Inventor · disambiguated record
John T. Ols
Also filed as: OLS JOHN T
22 granted patents·3 pending applications·181 citations·filing 2003–2023
93Inventor score
Top patents by PatentIndex Score
25 records- 0193US7954325B2Gas turbine combustorUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jun 7, 2011·43 cites·13 claims
- 0290US7093441B2Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volumeUNITED TECHNOLOGIES CORP·Filed 2003·Granted Aug 22, 2006·79 cites·20 claims
- 0387US9920641B2Gas turbine engine mid-turbine frame configurationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 20, 2018·5 cites·20 claims
- 0486US11959422B2Combustor to vane sealing assembly and method of forming sameRAYTHEON TECH CORP·Filed 2023·Granted Apr 16, 2024·1 cites·20 claims
- 0585US9982548B2Turbine vanes with variable filletsUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 29, 2018·10 cites·22 claims
- 0682US9850771B2Gas turbine engine sealing arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·3 cites·14 claims
- 0782US7665307B2Dual wall combustor linerUNITED TECHNOLOGIES CORP·Filed 2005·Granted Feb 23, 2010·19 cites·15 claims
- 0881US10328526B2Laser powder deposition weld rework for gas turbine engine non-fusion weldable nickel castingsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 25, 2019·7 cites·17 claims
- 0973US11021980B2Gas turbine engine turbine vane ring arrangementRAYTHEON TECH CORP·Filed 2019·Granted Jun 1, 2021·1 cites·20 claims
- 1067US11619174B2Combustor to vane sealing assembly and method of forming sameRAYTHEON TECH CORP·Filed 2021·Granted Apr 4, 2023·0 cites·13 claims
- 1163US8800290B2CombustorBURD STEVEN W·Filed 2007·Granted Aug 12, 2014·7 cites·23 claims
- 1260US10344603B2Gas turbine engine turbine vane ring arrangementUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 9, 2019·1 cites·12 claims
- 1357US10641114B2Turbine vane with non-uniform wall thicknessUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 5, 2020·1 cites·8 claims
- 1457US9568197B2Integrated fuel nozzle with feedback control for a gas turbine engineOLS JOHN T·Filed 2007·Granted Feb 14, 2017·4 cites·2 claims
- 1557US2018080335A1Gas turbine engine sealing arrangementUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 1651US10619496B2Turbine vane with variable trailing edge inner radiusUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 14, 2020·0 cites·23 claims
- 1751US10107118B2Flow discourager for vane sealing area of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 23, 2018·0 cites·20 claims
- 1849US10808936B2Interrupted midrail for combustor panelUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 20, 2020·0 cites·20 claims
- 1949US9945236B2Gas turbine hubUNITED TECHNOLOGIES CORP·Filed 2014·Granted Apr 17, 2018·0 cites·17 claims
- 2048US11111801B2Turbine vane with platform padUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 7, 2021·0 cites·4 claims
- 2146US2016194969A1Turbine Vane With Platform RibUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 2239US11698005B2Flow diverter for mid-turbine frame cooling air deliveryRAYTHEON TECH CORP·Filed 2021·Granted Jul 11, 2023·0 cites·17 claims
- 2339US11021976B2Hardware geometry for increasing part overlap and maintaining clearanceUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 1, 2021·0 cites·13 claims
- 2438US10408088B2Mid-turbine frame stator with repairable bushing and retention pinUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 10, 2019·0 cites·18 claims
- 2538US2021222878A1Combustor to vane sealing assembly and method of forming sameUNITED TECHNOLOGIES CORP·Filed 2020·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →