Inventor

GALLAGHER EDWARD J

US66 patents

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

UNITED TECHNOLOGIES CORP

33 patents

US9353628B2May 31, 2016

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP14 citations92

US9163517B2Oct 20, 2015

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP14 citations92

US9140127B2Sep 22, 2015

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP18 citations92

US10590775B2Mar 17, 2020

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP9 citations84

US10465702B2Nov 5, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP7 citations84

US10036257B2Jul 31, 2018

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP14 citations84

US9988908B2Jun 5, 2018

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP5 citations84

US9777580B2Oct 3, 2017

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP4 citations84

US9605542B2Mar 28, 2017

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP13 citations84

US9599064B2Mar 21, 2017

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP12 citations84

US9574574B2Feb 21, 2017

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP6 citations84

US9399917B2Jul 26, 2016

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP6 citations84

US9347323B2May 24, 2016

Gas turbine engine airfoil total chord relative to span

UNITED TECHNOLOGIES CORP13 citations84

US10738627B2Aug 11, 2020

Geared low fan pressure ratio fan exit guide vane stagger angle

UNITED TECHNOLOGIES CORP8 citations83

US10358924B2Jul 23, 2019

Turbofan arrangement with blade channel variations

UNITED TECHNOLOGIES CORP5 citations83

US9909505B2Mar 6, 2018

Efficient, low pressure ratio propulsor for gas turbine engines

UNITED TECHNOLOGIES CORP8 citations83

US9869191B2Jan 16, 2018

Geared low fan pressure ratio fan exit guide vane stagger angle

UNITED TECHNOLOGIES CORP12 citations83

US9470093B2Oct 18, 2016

Turbofan arrangement with blade channel variations

UNITED TECHNOLOGIES CORP5 citations83

US10330111B2Jun 25, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP8 citations80

US10794192B2Oct 6, 2020

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP4 citations73

US10605202B2Mar 31, 2020

Efficient, low pressure ratio propulsor for gas turbine engines

UNITED TECHNOLOGIES CORP1 citations73

US10584715B2Mar 10, 2020

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP2 citations73

US10570916B2Feb 25, 2020

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP1 citations73

US10422226B2Sep 24, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP5 citations73

US10358925B2Jul 23, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP1 citations73

US10352331B2Jul 16, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP3 citations73

US10309414B2Jun 4, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP5 citations73

US10184483B2Jan 22, 2019

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP2 citations73

US9567858B2Feb 14, 2017

Gas turbine engine airfoil

UNITED TECHNOLOGIES CORP2 citations73

US10012150B2Jul 3, 2018

Efficient, low pressure ratio propulsor for gas turbine engines

UNITED TECHNOLOGIES CORP3 citations72

US10060263B2Aug 28, 2018

Incidence-tolerant, high-turning fan exit stator

UNITED TECHNOLOGIES CORP6 citations68

US9926885B2Mar 27, 2018

Efficient, low pressure ratio propulsor for gas turbine engines

UNITED TECHNOLOGIES CORP1 citations63

US11118459B2Sep 14, 2021

Turbofan arrangement with blade channel variations

UNITED TECHNOLOGIES CORP0 citations62

RAYTHEON TECH CORP

12 patents

US11041507B2Jun 22, 2021

Gas turbine engine airfoil

RAYTHEON TECH CORP5 citations84

US11867195B2Jan 9, 2024

Gas turbine engine airfoil

RAYTHEON TECH CORP1 citations73

US11767856B2Sep 26, 2023

Gas turbine engine airfoil

RAYTHEON TECH CORP2 citations73

US11408436B2Aug 9, 2022

Gas turbine engine airfoil

RAYTHEON TECH CORP1 citations73

US11209013B2Dec 28, 2021

Gas turbine engine airfoil

RAYTHEON TECH CORP1 citations73

US11073157B2Jul 27, 2021

Efficient, low pressure ratio propulsor for gas turbine engines

RAYTHEON TECH CORP1 citations72

US11466572B2Oct 11, 2022

Gas turbine engine with blade channel variations

RAYTHEON TECH CORP0 citations62

US11391294B2Jul 19, 2022

Gas turbine engine airfoil

RAYTHEON TECH CORP0 citations62

US11193496B2Dec 7, 2021

Gas turbine engine airfoil

RAYTHEON TECH CORP0 citations62

US11193497B2Dec 7, 2021

Gas turbine engine airfoil

RAYTHEON TECH CORP0 citations62

US10914315B2Feb 9, 2021

Gas turbine engine airfoil

RAYTHEON TECH CORP0 citations62

US10890195B2Jan 12, 2021

Gas turbine engine airfoil

RAYTHEON TECH CORP0 citations62

GALLAGHER EDWARD J

4 patents

US9121368B2Sep 1, 2015

Efficient, low pressure ratio propulsor for gas turbine engines

GALLAGHER EDWARD J10 citations92

US9506422B2Nov 29, 2016

Efficient, low pressure ratio propulsor for gas turbine engines

GALLAGHER EDWARD J4 citations83

US9121412B2Sep 1, 2015

Efficient, low pressure ratio propulsor for gas turbine engines

GALLAGHER EDWARD J14 citations83

US9790797B2Oct 17, 2017

Subsonic swept fan blade

GALLAGHER EDWARD J16 citations81

BALTAS CONSTANTINE

1 patent

US9017037B2Apr 28, 2015

Rotor with flattened exit pressure profile

BALTAS CONSTANTINE12 citations83

Showing the top 50 of 66 patents by PatentIndex Score.