Inventor
WHITFIELD CHRISTOPHER
US22 patents
⚠️ This page may combine multiple inventors who share the name “WHITFIELD CHRISTOPHER”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
17 patentsUS11137140B2Oct 5, 2021
Dilution holes with ridge feature for gas turbine engines
UNITED TECHNOLOGIES CORP6 citations77
US10590779B2Mar 17, 2020
Double wall turbine gas turbine engine blade cooling configuration
UNITED TECHNOLOGIES CORP4 citations73
US10196902B2Feb 5, 2019
Cooling for gas turbine engine components
UNITED TECHNOLOGIES CORP3 citations72
US10427075B2Oct 1, 2019
Debris strainer for gas turbine engine cooling flow
UNITED TECHNOLOGIES CORP5 citations71
US10648363B2May 12, 2020
Turbine vane cooling arrangement
UNITED TECHNOLOGIES CORP2 citations69
US10533425B2Jan 14, 2020
Doublet vane assembly for a gas turbine engine
UNITED TECHNOLOGIES CORP2 citations69
US10408453B2Sep 10, 2019
Dilution holes for gas turbine engines
UNITED TECHNOLOGIES CORP5 citations69
US10626735B2Apr 21, 2020
Double wall turbine gas turbine engine blade cooling configuration
UNITED TECHNOLOGIES CORP1 citations62
US11015464B2May 25, 2021
Conformal seal and vane bow wave cooling
UNITED TECHNOLOGIES CORP0 citations61
US10982552B2Apr 20, 2021
Gas turbine engine component with film cooling hole
UNITED TECHNOLOGIES CORP0 citations61
US9957810B2May 1, 2018
Film hole with protruding flow accumulator
UNITED TECHNOLOGIES CORP1 citations51
US10584601B2Mar 10, 2020
Conformal seal and vane bow wave cooling
UNITED TECHNOLOGIES CORP0 citations50
US10641102B2May 5, 2020
Turbine vane cluster including enhanced vane cooling
UNITED TECHNOLOGIES CORP0 citations47
US10648345B2May 12, 2020
Double wall turbine gas turbine engine blade cooling configuration
UNITED TECHNOLOGIES CORP0 citations41
US10508555B2Dec 17, 2019
Double wall turbine gas turbine engine blade cooling configuration
UNITED TECHNOLOGIES CORP0 citations41
US10378363B2Aug 13, 2019
Resupply hole of cooling air into gas turbine blade serpentine passage
UNITED TECHNOLOGIES CORP0 citations41
US10738701B2Aug 11, 2020
Conformal seal bow wave cooling
UNITED TECHNOLOGIES CORP0 citations40
RAYTHEON TECH CORP
3 patentsUS10808548B2Oct 20, 2020
Double wall turbine gas turbine engine blade cooling configuration
RAYTHEON TECH CORP1 citations62
US11041391B2Jun 22, 2021
Conformal seal and vane bow wave cooling
RAYTHEON TECH CORP1 citations60
US10781697B2Sep 22, 2020
Double wall turbine gas turbine engine blade cooling configuration
RAYTHEON TECH CORP0 citations41