US8651805B2Hot gas path component cooling systemLACY BENJAMIN PAUL·Filed 2010·Granted Feb 18, 2014·35 cites·19 claims
- 0296US9273561B2Cooling structures for turbine rotor blade tipsLACY BENJAMIN PAUL·Filed 2012·Granted Mar 1, 2016·28 cites·18 claims
- 0396US8499566B2Combustor liner cooling systemLACY BENJAMIN PAUL·Filed 2010·Granted Aug 6, 2013·52 cites·20 claims
- 0495US8753083B2Curved cooling passages for a turbine componentLACY BENJAMIN PAUL·Filed 2011·Granted Jun 17, 2014·23 cites·19 claims
- 0595US8147121B2Pre-mixing apparatus for a turbine engineLACY BENJAMIN PAUL·Filed 2008·Granted Apr 3, 2012·44 cites·15 claims
- 0693US9188012B2Cooling structures in the tips of turbine rotor bladesLACY BENJAMIN PAUL·Filed 2012·Granted Nov 17, 2015·17 cites·21 claims
- 0793US8870535B2AirfoilLACY BENJAMIN PAUL·Filed 2012·Granted Oct 28, 2014·16 cites·21 claims
- 0893US8870536B2AirfoilLACY BENJAMIN PAUL·Filed 2012·Granted Oct 28, 2014·16 cites·21 claims
- 0993US8523527B2Apparatus for cooling a platform of a turbine componentLACY BENJAMIN PAUL·Filed 2010·Granted Sep 3, 2013·16 cites·20 claims
- 1090US8956104B2Bucket assembly for turbine systemLACY BENJAMIN PAUL·Filed 2011·Granted Feb 17, 2015·13 cites·20 claims
- 1184US8225614B2Shim for sealing transition piecesLACY BENJAMIN PAUL·Filed 2010·Granted Jul 24, 2012·9 cites·15 claims
- 1281US9127549B2Turbine shroud cooling assembly for a gas turbine systemLACY BENJAMIN PAUL·Filed 2012·Granted Sep 8, 2015·7 cites·16 claims
- 1381US8453454B2Coannular oil injection nozzleLACY BENJAMIN PAUL·Filed 2010·Granted Jun 4, 2013·4 cites·9 claims
- 1471US8209986B2Multi-tube thermal fuse for nozzle protection from a flame holding or flashback eventLACY BENJAMIN PAUL·Filed 2008·Granted Jul 3, 2012·11 cites·17 claims
- 1568US9382810B2Closed loop cooling system for a gas turbineLACY BENJAMIN PAUL·Filed 2012·Granted Jul 5, 2016·3 cites·10 claims
- 1667US9303517B2Channel marker and related methodsLACY BENJAMIN PAUL·Filed 2012·Granted Apr 5, 2016·0 cites·6 claims
- 1765US9151179B2Turbine shroud segment cooling system and methodLACY BENJAMIN PAUL·Filed 2011·Granted Oct 6, 2015·3 cites·20 claims
- 1855US8297059B2Nozzle for a turbomachineLACY BENJAMIN PAUL·Filed 2009·Granted Oct 30, 2012·4 cites·9 claims
- 1954US8117845B2Systems to facilitate reducing flashback/flame holding in combustion systemsLACY BENJAMIN PAUL·Filed 2007·Granted Feb 21, 2012·4 cites·15 claims
- 2046US2012210718A1Plating of ceramic matrix composite parts as joining method in gas turbine hardwareLACY BENJAMIN PAUL·Filed 2011·Application pending·0 cites
- 2144US2013313307A1Method for manufacturing a hot gas path componentLACY BENJAMIN PAUL·Filed 2012·Application pending·0 cites
- 2243US9140454B2Bundled multi-tube nozzle for a turbomachineLACY BENJAMIN PAUL·Filed 2009·Granted Sep 22, 2015·0 cites·20 claims
- 2342US2014062034A1Gas path leakage seal for a turbineLACY BENJAMIN PAUL·Filed 2012·Application pending·0 cites
- 2442US2013094971A1Hot gas path component for turbine systemLACY BENJAMIN PAUL·Filed 2011·Application pending·0 cites
- 2542US2013139386A1Honeycomb construction for abradable angel wingLACY BENJAMIN PAUL·Filed 2011·Application pending·0 cites
- 2642US2011225947A1System and methods for altering air flow in a combustorLACY BENJAMIN PAUL·Filed 2010·Application pending·0 cites
- 2741US2012156054A1Turbine component with near-surface cooling passage and process thereforLACY BENJAMIN PAUL·Filed 2010·Application pending·0 cites
- 2837US2012167389A1Method for providing a film cooled articleLACY BENJAMIN PAUL·Filed 2011·Application pending·0 cites
- 2934US2012301319A1Curved Passages for a Turbine ComponentLACY BENJAMIN PAUL·Filed 2011·Application pending·0 cites
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