Inventor
GREGG SHAWN J
US27 patents
⚠️ This page may combine multiple inventors who share the name “GREGG SHAWN J”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
19 patentsUS8348613B2Jan 8, 2013
Airflow influencing airfoil feature array
UNITED TECHNOLOGIES CORP29 citations92
US7665968B2Feb 23, 2010
Cooled rotor blade
UNITED TECHNOLOGIES CORP26 citations92
US7186082B2Mar 6, 2007
Cooled rotor blade and method for cooling a rotor blade
UNITED TECHNOLOGIES CORP26 citations92
US6929451B2Aug 16, 2005
Cooled rotor blade with vibration damping device
UNITED TECHNOLOGIES CORP33 citations92
US7125225B2Oct 24, 2006
Cooled rotor blade with vibration damping device
UNITED TECHNOLOGIES CORP52 citations91
US7467924B2Dec 23, 2008
Turbine blade including revised platform
UNITED TECHNOLOGIES CORP25 citations89
US7452186B2Nov 18, 2008
Turbine blade including revised trailing edge cooling
UNITED TECHNOLOGIES CORP19 citations89
US10196917B2Feb 5, 2019
Blade outer air seal with cored passages
UNITED TECHNOLOGIES CORP6 citations83
US9476313B2Oct 25, 2016
Gas turbine engine including a pre-diffuser heat exchanger
UNITED TECHNOLOGIES CORP7 citations83
US7059825B2Jun 13, 2006
Cooled rotor blade
UNITED TECHNOLOGIES CORP16 citations81
US7018176B2Mar 28, 2006
Cooled turbine airfoil
UNITED TECHNOLOGIES CORP15 citations79
US7033140B2Apr 25, 2006
Cooled rotor blade with vibration damping device
UNITED TECHNOLOGIES CORP9 citations74
US10502075B2Dec 10, 2019
Platform cooling circuit for a gas turbine engine component
UNITED TECHNOLOGIES CORP3 citations73
US10239156B2Mar 26, 2019
Multi-density, multi-property turbine component
UNITED TECHNOLOGIES CORP3 citations73
US10024172B2Jul 17, 2018
Gas turbine engine airfoil
UNITED TECHNOLOGIES CORP6 citations72
US8353668B2Jan 15, 2013
Airfoil insert having a tab extending away from the body defining a portion of outlet periphery
UNITED TECHNOLOGIES CORP6 citations72
US9334755B2May 10, 2016
Airfoil with variable trip strip height
UNITED TECHNOLOGIES CORP6 citations71
US11377965B2Jul 5, 2022
Gas turbine engine airfoil cooling circuit arrangement
UNITED TECHNOLOGIES CORP0 citations62
US9080452B2Jul 14, 2015
Gas turbine engine airfoil with vane platform cooling passage
UNITED TECHNOLOGIES CORP1 citations50