Inventor · disambiguated record
Jeffrey S. Beattie
Also filed as: BEATTIE JEFFREY · BEATTIE JEFFREY S
26 granted patents·3 pending applications·153 citations·filing 2004–2019
95Inventor score
Files withUNITED TECHNOLOGIES CORP20BEATTIE JEFFREY S3SPANGLER BRANDON W2LEVINE JEFFREY R1ROMANELLI IV JAMES1
Top patents by PatentIndex Score
29 records- 0193US7121800B2Turbine blade nested seal damper assemblyUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 17, 2006·69 cites·27 claims
- 0291US9279331B2Gas turbine engine airfoil with dirt purge feature and core for making sameLEVINE JEFFREY R·Filed 2012·Granted Mar 8, 2016·6 cites·18 claims
- 0387US8356978B2Turbine airfoil platform cooling coreUNITED TECHNOLOGIES CORP·Filed 2009·Granted Jan 22, 2013·26 cites·18 claims
- 0486US10907481B2Platform cooling core for a gas turbine engine rotor bladeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 2, 2021·3 cites·21 claims
- 0586US10100648B2Damper seal installation featuresUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 16, 2018·4 cites·13 claims
- 0685US9938837B2Gas turbine engine airfoil trailing edge passage and core for making sameUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 10, 2018·4 cites·9 claims
- 0783US10364682B2Platform cooling core for a gas turbine engine rotor bladeUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 30, 2019·6 cites·16 claims
- 0879US9422817B2Turbine blade root with microcircuit cooling passagesBEATTIE JEFFREY S·Filed 2012·Granted Aug 23, 2016·2 cites·20 claims
- 0977US9932834B2Rotor blade with a conic spline fillet at an intersection between a platform and a neckUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 3, 2018·5 cites·22 claims
- 1076US9587495B2Mistake proof damper pocket sealsBEATTIE JEFFREY S·Filed 2012·Granted Mar 7, 2017·5 cites·12 claims
- 1169US8942837B2Method for inspecting a manufacturing deviceROMANELLI JAMES·Filed 2012·Granted Jan 27, 2015·2 cites·4 claims
- 1269US8240987B2Gas turbine engine systems involving baffle assembliesSPANGLER BRANDON W·Filed 2008·Granted Aug 14, 2012·11 cites·14 claims
- 1365US10533453B2Engine component having platform with passagewayUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 14, 2020·1 cites·17 claims
- 1463US9546556B2Turbine blade root profileUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jan 17, 2017·2 cites·25 claims
- 1562US9243500B2Turbine blade platform with U-channel cooling holesZELESKY MARK F·Filed 2012·Granted Jan 26, 2016·2 cites·15 claims
- 1660US10227875B2Gas turbine engine component with combined mate face and platform coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 12, 2019·2 cites·14 claims
- 1760US10180067B2Mate face cooling holes for gas turbine engine componentBEATTIE JEFFREY S·Filed 2012·Granted Jan 15, 2019·2 cites·19 claims
- 1857US10253642B2Gas turbine engine with disk having periphery with protrusionsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 9, 2019·1 cites·16 claims
- 1957US2015153726A1Method for inspecting a manufacturing deviceROMANELLI IV JAMES·Filed 2014·Application pending·0 cites
- 2052US10167722B2Disk outer rim sealUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 1, 2019·0 cites·18 claims
- 2149US10822952B2Feature to provide cooling flow to diskUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 3, 2020·0 cites·8 claims
- 2248US10563525B2Blade feature to support segmented coverplateUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 18, 2020·0 cites·29 claims
- 2348US10301958B2Gas turbine engine with seal having protrusionsUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 28, 2019·0 cites·16 claims
- 2447US10203196B2Inspecting one or more apertures of a component using moldable materialUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 12, 2019·0 cites·17 claims
- 2546US2008131285A1RMC-defined tip blowing slots for turbine bladesUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 2645US10247023B2Seal damper with improved retentionUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 2, 2019·0 cites·12 claims
- 2744US2016305254A1Rotor blade platform cooling passageUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2840US10226814B2Cast component having corner radius to reduce recrystallizationUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 12, 2019·0 cites·18 claims
- 2940US8257045B2Platforms with curved side edges and gas turbine engine systems involving such platformsSPANGLER BRANDON W·Filed 2008·Granted Sep 4, 2012·0 cites·21 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →