Inventor · disambiguated record
Om P. Sharma
Also filed as: SHARMA OM · SHARMA OM P · SHARMA OM PARKASH
32 granted patents·7 pending applications·655 citations·filing 1994–2023
97Inventor score
Files withUNITED TECHNOLOGIES CORP30RAYTHEON TECH CORP4SHARMA OM P3DASGUPTA ARINDAM1SUCIU GABRIEL L1
Top patents by PatentIndex Score
39 records- 0193US5525038ARotor airfoils to control tip leakage flowsUNITED TECHNOLOGIES CORP·Filed 1994·Granted Jun 11, 1996·128 cites·6 claims
- 0292US11655778B2Morphing structures for fan inlet variable vanesRAYTHEON TECH CORP·Filed 2021·Granted May 23, 2023·3 cites·20 claims
- 0391US7371049B2Manufacturable and inspectable microcircuit cooling for bladesUNITED TECHNOLOGIES CORP·Filed 2005·Granted May 13, 2008·35 cites·28 claims
- 0490US6619909B2Casing treatment for a fluid compressorUNITED TECHNOLOGIES CORP·Filed 2001·Granted Sep 16, 2003·53 cites·15 claims
- 0589US6231301B1Casing treatment for a fluid compressorUNITED TECHNOLOGIES CORP·Filed 1998·Granted May 15, 2001·77 cites·18 claims
- 0687US7311497B2Manufacturable and inspectable microcircuitsUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 25, 2007·25 cites·19 claims
- 0786US11162416B2Attritable engine integrated with vehicleUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 2, 2021·3 cites·18 claims
- 0886US10619483B2Partially shrouded gas turbine engine fanUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 14, 2020·5 cites·17 claims
- 0986US5486091AGas turbine airfoil clockingUNITED TECHNOLOGIES CORP·Filed 1994·Granted Jan 23, 1996·81 cites·7 claims
- 1085US7984607B2Gas turbine engine systems and related methods involving vane-blade count ratios greater than unityUNITED TECHNOLOGIES CORP·Filed 2007·Granted Jul 26, 2011·21 cites·8 claims
- 1185US7513040B2Manufacturable and inspectable cooling microcircuits for blade-outer-air-sealsUNITED TECHNOLOGIES CORP·Filed 2005·Granted Apr 7, 2009·20 cites·10 claims
- 1284US11156156B2Gas turbine engine with a unitary structure and method for manufacturing the sameUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 26, 2021·3 cites·18 claims
- 1384US7726937B2Turbine engine compressor vanesUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jun 1, 2010·30 cites·24 claims
- 1484US7322796B2Turbine vane constructionUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jan 29, 2008·23 cites·16 claims
- 1584US6059522ACompressor stall diagnostics and avoidanceUNITED TECHNOLOGIES CORP·Filed 1996·Granted May 9, 2000·62 cites·13 claims
- 1683US8292570B2Low pressure turbine with counter-rotating drives for single spoolSUCIU GABRIEL L·Filed 2008·Granted Oct 23, 2012·19 cites·7 claims
- 1782US7942632B2Variable-shape variable-stagger inlet guide vane flapUNITED TECHNOLOGIES CORP·Filed 2007·Granted May 17, 2011·20 cites·15 claims
- 1881US11519289B2Systems and methods for hybrid electric turbine enginesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Dec 6, 2022·2 cites·20 claims
- 1981US8973374B2Blades in a turbine section of a gas turbine engineSHARMA OM P·Filed 2011·Granted Mar 10, 2015·7 cites·11 claims
- 2080US11904405B2Additively controlled surface roughness for designed performanceRAYTHEON TECH CORP·Filed 2022·Granted Feb 20, 2024·0 cites·5 claims
- 2179US7413406B2Turbine blade with radial cooling channelsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Aug 19, 2008·20 cites·20 claims
- 2277US11199136B2Additively manufactured thermally insulating structureUNITED TECHNOLOGIES CORP·Filed 2018·Granted Dec 14, 2021·2 cites·17 claims
- 2377US10808545B2Gas turbine engine fan blade, design, and fabricationUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 20, 2020·2 cites·21 claims
- 2474US12247529B2Morphing structures for fan inlet variable vanesRAYTHEON TECH CORP·Filed 2023·Granted Mar 11, 2025·0 cites·19 claims
- 2571US8468797B2Gas turbine engine systems and related methods involving vane-blade count ratios greater than unitySHARMA OM P·Filed 2011·Granted Jun 25, 2013·4 cites·11 claims
- 2670US11242769B2Additively controlled surface roughness for designed performanceUNITED TECHNOLOGIES CORP·Filed 2018·Granted Feb 8, 2022·0 cites·7 claims
- 2765US7594794B2Leaned high pressure compressor inlet guide vaneUNITED TECHNOLOGIES CORP·Filed 2006·Granted Sep 29, 2009·10 cites·22 claims
- 2863US11988140B2Gas turbine engine inlet wall designRAYTHEON TECH CORP·Filed 2021·Granted May 21, 2024·0 cites·14 claims
- 2954US11136895B2Spiraling grooves as a hub treatment for cantilevered stators in compressorsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 5, 2021·0 cites·10 claims
- 3050US10330010B2Compressor core inner diameter coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 25, 2019·0 cites·18 claims
- 3149US10907544B2Gas turbine engine inlet wall designUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 2, 2021·0 cites·12 claims
- 3248US8516793B2Gas turbine engine systems and related methods involving vane-blade count ratios greater than unitySHARMA OM P·Filed 2011·Granted Aug 27, 2013·0 cites·7 claims
- 3346US2020182155A1Casing with integral cavityUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 3445US2020318549A1Non-axisymmetric combustor for improved durabilityUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 3544US2020191061A1Integrated additive bladder for charging and insulation of small attritable engineUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 3644US2015227677A1Gas Turbine Engine With First Turbine Vane ClockingUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 3743US2009116956A1Manufacturable and inspectable cooling microcircuits for blade-outer-air-sealsUNITED TECHNOLOGIES CORP·Filed 2009·Application pending·0 cites
- 3842US2020248560A1Tandem fan for boundary layer ingestion systemsUNITED TECHNOLOGIES CORP·Filed 2020·Application pending·0 cites
- 3937US2013239542A1Structures and methods for intercooling aircraft gas turbine enginesDASGUPTA ARINDAM·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →