Inventor · disambiguated record
Shelton O. Duelm
Also filed as: DUELM SHELTON O
19 granted patents·9 pending applications·103 citations·filing 2010–2021
93Inventor score
Top patents by PatentIndex Score
28 records- 0196US10174627B2Gas turbine engine thin wall composite vane airfoilUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 8, 2019·28 cites·17 claims
- 0290US9017033B2Fan blade platformBROWN CHARLES W·Filed 2012·Granted Apr 28, 2015·15 cites·20 claims
- 0387US10392951B2Vane assembly with trapped segmented vane structuresUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 27, 2019·4 cites·15 claims
- 0485US9957821B2Gas turbine engine composite airfoil trailing edgeUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 1, 2018·8 cites·19 claims
- 0584US8961125B2Gas turbine engine part retentionCHUONG CONWAY·Filed 2011·Granted Feb 24, 2015·14 cites·19 claims
- 0679US9759226B2Low profile fan platform attachmentUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 12, 2017·5 cites·12 claims
- 0777US8596969B2Axial retention feature for gas turbine engine vanesCHUONG CONWAY·Filed 2010·Granted Dec 3, 2013·6 cites·18 claims
- 0876US9551238B2Pin connector for ceramic matrix composite turbine frameUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jan 24, 2017·5 cites·23 claims
- 0971US9133723B2Shield system for gas turbine engineVO TUAN DAVID·Filed 2012·Granted Sep 15, 2015·6 cites·31 claims
- 1070US10578120B2Low profile fan platform attachmentUNITED TECHNOLOGIES CORP·Filed 2017·Granted Mar 3, 2020·1 cites·11 claims
- 1169US10119423B2Gas turbine engine fan spacer platform attachmentsUNITED TECHNOLOGIES CORP·Filed 2013·Granted Nov 6, 2018·3 cites·11 claims
- 1267US9328626B2Annular turbomachine seal and heat shieldDUELM SHELTON O·Filed 2012·Granted May 3, 2016·5 cites·19 claims
- 1363US2021293151A1Cmc airfoil with sharp trailing edge and method of making sameRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 1461US2019360348A1Vane assembly with trapped segmented vane structuresUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 1559US10487675B2Stress mitigation feature for composite airfoil leading edgeUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 26, 2019·1 cites·12 claims
- 1657US10774687B2Gas turbine engine attachment structure and method thereforUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 15, 2020·0 cites·15 claims
- 1756US9022728B2Feather seal slotZIMMERMANN ALISHA M·Filed 2011·Granted May 5, 2015·2 cites·7 claims
- 1854US2016230569A1Cmc airfoil with sharp trailing edge and method of making sameUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 1951US10151218B2Gas turbine engine attachment structure and method thereforUNITED TECHNOLOGIES CORP·Filed 2014·Granted Dec 11, 2018·0 cites·9 claims
- 2046US10167779B2Mid-turbine frame heat shieldUNITED TECHNOLOGIES CORP·Filed 2012·Granted Jan 1, 2019·0 cites·20 claims
- 2145US2016069199A1Stator vane platform with flangesUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2244US2014255174A1Manufacture of full ring strut vane packUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 2343US9163582B2Convergent-divergent gas turbine nozzle comprising movable flaps having a variable thickness in a lateral directionTREAT CHRISTOPHER·Filed 2012·Granted Oct 20, 2015·0 cites·19 claims
- 2442US2014248146A1Attachment apparatus for ceramic matrix composite materialsUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 2540US2017306780A1Floating, non-contact seal with rounded edgeUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 2639US2014314547A1Attachment apparatus for ceramic matrix composite materialsSANDER DAVID J·Filed 2012·Application pending·0 cites
- 2736US9851008B2Seal land for static structure of a gas turbine enginePORTER STEVEN D·Filed 2012·Granted Dec 26, 2017·0 cites·23 claims
- 2836US2014010662A1Composite airfoil with integral platformDUELM SHELTON O·Filed 2012·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Shelton O. Duelm 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 →