P

Inventor

SLAVENS THOMAS N

US90 patents
⚠️ This page may combine multiple inventors who share the name “SLAVENS THOMAS N”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

UNITED TECHNOLOGIES CORP

44 patents
US10036258B2Jul 31, 2018

Gas turbine engine component having vascular engineered lattice structure

UNITED TECHNOLOGIES CORP30 citations94
US9988923B2Jun 5, 2018

Seal for gas turbine engine

UNITED TECHNOLOGIES CORP24 citations93
US9714580B2Jul 25, 2017

Trough seal for gas turbine engine

UNITED TECHNOLOGIES CORP24 citations93
US10662781B2May 26, 2020

Gas turbine engine component having vascular engineered lattice structure

UNITED TECHNOLOGIES CORP9 citations84
US10247419B2Apr 2, 2019

Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustor

UNITED TECHNOLOGIES CORP7 citations84
US9932841B2Apr 3, 2018

Workpiece manufactured from an additive manufacturing system having a particle separator and method of operation

UNITED TECHNOLOGIES CORP8 citations84
US9713843B2Jul 25, 2017

Method for additively constructing internal channels

UNITED TECHNOLOGIES CORP14 citations84
US10385774B2Aug 20, 2019

Split compressor turbine engine

UNITED TECHNOLOGIES CORP6 citations83
US10104313B2Oct 16, 2018

Method for turbine component qualification

UNITED TECHNOLOGIES CORP11 citations82
US10316668B2Jun 11, 2019

Gas turbine engine component having curved turbulator

UNITED TECHNOLOGIES CORP9 citations78
US10683768B2Jun 16, 2020

Circumferential axial segmented trough seal

UNITED TECHNOLOGIES CORP4 citations73
US10612392B2Apr 7, 2020

Gas turbine engine component with conformal fillet cooling path

UNITED TECHNOLOGIES CORP2 citations73
US10487667B2Nov 26, 2019

Airfoil, and method for manufacturing the same

UNITED TECHNOLOGIES CORP2 citations73
US10370981B2Aug 6, 2019

Gas turbine engine component cooling circuit with respirating pedestal

UNITED TECHNOLOGIES CORP3 citations73
US10329918B2Jun 25, 2019

Multiple piece engine component

UNITED TECHNOLOGIES CORP5 citations73
US10301967B2May 28, 2019

Incident tolerant turbine vane gap flow discouragement

UNITED TECHNOLOGIES CORP2 citations73
US10287900B2May 14, 2019

Incident tolerant turbine vane cooling

UNITED TECHNOLOGIES CORP2 citations73
US10247099B2Apr 2, 2019

Pedestals with heat transfer augmenter

UNITED TECHNOLOGIES CORP6 citations73
US10247011B2Apr 2, 2019

Gas turbine engine component with increased cooling capacity

UNITED TECHNOLOGIES CORP2 citations73
US10240464B2Mar 26, 2019

Gas turbine engine airfoil with leading edge trench and impingement cooling

UNITED TECHNOLOGIES CORP4 citations73
US10233842B2Mar 19, 2019

Tangential on-board injectors for gas turbine engines

UNITED TECHNOLOGIES CORP4 citations73
US10156359B2Dec 18, 2018

Gas turbine engine component having vascular engineered lattice structure

UNITED TECHNOLOGIES CORP3 citations73
US10094229B2Oct 9, 2018

Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation

UNITED TECHNOLOGIES CORP2 citations73
US10066549B2Sep 4, 2018

Variable vane segment

UNITED TECHNOLOGIES CORP2 citations73
US10040115B2Aug 7, 2018

Additively manufactured casting articles for manufacturing gas turbine engine parts

UNITED TECHNOLOGIES CORP5 citations73
US10012088B2Jul 3, 2018

Additive manufacturing system utilizing an epitaxy process and method of operation

UNITED TECHNOLOGIES CORP5 citations73
US9932835B2Apr 3, 2018

Airfoil cooling device and method of manufacture

UNITED TECHNOLOGIES CORP3 citations73
US10364683B2Jul 30, 2019

Gas turbine engine component cooling passage turbulator

UNITED TECHNOLOGIES CORP2 citations72
US10273809B2Apr 30, 2019

Centrifugal airfoil cooling modulation

UNITED TECHNOLOGIES CORP4 citations72
US10196902B2Feb 5, 2019

Cooling for gas turbine engine components

UNITED TECHNOLOGIES CORP3 citations72
US10012090B2Jul 3, 2018

Airfoil cooling apparatus

UNITED TECHNOLOGIES CORP2 citations72
US10626730B2Apr 21, 2020

Enhanced cooling for blade tip

UNITED TECHNOLOGIES CORP4 citations71
US10385728B2Aug 20, 2019

Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle

UNITED TECHNOLOGIES CORP2 citations71
US10245637B2Apr 2, 2019

Low modulus shot sleeve for high temperature die casting

UNITED TECHNOLOGIES CORP2 citations70
US11143034B2Oct 12, 2021

Multiple piece engine component

UNITED TECHNOLOGIES CORP0 citations63
US10830096B2Nov 10, 2020

Rotating turbine vane bearing cooling

UNITED TECHNOLOGIES CORP1 citations63
US10329923B2Jun 25, 2019

Gas turbine engine airfoil leading edge cooling

UNITED TECHNOLOGIES CORP1 citations63
US9116051B2Aug 25, 2015

Actively cooled gas turbine sensor probe housing

UNITED TECHNOLOGIES CORP2 citations63
US11059093B2Jul 13, 2021

Additively manufactured core for use in casting an internal cooling circuit of a gas turbine engine component

UNITED TECHNOLOGIES CORP0 citations62
US10960460B2Mar 30, 2021

Additive manufactured mold, a method of manufacturing the mold, and a workpiece casted from the mold

UNITED TECHNOLOGIES CORP1 citations62
US10954800B2Mar 23, 2021

Fluidic machining method and system

UNITED TECHNOLOGIES CORP0 citations62
US10935240B2Mar 2, 2021

Additive manufactured combustor heat shield

UNITED TECHNOLOGIES CORP1 citations62
US10844730B2Nov 24, 2020

Centrifugal airfoil cooling modulation

UNITED TECHNOLOGIES CORP1 citations62
US10465530B2Nov 5, 2019

Gas turbine engine component cooling cavity with vortex promoting features

UNITED TECHNOLOGIES CORP1 citations62

MARTIN THOMAS J

2 patents

RAYTHEON TECH CORP

2 patents

SLAVENS THOMAS N

1 patent

RTX CORP

1 patent

Showing the top 50 of 90 patents by PatentIndex Score.