Inventor

THOMAS RUSSELL H

US10 patents

⚠️ This page may combine multiple inventors who share the name “THOMAS RUSSELL H”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

NASA

2 patents

US8015819B2Sep 13, 2011

Wet active chevron nozzle for controllable jet noise reduction

NASA9 citations82

US9669921B2Jun 6, 2017

Active aircraft pylon noise control system

NASA0 citations46

THOMAS RUSSELL H

2 patents

US9022311B2May 5, 2015

Active aircraft pylon noise control system

THOMAS RUSSELL H7 citations75

US8876043B2Nov 4, 2014

Aircraft engine exhaust nozzle system for jet noise reduction

THOMAS RUSSELL H0 citations44

VIRGINIA POLYTECHNIC INST

1 patent

US5515444AMay 7, 1996

Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors

VIRGINIA POLYTECHNIC INST98 citations92

INNOVATIVE TECH CENTER

1 patent

US5355417AOct 11, 1994

Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors

INNOVATIVE TECH CENTER78 citations92

DEFENSE RESEARCH TECHNOLOGIES

1 patent

US5662136ASep 2, 1997

Acousto-fluidic driver for active control of turbofan engine noise

DEFENSE RESEARCH TECHNOLOGIES22 citations90

JONES MICHAEL G

1 patent

US9623952B1Apr 18, 2017

External acoustic liners for multi-functional aircraft noise reduction

JONES MICHAEL G8 citations81

MENGLE VINOD G

1 patent

US8157207B2Apr 17, 2012

Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods

MENGLE VINOD G14 citations79

CZECH MICHAEL J

1 patent

US8651429B2Feb 18, 2014

Blended cutout flap for reduction of jet-flap interaction noise

CZECH MICHAEL J2 citations53