Inventor · disambiguated record
Oleg Petrenko
Also filed as: PETRENKO OLEG
9 granted patents·1 pending application·40 citations·filing 2012–2019
85Inventor score
Top patents by PatentIndex Score
10 records- 0195US8375699B1Variable area fan nozzle with wall thickness distributionUNITED TECHNOLOGIES CORP·Filed 2012·Granted Feb 19, 2013·24 cites·21 claims
- 0292US11181074B2Variable area fan nozzle with wall thickness distributionUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 23, 2021·4 cites·13 claims
- 0387US11236701B2Convergent divergent exit nozzle for a gas turbine engineRAYTHEON TECH CORP·Filed 2018·Granted Feb 1, 2022·3 cites·8 claims
- 0482US10371092B2Convergent divergent exit nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·3 cites·13 claims
- 0568US10302042B2Variable area fan nozzle with wall thickness distributionUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 28, 2019·1 cites·12 claims
- 0666US9394852B2Variable area fan nozzle with wall thickness distributionUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 19, 2016·2 cites·21 claims
- 0762US9249731B2Nacelle bifurcation for gas turbine engineSIDELKOVSKIY DMITRIY B·Filed 2012·Granted Feb 2, 2016·3 cites·18 claims
- 0849US10550704B2High performance convergent divergent nozzleUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 4, 2020·0 cites·14 claims
- 0948US9429103B2Variable area fan nozzle with wall thickness distributionATASSI OLIVER V·Filed 2013·Granted Aug 30, 2016·0 cites·5 claims
- 1042US2014216005A1Gas Turbine Engine Assembly Including A Thrust ReverserUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →