P

Inventor

BERGMAN RUSSELL J

US52 patents
⚠️ This page may combine multiple inventors who share the name “BERGMAN RUSSELL J”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

UNITED TECHNOLOGIES CORP

24 patents
US8360716B2Jan 29, 2013

Nozzle segment with reduced weight flange

UNITED TECHNOLOGIES CORP20 citations89
US9920633B2Mar 20, 2018

Compound fillet for a gas turbine airfoil

UNITED TECHNOLOGIES CORP15 citations80
US10502075B2Dec 10, 2019

Platform cooling circuit for a gas turbine engine component

UNITED TECHNOLOGIES CORP3 citations73
US10280780B2May 7, 2019

Sealing systems for gas turbine engine vane platforms

UNITED TECHNOLOGIES CORP2 citations73
US9970308B2May 15, 2018

Feather seal

UNITED TECHNOLOGIES CORP3 citations73
US10648353B2May 12, 2020

Low loss airfoil platform rim seal assembly

UNITED TECHNOLOGIES CORP5 citations72
US10641108B2May 5, 2020

Turbine blade shroud for gas turbine engine with power turbine and method of manufacturing same

UNITED TECHNOLOGIES CORP2 citations72
US10641117B2May 5, 2020

Multiple injector holes for gas turbine engine vane

UNITED TECHNOLOGIES CORP2 citations71
US10584602B2Mar 10, 2020

Multi-airfoil split and rejoin method

UNITED TECHNOLOGIES CORP5 citations71
US10352182B2Jul 16, 2019

Internal cooling of stator vanes

UNITED TECHNOLOGIES CORP2 citations71
US10239142B2Mar 26, 2019

Multi-airfoil split and rejoin method to produce enhanced durability coating

UNITED TECHNOLOGIES CORP5 citations71
US10107140B2Oct 23, 2018

Turbine airfoil segment having film cooling hole arrangement

UNITED TECHNOLOGIES CORP4 citations71
US10030529B2Jul 24, 2018

Combined featherseal slot and lightening pocket

UNITED TECHNOLOGIES CORP4 citations70
US10301951B2May 28, 2019

Turbine vane gusset

UNITED TECHNOLOGIES CORP2 citations67
US11377965B2Jul 5, 2022

Gas turbine engine airfoil cooling circuit arrangement

UNITED TECHNOLOGIES CORP0 citations62
US10502092B2Dec 10, 2019

Internally cooled turbine platform

UNITED TECHNOLOGIES CORP1 citations62
US11053808B2Jul 6, 2021

Multiple injector holes for gas turbine engine vane

UNITED TECHNOLOGIES CORP0 citations61
US10443434B2Oct 15, 2019

Turbine airfoil platform segment with film cooling hole arrangement

UNITED TECHNOLOGIES CORP1 citations60
US11458530B2Oct 4, 2022

Repair of core positioning features in cast components

UNITED TECHNOLOGIES CORP0 citations57
US10844739B2Nov 24, 2020

Platforms with leading edge features

UNITED TECHNOLOGIES CORP0 citations52
US10458291B2Oct 29, 2019

Cover plate for a component of a gas turbine engine

UNITED TECHNOLOGIES CORP0 citations52
US10378371B2Aug 13, 2019

Anti-rotation vane

UNITED TECHNOLOGIES CORP0 citations51
US10301966B2May 28, 2019

Turbine airfoil platform segment with film cooling hole arrangement

UNITED TECHNOLOGIES CORP0 citations50
US10132176B2Nov 20, 2018

Split airfoil cluster and method therefor

UNITED TECHNOLOGIES CORP1 citations50

RAYTHEON TECH CORP

11 patents

BERGMAN RUSSELL J

5 patents

SPANGLER BRANDON W

5 patents

RTX CORP

2 patents

PAPPLE MICHAEL LESLIE CLYDE

1 patent

GREGG SHAWN J

1 patent

CAPRARIO JOSEPH T

1 patent

Showing the top 50 of 52 patents by PatentIndex Score.