Inventor
ENNACER MOHAMMED
CA19 patents
⚠️ This page may combine multiple inventors who share the name “ENNACER MOHAMMED”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
PRATT & WHITNEY CANADA
11 patentsUS10570773B2Feb 25, 2020
Turbine shroud cooling
PRATT & WHITNEY CANADA2 citations70
US10533454B2Jan 14, 2020
Turbine shroud cooling
PRATT & WHITNEY CANADA6 citations70
US10502093B2Dec 10, 2019
Turbine shroud cooling
PRATT & WHITNEY CANADA3 citations70
US11578600B1Feb 14, 2023
Turbine blade airfoil profile
PRATT & WHITNEY CANADA3 citations67
US12553450B2Feb 17, 2026
Plenum closure panel with integrated airflow direction device
PRATT & WHITNEY CANADA0 citations62
US11274569B2Mar 15, 2022
Turbine shroud cooling
PRATT & WHITNEY CANADA1 citations59
US11118475B2Sep 14, 2021
Turbine shroud cooling
PRATT & WHITNEY CANADA1 citations59
US10941709B2Mar 9, 2021
Gas turbine engine and cooling air configuration for turbine section thereof
PRATT & WHITNEY CANADA1 citations58
US11536141B1Dec 27, 2022
Turbine vane airfoil profile
PRATT & WHITNEY CANADA0 citations57
US11365645B2Jun 21, 2022
Turbine shroud cooling
PRATT & WHITNEY CANADA1 citations55
US11015450B2May 25, 2021
High pressure turbine blade airfoil profile
PRATT & WHITNEY CANADA0 citations47
UNITED TECHNOLOGIES CORP
5 patentsUS10502075B2Dec 10, 2019
Platform cooling circuit for a gas turbine engine component
UNITED TECHNOLOGIES CORP3 citations73
US10107140B2Oct 23, 2018
Turbine airfoil segment having film cooling hole arrangement
UNITED TECHNOLOGIES CORP4 citations71
US11377965B2Jul 5, 2022
Gas turbine engine airfoil cooling circuit arrangement
UNITED TECHNOLOGIES CORP0 citations62
US10443434B2Oct 15, 2019
Turbine airfoil platform segment with film cooling hole arrangement
UNITED TECHNOLOGIES CORP1 citations60
US10301966B2May 28, 2019
Turbine airfoil platform segment with film cooling hole arrangement
UNITED TECHNOLOGIES CORP0 citations50