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 patentsUS10036258B2Jul 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 patentsRAYTHEON TECH CORP
2 patentsSLAVENS THOMAS N
1 patentRTX CORP
1 patentShowing the top 50 of 90 patents by PatentIndex Score.