P

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 patents
US11137140B2Oct 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 patents

RTX CORP

2 patents