P

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 patents
US6810673B2Nov 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 patents

SNYDER TIMOTHY S

4 patents

RTX CORP

4 patents

KIM WON-WOOK

2 patents

CUNHA FRANK J

1 patent

EASTWOOD JONATHAN JEFFERY

1 patent

CUNHA FRANCISCO J

1 patent

ERBAS-SEN NURHAK

1 patent

MCKENZIE CRISEN

1 patent

Showing the top 50 of 77 patents by PatentIndex Score.