Inventor · disambiguated record
John H. Mosley
Also filed as: MOSLEY JOHN H
11 granted patents·2 pending applications·62 citations·filing 2002–2025
88Inventor score
Top patents by PatentIndex Score
13 records- 0190US9803502B2Cooling passages for a mid-turbine frameUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 31, 2017·6 cites·13 claims
- 0288US10215098B2Bearing compartment sealUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 26, 2019·5 cites·17 claims
- 0386US9091173B2Turbine coolant supply systemMOSLEY JOHN H·Filed 2012·Granted Jul 28, 2015·21 cites·17 claims
- 0483US10072585B2Gas turbine engine turbine impeller pressurizationUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 11, 2018·8 cites·11 claims
- 0583US9920651B2Cooling passages for a mid-turbine frameUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 20, 2018·4 cites·16 claims
- 0680US11578668B2Gas turbine engine control based on characteristic of cooled airUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 14, 2023·3 cites·2 claims
- 0778US10443498B2Gas turbine engine cooling fluid metering systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 15, 2019·3 cites·13 claims
- 0857US11939919B2Gas turbine engine cooling fluid metering systemUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 26, 2024·0 cites·20 claims
- 0957US2025257692A1Thermal conditioning assembly for a gas turbine engineRTX CORP·Filed 2025·Application pending·0 cites
- 1050US6884023B2Integral swirl knife edge injection assemblyUNITED TECHNOLOGIES CORP·Filed 2002·Granted Apr 26, 2005·12 cites·18 claims
- 1149US10815891B2Inner diffuser case struts for a combustor of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 27, 2020·0 cites·2 claims
- 1248US9995171B2Cooling passages for a mid-turbine frameUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·0 cites·10 claims
- 1346US2021317785A1Cooling system for a gas turbine engineRAYTHEON TECH CORP·Filed 2020·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →