Inventor
SNYDER TIMOTHY S
US77 patents
⚠️ This page may combine multiple inventors who share the name “SNYDER TIMOTHY S”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
29 patentsUS6810673B2Nov 2, 2004
Low emissions combustor for a gas turbine engine
UNITED TECHNOLOGIES CORP177 citations99
US6606861B2Aug 19, 2003
Low emissions combustor for a gas turbine engine
UNITED TECHNOLOGIES CORP181 citations99
US5706643AJan 13, 1998
Active gas turbine combustion control to minimize nitrous oxide emissions
UNITED TECHNOLOGIES CORP69 citations95
US7195456B2Mar 27, 2007
Turbine engine guide vane and arrays thereof
UNITED TECHNOLOGIES CORP59 citations94
US6176087B1Jan 23, 2001
Bluff body premixing fuel injector and method for premixing fuel and air
UNITED TECHNOLOGIES CORP52 citations94
US7007864B2Mar 7, 2006
Fuel nozzle design
UNITED TECHNOLOGIES CORP30 citations93
US5899076AMay 4, 1999
Flame disgorging two stream tangential entry nozzle
UNITED TECHNOLOGIES CORP20 citations92
US5256352AOct 26, 1993
Air-liquid mixer
UNITED TECHNOLOGIES CORP51 citations92
US6513329B1Feb 4, 2003
Premixing fuel and air
UNITED TECHNOLOGIES CORP32 citations91
US5461865AOct 31, 1995
Tangential entry fuel nozzle
UNITED TECHNOLOGIES CORP45 citations91
US5479773AJan 2, 1996
Tangential air entry fuel nozzle
UNITED TECHNOLOGIES CORP29 citations88
US10794596B2Oct 6, 2020
Dual fuel nozzle with liquid filming atomization for a gas turbine engine
UNITED TECHNOLOGIES CORP13 citations84
US9851105B2Dec 26, 2017
Self-cooled orifice structure
UNITED TECHNOLOGIES CORP7 citations84
US7798765B2Sep 21, 2010
Out-flow margin protection for a gas turbine engine
UNITED TECHNOLOGIES CORP14 citations84
US10228137B2Mar 12, 2019
Dual fuel nozzle with swirling axial gas injection for a gas turbine engine
UNITED TECHNOLOGIES CORP9 citations83
US9194585B2Nov 24, 2015
Cooling for combustor liners with accelerating channels
UNITED TECHNOLOGIES CORP10 citations82
US10317080B2Jun 11, 2019
Co-swirl orientation of combustor effusion passages for gas turbine engine combustor
UNITED TECHNOLOGIES CORP9 citations80
US5896739AApr 27, 1999
Method of disgorging flames from a two stream tangential entry nozzle
UNITED TECHNOLOGIES CORP14 citations74
US5865609AFeb 2, 1999
Method of combustion with low acoustics
UNITED TECHNOLOGIES CORP11 citations74
US11725818B2Aug 15, 2023
Bluff-body piloted high-shear injector and method of using same
UNITED TECHNOLOGIES CORP2 citations73
US11506390B2Nov 22, 2022
Multi-fuel bluff-body piloted high-shear injector and method of using same
UNITED TECHNOLOGIES CORP5 citations73
US11236906B2Feb 1, 2022
Combustor cooled quench zone array
UNITED TECHNOLOGIES CORP2 citations73
US10094563B2Oct 9, 2018
Microcircuit cooling for gas turbine engine combustor
UNITED TECHNOLOGIES CORP2 citations73
US10240533B2Mar 26, 2019
Fuel distribution within a gas turbine engine combustor
UNITED TECHNOLOGIES CORP2 citations72
US10077903B2Sep 18, 2018
Hybrid through holes and angled holes for combustor grommet cooling
UNITED TECHNOLOGIES CORP4 citations72
US9909761B2Mar 6, 2018
Combustor wall assembly for a turbine engine
UNITED TECHNOLOGIES CORP2 citations72
US11378275B2Jul 5, 2022
High shear swirler with recessed fuel filmer for a gas turbine engine
UNITED TECHNOLOGIES CORP4 citations71
US7475546B2Jan 13, 2009
Augmentor pilot nozzle
UNITED TECHNOLOGIES CORP5 citations71
US6971239B2Dec 6, 2005
Augmentor pilot nozzle
UNITED TECHNOLOGIES CORP8 citations71
RAYTHEON TECH CORP
6 patentsUS11649964B2May 16, 2023
Fuel injector assembly for a turbine engine
RAYTHEON TECH CORP5 citations86
US11846421B2Dec 19, 2023
Integrated fuel swirlers
RAYTHEON TECH CORP4 citations75
US11754287B2Sep 12, 2023
Fuel injector assembly for a turbine engine
RAYTHEON TECH CORP3 citations73
US11421883B2Aug 23, 2022
Fuel injector assembly with a helical swirler passage for a turbine engine
RAYTHEON TECH CORP3 citations73
US12038175B2Jul 16, 2024
Extended bulkhead panel
RAYTHEON TECH CORP0 citations63
US11525577B2Dec 13, 2022
Extended bulkhead panel
RAYTHEON TECH CORP0 citations63
SNYDER TIMOTHY S
4 patentsUS8069648B2Dec 6, 2011
Impingement cooling for turbofan exhaust assembly
SNYDER TIMOTHY S50 citations97
US8739546B2Jun 3, 2014
Gas turbine combustor with quench wake control
SNYDER TIMOTHY S20 citations91
US9068751B2Jun 30, 2015
Gas turbine combustor with staged combustion
SNYDER TIMOTHY S16 citations84
US9115897B2Aug 25, 2015
Gas turbine engine systems and methods involving enhanced fuel dispersion
SNYDER TIMOTHY S8 citations80
RTX CORP
4 patentsUS11976820B2May 7, 2024
Multi-fueled, water injected hydrogen fuel injector
RTX CORP3 citations75
US11920525B2Mar 5, 2024
Liquid and hydrogen/methane fuel injector
RTX CORP3 citations75
US12422142B2Sep 23, 2025
Fuel injector assembly for a turbine engine
RTX CORP0 citations63
US12359810B2Jul 15, 2025
Extended bulkhead panel
RTX CORP0 citations63
KIM WON-WOOK
2 patentsCUNHA FRANK J
1 patentEASTWOOD JONATHAN JEFFERY
1 patentCUNHA FRANCISCO J
1 patentERBAS-SEN NURHAK
1 patentMCKENZIE CRISEN
1 patentShowing the top 50 of 77 patents by PatentIndex Score.