Inventor · disambiguated record
Timothy S. Snyder
Also filed as: SNYDER III TIMOTHY S · SNYDER TIMOTHY · SNYDER TIMOTHY S
76 granted patents·18 pending applications·1,087 citations·filing 1992–2025
99Inventor score
Files withUNITED TECHNOLOGIES CORP54RTX CORP14RAYTHEON TECH CORP13SNYDER TIMOTHY S5CUNHA FRANCISCO J2
Top patents by PatentIndex Score
94 records- 0198US11649964B2Fuel injector assembly for a turbine engineRAYTHEON TECH CORP·Filed 2020·Granted May 16, 2023·5 cites·16 claims
- 0298US9057523B2Microcircuit cooling for gas turbine engine combustorCUNHA FRANK J·Filed 2011·Granted Jun 16, 2015·31 cites·9 claims
- 0398US6810673B2Low emissions combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2003·Granted Nov 2, 2004·177 cites·18 claims
- 0498US6606861B2Low emissions combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2001·Granted Aug 19, 2003·181 cites·5 claims
- 0595US11976820B2Multi-fueled, water injected hydrogen fuel injectorRTX CORP·Filed 2022·Granted May 7, 2024·3 cites·16 claims
- 0695US11846421B2Integrated fuel swirlersRAYTHEON TECH CORP·Filed 2020·Granted Dec 19, 2023·4 cites·20 claims
- 0794US11754287B2Fuel injector assembly for a turbine engineRAYTHEON TECH CORP·Filed 2020·Granted Sep 12, 2023·3 cites·15 claims
- 0894US11421883B2Fuel injector assembly with a helical swirler passage for a turbine engineRAYTHEON TECH CORP·Filed 2020·Granted Aug 23, 2022·3 cites·18 claims
- 0994US8069648B2Impingement cooling for turbofan exhaust assemblySNYDER TIMOTHY S·Filed 2008·Granted Dec 6, 2011·50 cites·22 claims
- 1093US11920525B2Liquid and hydrogen/methane fuel injectorRTX CORP·Filed 2022·Granted Mar 5, 2024·3 cites·17 claims
- 1191US11506390B2Multi-fuel bluff-body piloted high-shear injector and method of using sameUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 22, 2022·5 cites·19 claims
- 1291US9851105B2Self-cooled orifice structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·7 cites·20 claims
- 1391US9068751B2Gas turbine combustor with staged combustionSNYDER TIMOTHY S·Filed 2010·Granted Jun 30, 2015·16 cites·12 claims
- 1490US10794596B2Dual fuel nozzle with liquid filming atomization for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 6, 2020·13 cites·22 claims
- 1588US9377198B2Heat shield for a combustorEASTWOOD JONATHAN JEFFERY·Filed 2012·Granted Jun 28, 2016·10 cites·27 claims
- 1688US7195456B2Turbine engine guide vane and arrays thereofUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 27, 2007·59 cites·16 claims
- 1787US10228137B2Dual fuel nozzle with swirling axial gas injection for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 12, 2019·9 cites·9 claims
- 1886US11378275B2High shear swirler with recessed fuel filmer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 5, 2022·4 cites·13 claims
- 1986US9194585B2Cooling for combustor liners with accelerating channelsUNITED TECHNOLOGIES CORP·Filed 2012·Granted Nov 24, 2015·10 cites·20 claims
- 2086US6176087B1Bluff body premixing fuel injector and method for premixing fuel and airUNITED TECHNOLOGIES CORP·Filed 1997·Granted Jan 23, 2001·52 cites·18 claims
- 2186US5706643AActive gas turbine combustion control to minimize nitrous oxide emissionsUNITED TECHNOLOGIES CORP·Filed 1995·Granted Jan 13, 1998·69 cites·11 claims
- 2285US12422142B2Fuel injector assembly for a turbine engineRTX CORP·Filed 2023·Granted Sep 23, 2025·0 cites·10 claims
- 2385US10317080B2Co-swirl orientation of combustor effusion passages for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 11, 2019·9 cites·7 claims
- 2485US10077903B2Hybrid through holes and angled holes for combustor grommet coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 18, 2018·4 cites·10 claims
- 2585US6513329B1Premixing fuel and airUNITED TECHNOLOGIES CORP·Filed 2000·Granted Feb 4, 2003·32 cites·6 claims
- 2685US5256352AAir-liquid mixerUNITED TECHNOLOGIES CORP·Filed 1992·Granted Oct 26, 1993·51 cites·1 claims
- 2784US12359810B2Extended bulkhead panelRTX CORP·Filed 2024·Granted Jul 15, 2025·0 cites·8 claims
- 2884US11808455B2Gas turbine engine combustor with integral fuel conduit(s)RAYTHEON TECH CORP·Filed 2021·Granted Nov 7, 2023·1 cites·18 claims
- 2984US9052111B2Turbine engine combustor wall with non-uniform distribution of effusion aperturesERBAS-SEN NURHAK·Filed 2012·Granted Jun 9, 2015·11 cites·14 claims
- 3083US11236906B2Combustor cooled quench zone arrayUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 1, 2022·2 cites·16 claims
- 3183US5461865ATangential entry fuel nozzleUNITED TECHNOLOGIES CORP·Filed 1994·Granted Oct 31, 1995·45 cites·11 claims
- 3282US8739546B2Gas turbine combustor with quench wake controlSNYDER TIMOTHY S·Filed 2009·Granted Jun 3, 2014·20 cites·20 claims
- 3382US8484943B2Impingement cooling for turbofan exhaust assemblyCUNHA FRANCISCO J·Filed 2011·Granted Jul 16, 2013·7 cites·15 claims
- 3481US9322554B2Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustorKIM WON-WOOK·Filed 2011·Granted Apr 26, 2016·8 cites·29 claims
- 3579US11920524B2Multi-fuel, fuel injection system for a turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Mar 5, 2024·1 cites·19 claims
- 3679US11725818B2Bluff-body piloted high-shear injector and method of using sameUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 15, 2023·2 cites·17 claims
- 3779US9360215B2Combustor having a beveled grommetMCKENZIE CRISEN·Filed 2012·Granted Jun 7, 2016·9 cites·12 claims
- 3878US10094563B2Microcircuit cooling for gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 9, 2018·2 cites·20 claims
- 3977US9909761B2Combustor wall assembly for a turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 6, 2018·2 cites·12 claims
- 4076US12038175B2Extended bulkhead panelRAYTHEON TECH CORP·Filed 2022·Granted Jul 16, 2024·0 cites·5 claims
- 4176US7475546B2Augmentor pilot nozzleUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jan 13, 2009·5 cites·7 claims
- 4275US11391461B2Combustor bulkhead with circular impingement hole patternUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jul 19, 2022·1 cites·15 claims
- 4374US7798765B2Out-flow margin protection for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2007·Granted Sep 21, 2010·14 cites·26 claims
- 4472US11346557B2Aerodynamic guide plate collar for swirler assemblyUNITED TECHNOLOGIES CORP·Filed 2019·Granted May 31, 2022·1 cites·16 claims
- 4570US2025223930A1Multi-fuel, fuel injection system for a turbine engineRTX CORP·Filed 2024·Application pending·0 cites
- 4669US11525577B2Extended bulkhead panelRAYTHEON TECH CORP·Filed 2020·Granted Dec 13, 2022·0 cites·10 claims
- 4769US7007864B2Fuel nozzle designUNITED TECHNOLOGIES CORP·Filed 2002·Granted Mar 7, 2006·30 cites·11 claims
- 4868US11187413B2Dirt collector systemUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 30, 2021·1 cites·10 claims
- 4968US5479773ATangential air entry fuel nozzleUNITED TECHNOLOGIES CORP·Filed 1994·Granted Jan 2, 1996·29 cites·6 claims
- 5067US10330320B2Circumferentially and axially staged annular combustor for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 25, 2019·2 cites·13 claims
Showing the top 50 of 94 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →