Inventor · disambiguated record
David R. Pack
Also filed as: PACK DAVID R
19 granted patents·3 pending applications·240 citations·filing 2001–2025
92Inventor score
Top patents by PatentIndex Score
22 records- 0198US6974308B2High effectiveness cooled turbine vane or bladeHONEYWELL INT INC·Filed 2001·Granted Dec 13, 2005·176 cites·39 claims
- 0297US10378364B2Modified structural truss for airfoilsUNITED TECHNOLOGIES CORP·Filed 2017·Granted Aug 13, 2019·24 cites·20 claims
- 0396US11629602B2Cooling schemes for airfoils for gas turbine enginesRAYTHEON TECH CORP·Filed 2022·Granted Apr 18, 2023·4 cites·20 claims
- 0495US11149550B2Blade neck transitionUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 19, 2021·11 cites·27 claims
- 0595US10871074B2Blade/vane cooling passagesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Dec 22, 2020·12 cites·15 claims
- 0691US11905849B2Cooling schemes for airfoils for gas turbine enginesRTX CORP·Filed 2022·Granted Feb 20, 2024·2 cites·18 claims
- 0791US9719363B2Segmented rim seal spacer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 1, 2017·6 cites·14 claims
- 0888US11286793B2Airfoil with ribs having connector arms and apertures defining a cooling circuitUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 29, 2022·4 cites·21 claims
- 0979US2025092789A1Airfoils with Lobed Cooling CavitiesRTX CORP·Filed 2024·Application pending·0 cites
- 1076US12173618B2Airfoils with lobed cooling cavitiesRTX CORP·Filed 2023·Granted Dec 24, 2024·0 cites·20 claims
- 1176US2024271536A1Airfoil with ribs defining shaped cooling channelRTX CORP·Filed 2024·Application pending·0 cites
- 1275US11480059B2Airfoil with rib having connector armsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 25, 2022·1 cites·8 claims
- 1371US12281595B1Turbine blade with boomerang shaped wall cooling passagesRTX CORP·Filed 2023·Granted Apr 22, 2025·0 cites·18 claims
- 1470US11970954B2Airfoil with rib having connector armsRAYTHEON TECH CORP·Filed 2022·Granted Apr 30, 2024·0 cites·9 claims
- 1570US2025230751A1Turbine blade with boomerang shaped wall cooling passagesRTX CORP·Filed 2025·Application pending·0 cites
- 1666US11209221B2Modified shaped heat exchanger inlets/outletsRAYTHEON TECH CORP·Filed 2020·Granted Dec 28, 2021·0 cites·20 claims
- 1762US12000305B2Airfoil with ribs defining shaped cooling channelUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 4, 2024·0 cites·5 claims
- 1860US11952911B2Airfoil with connecting ribUNITED TECHNOLOGIES CORP·Filed 2019·Granted Apr 9, 2024·0 cites·22 claims
- 1959US10954799B2Gas turbine engine blade with variable density and wide chord tipUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 23, 2021·0 cites·16 claims
- 2057US12404775B1Turbine blade with cooling channelsRTX CORP·Filed 2024·Granted Sep 2, 2025·0 cites·20 claims
- 2151US10316671B2Gas turbine engine blade with variable density and wide chord tipUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 11, 2019·0 cites·11 claims
- 2247US10378453B2Method and assembly for reducing secondary heat in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 13, 2019·0 cites·16 claims
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →