Inventor · disambiguated record
Russell H. Thomas
Also filed as: THOMAS RUSSELL H
10 granted patents·238 citations·filing 1992–2015
89Inventor score
Files withNASA2THOMAS RUSSELL H2CZECH MICHAEL J1DEFENSE RESEARCH TECHNOLOGIES1INNOVATIVE TECH CENTER1
Top patents by PatentIndex Score
10 records- 0188US5515444AActive control of aircraft engine inlet noise using compact sound sources and distributed error sensorsVIRGINIA POLYTECHNIC INST·Filed 1994·Granted May 7, 1996·98 cites·6 claims
- 0284US5355417AActive control of aircraft engine inlet noise using compact sound sources and distributed error sensorsINNOVATIVE TECH CENTER·Filed 1992·Granted Oct 11, 1994·78 cites·14 claims
- 0380US9623952B1External acoustic liners for multi-functional aircraft noise reductionJONES MICHAEL G·Filed 2012·Granted Apr 18, 2017·8 cites·15 claims
- 0472US9022311B2Active aircraft pylon noise control systemTHOMAS RUSSELL H·Filed 2011·Granted May 5, 2015·7 cites·12 claims
- 0570US8015819B2Wet active chevron nozzle for controllable jet noise reductionNASA·Filed 2006·Granted Sep 13, 2011·9 cites·23 claims
- 0668US8157207B2Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methodsMENGLE VINOD G·Filed 2007·Granted Apr 17, 2012·14 cites·22 claims
- 0757US5662136AAcousto-fluidic driver for active control of turbofan engine noiseDEFENSE RESEARCH TECHNOLOGIES·Filed 1995·Granted Sep 2, 1997·22 cites·26 claims
- 0849US8651429B2Blended cutout flap for reduction of jet-flap interaction noiseCZECH MICHAEL J·Filed 2011·Granted Feb 18, 2014·2 cites·10 claims
- 0944US9669921B2Active aircraft pylon noise control systemNASA·Filed 2015·Granted Jun 6, 2017·0 cites·4 claims
- 1034US8876043B2Aircraft engine exhaust nozzle system for jet noise reductionTHOMAS RUSSELL H·Filed 2011·Granted Nov 4, 2014·0 cites·20 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →