Inventor · disambiguated record
Jason Smoke
Also filed as: SMOKE JASON · SMOKE JASON C
49 granted patents·11 pending applications·469 citations·filing 2003–2025
98Inventor score
Top patents by PatentIndex Score
60 records- 0197US8408446B1Methods and tooling assemblies for the manufacture of metallurgically-consolidated turbine engine componentsSMOKE JASON·Filed 2012·Granted Apr 2, 2013·41 cites·20 claims
- 0296US11181006B2Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangementHONEYWELL INT INC·Filed 2020·Granted Nov 23, 2021·17 cites·20 claims
- 0396US10907487B2Turbine shroud assemblies for gas turbine enginesHONEYWELL INT INC·Filed 2018·Granted Feb 2, 2021·24 cites·20 claims
- 0496US8668442B2Turbine nozzles and methods of manufacturing the sameMORRIS MARK C·Filed 2010·Granted Mar 11, 2014·19 cites·19 claims
- 0595US8047771B2Turbine nozzles and methods of manufacturing the sameHONEYWELL INT INC·Filed 2008·Granted Nov 1, 2011·24 cites·20 claims
- 0694US10857596B1Method of producing an abrasive tip for a turbine bladeHONEYWELL INT INC·Filed 2018·Granted Dec 8, 2020·9 cites·20 claims
- 0794US10677084B2Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangementHONEYWELL INT INC·Filed 2018·Granted Jun 9, 2020·10 cites·20 claims
- 0894US7625178B2High effectiveness cooled turbine bladeHONEYWELL INT INC·Filed 2006·Granted Dec 1, 2009·55 cites·20 claims
- 0993US11156116B2Turbine nozzle with reduced leakage feather sealsHONEYWELL INT INC·Filed 2019·Granted Oct 26, 2021·6 cites·14 claims
- 1093US9726022B2Axially-split radial turbinesHONEYWELL INT INC·Filed 2015·Granted Aug 8, 2017·12 cites·18 claims
- 1192US12091980B1Spring biased shroud retention system for gas turbine engineHONEYWELL INT INC·Filed 2023·Granted Sep 17, 2024·3 cites·20 claims
- 1292US10900378B2Turbine tip shroud assembly with plural shroud segments having internal cooling passagesHONEYWELL INT INC·Filed 2018·Granted Jan 26, 2021·7 cites·11 claims
- 1392US7610946B2Cooled turbine blade cast tip recessHONEYWELL INT INC·Filed 2007·Granted Nov 3, 2009·21 cites·11 claims
- 1491US10385433B2Methods for processing bonded dual alloy rotors including differential heat treatment processesHONEYWELL INT INC·Filed 2016·Granted Aug 20, 2019·2 cites·20 claims
- 1591US9938834B2Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereofHONEYWELL INT INC·Filed 2015·Granted Apr 10, 2018·5 cites·19 claims
- 1690US11506060B1Radial turbine rotor for gas turbine engineHONEYWELL INT INC·Filed 2021·Granted Nov 22, 2022·4 cites·20 claims
- 1790US9033670B2Axially-split radial turbines and methods for the manufacture thereofMITTENDORF DON·Filed 2012·Granted May 19, 2015·13 cites·18 claims
- 1888US9850760B2Directed cooling for rotating machineryHONEYWELL INT INC·Filed 2015·Granted Dec 26, 2017·6 cites·8 claims
- 1988US8381533B2Direct transfer axial tangential onboard injector system (TOBI) with self-supporting seal plateHONEYWELL INT INC·Filed 2009·Granted Feb 26, 2013·33 cites·18 claims
- 2087US11525401B2Impingement baffle for gas turbine engineHONEYWELL INT INC·Filed 2021·Granted Dec 13, 2022·2 cites·20 claims
- 2187US10260355B2Diverging-converging cooling passage for a turbine bladeHONEYWELL INT INC·Filed 2016·Granted Apr 16, 2019·5 cites·20 claims
- 2287US9724780B2Dual alloy turbine rotors and methods for manufacturing the sameHONEYWELL INT INC·Filed 2014·Granted Aug 8, 2017·5 cites·11 claims
- 2385US10563520B2Turbine component with shaped cooling pinsHONEYWELL INT INC·Filed 2017·Granted Feb 18, 2020·3 cites·17 claims
- 2485US8388307B2Turbine nozzle assembly including radially-compliant spring member for gas turbine engineSMOKE JASON·Filed 2009·Granted Mar 5, 2013·26 cites·17 claims
- 2583US10036254B2Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereofHONEYWELL INT INC·Filed 2015·Granted Jul 31, 2018·4 cites·13 claims
- 2677US11897065B2Composite turbine disc rotor for turbomachineHONEYWELL INT INC·Filed 2020·Granted Feb 13, 2024·1 cites·18 claims
- 2777US11293292B2Turbine scroll assembly for gas turbine engineHONEYWELL INT INC·Filed 2020·Granted Apr 5, 2022·1 cites·15 claims
- 2876US8534076B2Combustor-turbine seal interface for gas turbine engineWOODCOCK GREGORY O·Filed 2009·Granted Sep 17, 2013·16 cites·19 claims
- 2975US7097411B2Turbomachine compressor scroll with load-carrying inlet vanesHONEYWELL INT INC·Filed 2004·Granted Aug 29, 2006·33 cites·30 claims
- 3071US10669862B2Airfoil with leading edge convective cooling systemHONEYWELL INT INC·Filed 2018·Granted Jun 2, 2020·1 cites·18 claims
- 3171US10655859B2Turbine scroll assembly for gas turbine engineHONEYWELL INT INC·Filed 2017·Granted May 19, 2020·1 cites·18 claims
- 3270US8616832B2Turbine assemblies with impingement coolingSMOKE JASON·Filed 2009·Granted Dec 31, 2013·10 cites·20 claims
- 3370US8262342B2Gas turbine engine assemblies with recirculated hot gas ingestionMORRIS MARK C·Filed 2008·Granted Sep 11, 2012·12 cites·20 claims
- 3470US2025372290A1Magnetic array support structureHONEYWELL INT INC·Filed 2025·Application pending·0 cites
- 3568US9670781B2Gas turbine engines with turbine rotor blades having improved platform edgesHONEYWELL INT INC·Filed 2013·Granted Jun 6, 2017·3 cites·13 claims
- 3668US9506365B2Gas turbine engine components having sealed stress relief slots and methods for the fabrication thereofHONEYWELL INT INC·Filed 2014·Granted Nov 29, 2016·3 cites·19 claims
- 3766US6968697B2Integral compressor housing of gas turbine enginesHONEYWELL INT INC·Filed 2003·Granted Nov 29, 2005·25 cites·27 claims
- 3865US2021372289A1Turbine nozzle with reduced leakage feather sealsHONEYWELL INT INC·Filed 2021·Application pending·0 cites
- 3964US10954801B2Cooling circuit with shaped cooling pinsHONEYWELL INT INC·Filed 2019·Granted Mar 23, 2021·0 cites·18 claims
- 4062US10669617B2Methods for processing bonded dual alloy rotors including differential heat treatment processesHONEYWELL INT INC·Filed 2019·Granted Jun 2, 2020·0 cites·16 claims
- 4160US12345173B2Gas turbine engines and methods for reducing spool thrust in a turbine section thereofHONEYWELL INT INC·Filed 2023·Granted Jul 1, 2025·0 cites·20 claims
- 4260US2021140343A1Turbine tip shroud assembly with plural shroud segments having internal cooling passagesHONEYWELL INT INC·Filed 2020·Application pending·0 cites
- 4360US2020353577A1Turbine wheels, turbine engines including the same, and methods of fabricating turbine wheels with improved bond line geometryHONEYWELL INT INC·Filed 2020·Application pending·0 cites
- 4459US12442316B1Shroud system with two-stage spring and retainer system for gas turbine engine shroudHONEYWELL INT INC·Filed 2025·Granted Oct 14, 2025·0 cites·20 claims
- 4559US9844826B2Methods for manufacturing a turbine nozzle with single crystal alloy nozzle segmentsHONEYWELL INT INC·Filed 2014·Granted Dec 19, 2017·1 cites·13 claims
- 4658US12421906B2Gas turbine engines and methods for reducing spool thrust in a combustor section thereofHONEYWELL INT INC·Filed 2024·Granted Sep 23, 2025·0 cites·20 claims
- 4758US10399176B2Dual alloy turbine rotors and methods for manufacturing the sameHONEYWELL INT INC·Filed 2017·Granted Sep 3, 2019·0 cites·19 claims
- 4858US2023271150A1High temperature thermal process systemsHONEYWELL INT INC·Filed 2022·Application pending·0 cites
- 4957US8147197B2Turbine blade platformMORRIS MARK C·Filed 2009·Granted Apr 3, 2012·3 cites·20 claims
- 5056US10751843B2Turbine wheels, turbine engines including the same, and methods of fabricating turbine wheels with improved bond line geometryHONEYWELL INT INC·Filed 2017·Granted Aug 25, 2020·0 cites·16 claims
Showing the top 50 of 60 patent records by PatentIndex Score.
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