Inventor
JENNINGS TIMOTHY J
US43 patents
⚠️ This page may combine multiple inventors who share the name “JENNINGS TIMOTHY J”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
36 patentsUS10077664B2Sep 18, 2018
Gas turbine engine component having engineered vascular structure
UNITED TECHNOLOGIES CORP14 citations84
US10801334B2Oct 13, 2020
Cooling arrangement with purge partition
UNITED TECHNOLOGIES CORP2 citations73
US10753210B2Aug 25, 2020
Airfoil having improved cooling scheme
UNITED TECHNOLOGIES CORP2 citations72
US10196902B2Feb 5, 2019
Cooling for gas turbine engine components
UNITED TECHNOLOGIES CORP3 citations72
US11199096B1Dec 14, 2021
Turbomachine blade
UNITED TECHNOLOGIES CORP3 citations71
US10427075B2Oct 1, 2019
Debris strainer for gas turbine engine cooling flow
UNITED TECHNOLOGIES CORP5 citations71
US11143037B1Oct 12, 2021
Turbine blade cooling hole arrangement
UNITED TECHNOLOGIES CORP1 citations62
US11015454B2May 25, 2021
Coriolis optimized U-channel with root flag
UNITED TECHNOLOGIES CORP0 citations62
US10968753B1Apr 6, 2021
Airfoil having impingement leading edge
UNITED TECHNOLOGIES CORP0 citations62
US10961854B2Mar 30, 2021
Dirt funnel squealer purges
UNITED TECHNOLOGIES CORP1 citations62
US10954800B2Mar 23, 2021
Fluidic machining method and system
UNITED TECHNOLOGIES CORP0 citations62
US10890074B2Jan 12, 2021
Coriolis optimized u-channel with platform core
UNITED TECHNOLOGIES CORP0 citations62
US10801333B2Oct 13, 2020
Airfoils, cores, and methods of manufacture for forming airfoils having fluidly connected platform cooling circuits
UNITED TECHNOLOGIES CORP1 citations62
US10626734B2Apr 21, 2020
Airfoil having internal hybrid cooling cavities
UNITED TECHNOLOGIES CORP1 citations62
US10526898B2Jan 7, 2020
Airfoil cooling circuit
UNITED TECHNOLOGIES CORP1 citations62
US11319839B2May 3, 2022
Component having a dirt tolerant passage turn
UNITED TECHNOLOGIES CORP0 citations61
US11041395B2Jun 22, 2021
Airfoils and core assemblies for gas turbine engines and methods of manufacture
UNITED TECHNOLOGIES CORP0 citations61
US11015457B2May 25, 2021
Multi-walled airfoil core
UNITED TECHNOLOGIES CORP1 citations61
US10982552B2Apr 20, 2021
Gas turbine engine component with film cooling hole
UNITED TECHNOLOGIES CORP0 citations61
US11480057B2Oct 25, 2022
Airfoil cooling circuit
UNITED TECHNOLOGIES CORP0 citations52
US10731475B2Aug 4, 2020
Blade with inlet orifice on aft face of root
UNITED TECHNOLOGIES CORP0 citations52
US10584593B2Mar 10, 2020
Airfoil having impingement leading edge
UNITED TECHNOLOGIES CORP0 citations52
US11168571B2Nov 9, 2021
Airfoil having dead-end tip flag cavity
UNITED TECHNOLOGIES CORP0 citations51
US10941663B2Mar 9, 2021
Airfoil having improved leading edge cooling scheme and damage resistance
UNITED TECHNOLOGIES CORP0 citations51
US10907479B2Feb 2, 2021
Airfoil having improved leading edge cooling scheme and damage resistance
UNITED TECHNOLOGIES CORP0 citations51
US10107110B2Oct 23, 2018
Fluidic machining method and system
UNITED TECHNOLOGIES CORP0 citations51
US9957810B2May 1, 2018
Film hole with protruding flow accumulator
UNITED TECHNOLOGIES CORP1 citations51
US11274559B2Mar 15, 2022
Turbine blade tip dirt removal feature
UNITED TECHNOLOGIES CORP0 citations50
US11053803B2Jul 6, 2021
Airfoils and core assemblies for gas turbine engines and methods of manufacture
UNITED TECHNOLOGIES CORP0 citations50
US10415394B2Sep 17, 2019
Gas turbine engine blade with ceramic tip and cooling arrangement
UNITED TECHNOLOGIES CORP0 citations50
US10006371B2Jun 26, 2018
Film hole with in-wall accumulator
UNITED TECHNOLOGIES CORP1 citations50
US10760432B2Sep 1, 2020
Airfoil having fluidly connected hybrid cavities
UNITED TECHNOLOGIES CORP0 citations42
US10704398B2Jul 7, 2020
Airfoil having internal hybrid cooling cavities
UNITED TECHNOLOGIES CORP0 citations42
US10633980B2Apr 28, 2020
Airfoil having internal hybrid cooling cavities
UNITED TECHNOLOGIES CORP0 citations42
US10626733B2Apr 21, 2020
Airfoil having internal hybrid cooling cavities
UNITED TECHNOLOGIES CORP0 citations42
US9957814B2May 1, 2018
Gas turbine engine component with film cooling hole with accumulator
UNITED TECHNOLOGIES CORP0 citations40
RAYTHEON TECH CORP
4 patentsUS11649731B2May 16, 2023
Airfoil having internal hybrid cooling cavities
RAYTHEON TECH CORP0 citations62
US12006836B2Jun 11, 2024
Cooling arrangement for gas turbine engine component
RAYTHEON TECH CORP0 citations61
US11434768B2Sep 6, 2022
Multi-walled airfoil core
RAYTHEON TECH CORP1 citations61
US11815022B2Nov 14, 2023
Platform serpentine re-supply
RAYTHEON TECH CORP0 citations51