Inventor · disambiguated record
Adam M. Finney
Also filed as: FINNEY ADAM · FINNEY ADAM M
8 granted patents·16 pending applications·81 citations·filing 2009–2024
86Inventor score
Top patents by PatentIndex Score
24 records- 0192US8063501B2Gas turbine bleed energy recovery via counter rotating generatorFINNEY ADAM M·Filed 2009·Granted Nov 22, 2011·31 cites·15 claims
- 0287US8424800B2Multi-source emergency power optimizationFINNEY ADAM M·Filed 2010·Granted Apr 23, 2013·16 cites·20 claims
- 0385US8327651B2Transcritical fluid cooling for aerospace applicationsFINNEY ADAM M·Filed 2009·Granted Dec 11, 2012·21 cites·20 claims
- 0483US9255632B2Integrated torque limiter/no-back deviceFINNEY ADAM M·Filed 2012·Granted Feb 9, 2016·5 cites·11 claims
- 0569US10703462B2Flight control system regenerative brakingHAMILTON SUNDSTRAND CORP·Filed 2017·Granted Jul 7, 2020·2 cites·18 claims
- 0668US8902033B2Sealed inductor connection using litz wireSHEPARD CHARLES·Filed 2012·Granted Dec 2, 2014·2 cites·20 claims
- 0761US8829707B2Methods for aircraft emergency power managementKRENZ MICHAEL·Filed 2010·Granted Sep 9, 2014·3 cites·25 claims
- 0859US10215246B2Integrated torque limiter/no-back deviceHAMILTON SUNDSTRAND CORP·Filed 2015·Granted Feb 26, 2019·1 cites·10 claims
- 0954US2025075931A1System and method for controlling operation of a heat pump configured with an electric heaterCLUFF CHARLES·Filed 2024·Application pending·0 cites
- 1053US2025055282A1Power architecture for self-powered air conditioning systemsCARRIER CORP·Filed 2024·Application pending·0 cites
- 1153US2023288086A1Systems and methods for defrost control in heat pumpsCARRIER CORP·Filed 2023·Application pending·0 cites
- 1245US2014196469A1Low pressure compressor bleed exit for an aircraft pressurization systemHAMILTON SUNDSTRAND CORP·Filed 2014·Application pending·0 cites
- 1343US2013278370A1Spring-supported inductor coreFINNEY ADAM M·Filed 2012·Application pending·0 cites
- 1441US2013076035A1Motor-generator turbomachine starterKOENIG ANDREAS C·Filed 2011·Application pending·0 cites
- 1541US2013040545A1Low pressure compressor bleed exit for an aircraft pressurization systemHAMILTON SUNDSTRAND CORP·Filed 2011·Application pending·0 cites
- 1641US2013031912A1Gas turbine start architectureHAMILTON SUNDSTRAND CORP·Filed 2011·Application pending·0 cites
- 1739US2014001901A1Electric motor with a redundant seal arrangementFINNEY ADAM M·Filed 2012·Application pending·0 cites
- 1837US2013055724A1Gas turbine engine air cycle systemFINNEY ADAM M·Filed 2011·Application pending·0 cites
- 1937US2012297780A1Active fuel temperature controlBRUNO LOUIS J·Filed 2011·Application pending·0 cites
- 2036US2012138737A1Aircraft power distribution architectureBRUNO LOUIS J·Filed 2011·Application pending·0 cites
- 2136US2012221157A1Low pressure spool emergency generatorFINNEY ADAM M·Filed 2011·Application pending·0 cites
- 2236US2012312037A1Vapor cycle system with de-superheaterFINNEY ADAM M·Filed 2011·Application pending·0 cites
- 2335US2012036866A1Auxiliary power unit with multiple fuel sourcesFINNEY ADAM M·Filed 2010·Application pending·0 cites
- 2435US2012192578A1Gas turbine bleed ecs coolingFINNEY ADAM M·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →