Inventor · disambiguated record
Jeffrey Michael Jacques
Also filed as: JACQUES JEFFREY M · JACQUES JEFFREY MICHAEL
23 granted patents·2 pending applications·67 citations·filing 2012–2023
93Inventor score
Files withUNITED TECHNOLOGIES CORP15RAYTHEON TECH CORP5BEATTIE JEFFREY S3MOON FRANCIS R1ZELESKY MARK F1
Top patents by PatentIndex Score
25 records- 0196US10370991B2Gas turbine engine and seal assembly thereforeUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·18 cites·17 claims
- 0289US11287045B2Seal ringUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 29, 2022·4 cites·6 claims
- 0389US10436051B2Seal support structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 8, 2019·6 cites·12 claims
- 0487US10443450B2Seal support structure for a circumferential seal of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 15, 2019·4 cites·14 claims
- 0587US9963991B2Brush seal plateUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 8, 2018·5 cites·17 claims
- 0684US10018062B2Axial transfer tubeUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 10, 2018·4 cites·16 claims
- 0782US11306619B2Seal support structure for a circumferential seal of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 19, 2022·2 cites·12 claims
- 0881US11377967B2Pre-formed faceted turbine blade damper sealUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 5, 2022·3 cites·20 claims
- 0980US10801348B2Non-contacting dynamic sealUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 13, 2020·2 cites·3 claims
- 1079US9422817B2Turbine blade root with microcircuit cooling passagesBEATTIE JEFFREY S·Filed 2012·Granted Aug 23, 2016·2 cites·20 claims
- 1176US9587495B2Mistake proof damper pocket sealsBEATTIE JEFFREY S·Filed 2012·Granted Mar 7, 2017·5 cites·12 claims
- 1273US2023296028A1Non-contacting dynamic sealRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 1370US10301951B2Turbine vane gussetUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 28, 2019·2 cites·16 claims
- 1469US11674401B2Non-contacting dynamic sealRAYTHEON TECH CORP·Filed 2020·Granted Jun 13, 2023·0 cites·19 claims
- 1563US9546556B2Turbine blade root profileUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jan 17, 2017·2 cites·25 claims
- 1662US9243500B2Turbine blade platform with U-channel cooling holesZELESKY MARK F·Filed 2012·Granted Jan 26, 2016·2 cites·15 claims
- 1761US8607574B1Turbine engine exhaust nozzle flapMOON FRANCIS R·Filed 2012·Granted Dec 17, 2013·2 cites·17 claims
- 1860US10227875B2Gas turbine engine component with combined mate face and platform coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 12, 2019·2 cites·14 claims
- 1960US10180067B2Mate face cooling holes for gas turbine engine componentBEATTIE JEFFREY S·Filed 2012·Granted Jan 15, 2019·2 cites·19 claims
- 2053US12180857B2Turbine airfoil attachment with serration profileRAYTHEON TECH CORP·Filed 2023·Granted Dec 31, 2024·0 cites·17 claims
- 2153US2016109025A1Seal ringUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 2248US11225875B1Rail support beamsRAYTHEON TECH CORP·Filed 2021·Granted Jan 18, 2022·0 cites·20 claims
- 2345US11773731B2Bathtub damper seal arrangement for gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Oct 3, 2023·0 cites·20 claims
- 2445US10247023B2Seal damper with improved retentionUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 2, 2019·0 cites·12 claims
- 2540US10385705B2Gas turbine engine having a vane assemblyUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 20, 2019·0 cites·10 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →