Inventor · disambiguated record
Jeffrey J. Degray
Also filed as: DEGRAY JEFFREY · DEGRAY JEFFREY J
16 granted patents·2 pending applications·59 citations·filing 2012–2024
91Inventor score
Top patents by PatentIndex Score
18 records- 0191US10072517B2Gas turbine engine component having variable width feather seal slotUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 11, 2018·22 cites·20 claims
- 0289US11459898B2Airfoil cooling holesRAYTHEON TECH CORP·Filed 2021·Granted Oct 4, 2022·3 cites·20 claims
- 0389US10024172B2Gas turbine engine airfoilUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 17, 2018·6 cites·18 claims
- 0488US10557360B2Vane intersegment gap sealing arrangementUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 11, 2020·5 cites·17 claims
- 0585US11434768B2Multi-walled airfoil coreRAYTHEON TECH CORP·Filed 2021·Granted Sep 6, 2022·1 cites·20 claims
- 0684US10329937B2Flowpath component for a gas turbine engine including a chordal sealUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 25, 2019·4 cites·15 claims
- 0784US9752446B2Support buttressUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 5, 2017·4 cites·18 claims
- 0878US12371997B2Cooling arrangement for gas turbine engine componentRTX CORP·Filed 2024·Granted Jul 29, 2025·0 cites·19 claims
- 0978US10273820B2Turbine vane cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 30, 2019·2 cites·10 claims
- 1078US9334755B2Airfoil with variable trip strip heightUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 10, 2016·6 cites·13 claims
- 1175US10196913B1Featherseal having tapered radial portionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·2 cites·9 claims
- 1272US11015457B2Multi-walled airfoil coreUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·1 cites·12 claims
- 1368US12006836B2Cooling arrangement for gas turbine engine componentRAYTHEON TECH CORP·Filed 2022·Granted Jun 11, 2024·0 cites·16 claims
- 1456US9080452B2Gas turbine engine airfoil with vane platform cooling passageUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jul 14, 2015·1 cites·14 claims
- 1554US10107107B2Gas turbine engine component with discharge slot having oval geometryBOEKE MARK A·Filed 2012·Granted Oct 23, 2018·2 cites·22 claims
- 1654US2025278534A1Characterization of object attributes for component part requirementsRTX CORP·Filed 2024·Application pending·0 cites
- 1746US10443401B2Cooled turbine vane with alternately orientated film cooling hole rowsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 15, 2019·0 cites·20 claims
- 1836US2016326894A1Airfoil cooling passageUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Jeffrey J. Degray files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →