Inventor · disambiguated record
Anthony C. Jones
Also filed as: JONES ANTHONY · JONES ANTHONY C · JONES ANTHONY CHARLES
22 granted patents·1 pending application·330 citations·filing 1998–2013
96Inventor score
Files withHAMILTON SUNDSTRAND CORP10DUONG LOC QUANG3ADAIR DAVID RONALD2BRUNO LOUIS J1HAGSHENAS BEHZAD1
Top patents by PatentIndex Score
23 records- 0189US7055306B2Combined stage single shaft turbofan engineHAMILTON SUNDSTRAND CORP·Filed 2003·Granted Jun 6, 2006·45 cites·26 claims
- 0288US6942451B1Damping system for an expendable gas turbine engineHAMILTON SUNDSTRAND CORP·Filed 2003·Granted Sep 13, 2005·23 cites·12 claims
- 0387US9254924B2Pressure influencing assembly for an aircraft auxiliary systemNAGER ERIC ANDREW·Filed 2011·Granted Feb 9, 2016·14 cites·18 claims
- 0485US8662445B2Hybrid power system architecture for an aircraftHAMILTON SUNDSTRAND CORP·Filed 2013·Granted Mar 4, 2014·9 cites·5 claims
- 0581US8936439B2Radial turbine backface curvature stress reductionDUONG LOC QUANG·Filed 2011·Granted Jan 20, 2015·8 cites·21 claims
- 0681US8500064B2Hybrid power system architecture for an aircraftBRUNO LOUIS J·Filed 2011·Granted Aug 6, 2013·8 cites·8 claims
- 0780US8215115B2Combustor interface sealing arrangementADAIR DAVID RONALD·Filed 2009·Granted Jul 10, 2012·15 cites·19 claims
- 0879US8579591B2Centrifugal compressor impellerHO JOHN CHEN CHIANG·Filed 2010·Granted Nov 12, 2013·10 cites·12 claims
- 0974US9297266B2Method of sealing combustor liner and turbine nozzle interfaceADAIR DAVID RONALD·Filed 2012·Granted Mar 29, 2016·4 cites·19 claims
- 1073US8167540B2System for reducing compressor noiseSCHLINKER ROBERT HANS·Filed 2008·Granted May 1, 2012·9 cites·21 claims
- 1173US6941760B1Start system for expendable gas turbine engineHAMILTON SUNDSTRAND CORP·Filed 2003·Granted Sep 13, 2005·31 cites·17 claims
- 1270US7194866B1Static structure for an expendable gas turbine engineHAMILTON SUNDSTRAND CORP·Filed 2003·Granted Mar 27, 2007·24 cites·15 claims
- 1368US8147208B2Axially segmented impellerHAGSHENAS BEHZAD·Filed 2009·Granted Apr 3, 2012·10 cites·24 claims
- 1467US10087762B2Scallop curvature for radial turbine wheelDUONG LOC QUANG·Filed 2011·Granted Oct 2, 2018·3 cites·28 claims
- 1566US7216473B1Turbojet engine lubrication systemHAMILTON SUNDSTRAND CORP·Filed 1999·Granted May 15, 2007·42 cites·13 claims
- 1664US7748208B2Compact recirculating lubrication system for a miniature gas turbine engineHAMILTON SUNDSTRAND CORP·Filed 2006·Granted Jul 6, 2010·8 cites·22 claims
- 1761US6148601AEngine fuel control system and methodHAMILTON SUNDSTRAND CORP·Filed 1998·Granted Nov 21, 2000·33 cites·13 claims
- 1860US8876484B2Turbine blade pocket pin stress reliefDUONG LOC QUANG·Filed 2011·Granted Nov 4, 2014·1 cites·16 claims
- 1958US8310076B2Gearless turbo-generatorJONES ANTHONY C·Filed 2009·Granted Nov 13, 2012·11 cites·18 claims
- 2058US6896480B1Long term storage capable damping system for an expendable gas turbine engineHAMILTON SUNDSTRAND CORP·Filed 2003·Granted May 24, 2005·6 cites·9 claims
- 2156US8438858B1Rotational system for an expendable gas turbine engineJONES ANTHONY·Filed 2003·Granted May 14, 2013·16 cites·8 claims
- 2245US2008131277A1Ball bearing with carbon-carbon cage for gas turbine enginesHAMILTON SUNDSTRAND CORP·Filed 2006·Application pending·0 cites
- 2340US9279386B2Jet noise reduction using eduction effectPASCU VICTOR·Filed 2012·Granted Mar 8, 2016·0 cites·17 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →