Inventor · disambiguated record
Mohammed Ennacer
Also filed as: ENNACER MOHAMMED
18 granted patents·94 citations·filing 2012–2022
92Inventor score
Files withPRATT & WHITNEY CANADA10UNITED TECHNOLOGIES CORP5BERGMAN RUSSELL J1GREGG SHAWN J1PAPPLE MICHAEL LESLIE CLYDE1
Top patents by PatentIndex Score
18 records- 0198US8961108B2Cooling system for a turbine vaneBERGMAN RUSSELL J·Filed 2012·Granted Feb 24, 2015·51 cites·23 claims
- 0288US10533454B2Turbine shroud coolingPRATT & WHITNEY CANADA·Filed 2017·Granted Jan 14, 2020·6 cites·12 claims
- 0388US9222364B2Platform cooling circuit for a gas turbine engine componentPAPPLE MICHAEL LESLIE CLYDE·Filed 2012·Granted Dec 29, 2015·12 cites·8 claims
- 0485US10502075B2Platform cooling circuit for a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 10, 2019·3 cites·17 claims
- 0584US11578600B1Turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2021·Granted Feb 14, 2023·3 cites·17 claims
- 0682US10107140B2Turbine airfoil segment having film cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 23, 2018·4 cites·16 claims
- 0781US10502093B2Turbine shroud coolingPRATT & WHITNEY CANADA·Filed 2017·Granted Dec 10, 2019·3 cites·17 claims
- 0877US10570773B2Turbine shroud coolingPRATT & WHITNEY CANADA·Filed 2017·Granted Feb 25, 2020·2 cites·9 claims
- 0975US11118475B2Turbine shroud coolingPRATT & WHITNEY CANADA·Filed 2020·Granted Sep 14, 2021·1 cites·6 claims
- 1074US9759072B2Gas turbine engine airfoil cooling circuit arrangementGREGG SHAWN J·Filed 2012·Granted Sep 12, 2017·5 cites·16 claims
- 1172US11365645B2Turbine shroud coolingPRATT & WHITNEY CANADA·Filed 2020·Granted Jun 21, 2022·1 cites·19 claims
- 1270US11274569B2Turbine shroud coolingPRATT & WHITNEY CANADA·Filed 2019·Granted Mar 15, 2022·1 cites·12 claims
- 1366US10941709B2Gas turbine engine and cooling air configuration for turbine section thereofPRATT & WHITNEY CANADA·Filed 2018·Granted Mar 9, 2021·1 cites·18 claims
- 1462US10443434B2Turbine airfoil platform segment with film cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 15, 2019·1 cites·8 claims
- 1558US11536141B1Turbine vane airfoil profilePRATT & WHITNEY CANADA·Filed 2022·Granted Dec 27, 2022·0 cites·20 claims
- 1657US11377965B2Gas turbine engine airfoil cooling circuit arrangementUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 5, 2022·0 cites·10 claims
- 1749US11015450B2High pressure turbine blade airfoil profilePRATT & WHITNEY CANADA·Filed 2019·Granted May 25, 2021·0 cites·7 claims
- 1845US10301966B2Turbine airfoil platform segment with film cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 28, 2019·0 cites·8 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →