Inventor · disambiguated record
Charles Thistle
Also filed as: THISTLE CHARLES
12 granted patents·4 pending applications·24 citations·filing 2014–2019
85Inventor score
Files withUNITED TECHNOLOGIES CORP16
Top patents by PatentIndex Score
16 records- 0192US10677073B2Blade platform with damper restraintUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 9, 2020·9 cites·15 claims
- 0287US10731479B2Blade platform with damper restraintUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 4, 2020·5 cites·14 claims
- 0381US11377967B2Pre-formed faceted turbine blade damper sealUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 5, 2022·3 cites·20 claims
- 0479US10519782B2Airfoil having serpentine core resupply flow controlUNITED TECHNOLOGIES CORP·Filed 2017·Granted Dec 31, 2019·3 cites·19 claims
- 0574US10047611B2Turbine blade attachment curved rib stiffenersUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 14, 2018·2 cites·18 claims
- 0667US10724386B2Blade platform with damper restraintUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 28, 2020·1 cites·16 claims
- 0763US10662784B2Damper with varying thickness for a bladeUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 26, 2020·1 cites·20 claims
- 0857US10822959B2Blade tip coolingUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 3, 2020·0 cites·2 claims
- 0950US10077665B2Turbine blade attachment rails for attachment fillet stress reductionUNITED TECHNOLOGIES CORP·Filed 2016·Granted Sep 18, 2018·0 cites·18 claims
- 1047US10815792B2Gas turbine engine component with a cooling circuit having a flared baseUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 27, 2020·0 cites·11 claims
- 1143US2016298465A1Gas turbine engine component cooling passage with asymmetrical pedestalsUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1242US10612394B2Airfoil having serpentine core resupply flow controlUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 7, 2020·0 cites·12 claims
- 1342US2016208620A1Gas turbine engine airfoil turbulator for airfoil creep resistanceUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1440US10570749B2Gas turbine blade with pedestal arrayUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 25, 2020·0 cites·20 claims
- 1538US2018187558A1Blade platform with chamferUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 1635US2016326909A1Gas turbine engine component with separation rib for cooling passagesUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →