Inventor
TRINDADE RICARDO
US29 patents
⚠️ This page may combine multiple inventors who share the name “TRINDADE RICARDO”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
14 patentsUS7901180B2Mar 8, 2011
Enhanced turbine airfoil cooling
UNITED TECHNOLOGIES CORP18 citations78
US10704396B2Jul 7, 2020
Dual-wall impingement cavity for components of gas turbine engines
UNITED TECHNOLOGIES CORP2 citations73
US10227927B2Mar 12, 2019
Supply duct for cooling air from gas turbine compressor
UNITED TECHNOLOGIES CORP2 citations73
US10690346B2Jun 23, 2020
Washer for combustor assembly
UNITED TECHNOLOGIES CORP3 citations71
US10670273B2Jun 2, 2020
Cooling configurations for combustor attachment features
UNITED TECHNOLOGIES CORP5 citations71
US11078796B2Aug 3, 2021
Redundant entry cooling air feed hole blockage preventer for a gas turbine engine
UNITED TECHNOLOGIES CORP3 citations70
US10954815B2Mar 23, 2021
Divided baffle for components of gas turbine engines
UNITED TECHNOLOGIES CORP0 citations62
US10697307B2Jun 30, 2020
Hybrid cooling schemes for airfoils of gas turbine engines
UNITED TECHNOLOGIES CORP1 citations62
US10670274B2Jun 2, 2020
Cooling configurations for combustor attachment features
UNITED TECHNOLOGIES CORP1 citations61
US11073024B2Jul 27, 2021
Shape recessed surface cooling air feed hole blockage preventer for a gas turbine engine
UNITED TECHNOLOGIES CORP1 citations59
US11008872B2May 18, 2021
Extension air feed hole blockage preventer for a gas turbine engine
UNITED TECHNOLOGIES CORP1 citations59
US11939883B2Mar 26, 2024
Airfoil with arced pedestal row
UNITED TECHNOLOGIES CORP0 citations52
US11434770B2Sep 6, 2022
Tip cooling design
UNITED TECHNOLOGIES CORP0 citations52
US10480347B2Nov 19, 2019
Divided baffle for components of gas turbine engines
UNITED TECHNOLOGIES CORP0 citations52
PRATT & WHITNEY CANADA
7 patentsUS6406260B1Jun 18, 2002
Heat transfer promotion structure for internally convectively cooled airfoils
PRATT & WHITNEY CANADA69 citations96
US7611326B2Nov 3, 2009
HP turbine vane airfoil profile
PRATT & WHITNEY CANADA43 citations92
US7004720B2Feb 28, 2006
Cooled turbine vane platform
PRATT & WHITNEY CANADA47 citations92
US7258528B2Aug 21, 2007
Internally cooled airfoil for a gas turbine engine and method
PRATT & WHITNEY CANADA28 citations91
US7097418B2Aug 29, 2006
Double impingement vane platform cooling
PRATT & WHITNEY CANADA39 citations88
US7246989B2Jul 24, 2007
Shroud leading edge cooling
PRATT & WHITNEY CANADA17 citations82
US7278826B2Oct 9, 2007
Airfoil cooling passage trailing edge flow restriction
PRATT & WHITNEY CANADA14 citations79