Inventor · disambiguated record
Jonathan Jeffery Eastwood
Also filed as: EASTWOOD JONATHAN J · EASTWOOD JONATHAN JEFFERY
39 granted patents·6 pending applications·152 citations·filing 2009–2020
97Inventor score
Top patents by PatentIndex Score
45 records- 0194US10684017B2Passage geometry for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 16, 2020·19 cites·7 claims
- 0292US10288289B2Gas turbine engine diffuser-combustor assembly inner casingUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 14, 2019·7 cites·12 claims
- 0392US10215411B2Combustor panels having recessed railUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 26, 2019·7 cites·12 claims
- 0492US10161414B2High compressor exit guide vane assembly to pre-diffuser junctionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 25, 2018·9 cites·15 claims
- 0591US10612466B2Gas turbine engine active clearance control system using inlet particle separatorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 7, 2020·8 cites·11 claims
- 0691US10344623B2Pre-diffuser strut for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 9, 2019·6 cites·16 claims
- 0790US10830448B2Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 10, 2020·5 cites·20 claims
- 0888US9377198B2Heat shield for a combustorEASTWOOD JONATHAN JEFFERY·Filed 2012·Granted Jun 28, 2016·10 cites·27 claims
- 0987US10914187B2Active clearance control system and manifold for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 9, 2021·6 cites·20 claims
- 1087US10731858B2Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 4, 2020·10 cites·15 claims
- 1187US10648666B2Angled combustor liner cooling holes through transverse structure within a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 12, 2020·10 cites·13 claims
- 1287US8572979B2Gas turbine combustor liner cap assemblySMITH CRAIG F·Filed 2010·Granted Nov 5, 2013·14 cites·19 claims
- 1386US8839627B2Annular combustorEASTWOOD JONATHAN JEFFERY·Filed 2012·Granted Sep 23, 2014·10 cites·11 claims
- 1485US10753222B2Gas turbine engine blade outer air sealUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 25, 2020·5 cites·16 claims
- 1583US10808540B2Case for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 20, 2020·4 cites·17 claims
- 1676US10100675B2Outer diffuser case for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 16, 2018·2 cites·16 claims
- 1768US10208949B2System and apparatus for combustion swirler anti-rotationUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 19, 2019·1 cites·13 claims
- 1867US8523514B2Composite slider seal for turbojet penetrationEASTWOOD JONATHAN JEFFERY·Filed 2009·Granted Sep 3, 2013·10 cites·12 claims
- 1965US11287132B2Quench aperture body for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2020·Granted Mar 29, 2022·0 cites·9 claims
- 2065US10690348B2Turbine engine combustor heat shield with one or more cooling elementsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 23, 2020·2 cites·13 claims
- 2165US10519811B2Flange heat shieldUNITED TECHNOLOGIES CORP·Filed 2016·Granted Dec 31, 2019·1 cites·13 claims
- 2263US9297536B2Gas turbine engine combustor surge retentionEASTWOOD JONATHAN JEFFERY·Filed 2012·Granted Mar 29, 2016·2 cites·22 claims
- 2361US10571125B2Quench aperture body for a turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 25, 2020·1 cites·10 claims
- 2461US10240790B2Turbine engine combustor heat shield with multi-height railsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 26, 2019·1 cites·15 claims
- 2561US10215410B2Turbine engine combustor heat shield with multi-angled cooling aperturesUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 26, 2019·2 cites·13 claims
- 2657US11047575B2Combustor heat shield panelUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 29, 2021·0 cites·16 claims
- 2755US10670269B2Cast combustor liner panel gating feature for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 2, 2020·0 cites·14 claims
- 2855US10551065B2Heat shield for a combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 4, 2020·0 cites·15 claims
- 2954US10655856B2Dilution passage arrangement for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 19, 2020·0 cites·18 claims
- 3053US10774685B2Gas turbine engine exhaust componentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 15, 2020·0 cites·15 claims
- 3152US11143032B2Turbine rotor locking assembly and methodUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 12, 2021·0 cites·6 claims
- 3252US10808928B2Boss for combustor panelUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 20, 2020·0 cites·4 claims
- 3352US10669939B2Combustor seal for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 2, 2020·0 cites·19 claims
- 3451US10823410B2Cast combustor liner panel radius for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 3, 2020·0 cites·14 claims
- 3547US10550725B2Engine cases and associated flangeUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 4, 2020·0 cites·12 claims
- 3645US2020131916A1Turbine blade assemblyUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 3744US10746049B2Gas turbine engine case including bearing compartmentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 18, 2020·0 cites·20 claims
- 3844US10087767B2Pre-diffuser with multiple radiiUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 2, 2018·0 cites·13 claims
- 3942US2018283690A1Combustor panel heat transfer pins with varying geometric specificationsUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 4041US2018128485A1Stud arrangement for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 4140US10260750B2Combustor panels having angled railUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 16, 2019·0 cites·12 claims
- 4240US10041364B2Inner diffuser case cone and skirtUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 7, 2018·0 cites·21 claims
- 4340US2019078459A1Active clearance control system for gas turbine engine with power turbineUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 4434US2016245104A1Gas turbine engine and turbine configurationsUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 4534US2016290642A1Combustor configurations for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →