Inventor · disambiguated record
Dmitriy B. Sidelkovskiy
Also filed as: SIDELKOVSKIY DMITRIY · SIDELKOVSKIY DMITRIY B
21 granted patents·4 pending applications·46 citations·filing 2009–2024
92Inventor score
Files withUNITED TECHNOLOGIES CORP12RAYTHEON TECH CORP5RTX CORP4ROLLS ROYCE CORP2SIDELKOVSKIY DMITRIY B2
Top patents by PatentIndex Score
25 records- 0196US10738694B1Turbofan with motorized rotating inlet guide vaneUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 11, 2020·9 cites·19 claims
- 0289US10738710B2Multi-shaft gas turbine engineROLLS ROYCE CORP·Filed 2017·Granted Aug 11, 2020·5 cites·2 claims
- 0388US12312966B1Gas turbine engine with hybrid fan exit guide vanesRTX CORP·Filed 2024·Granted May 27, 2025·1 cites·20 claims
- 0488US9611788B2Multi-shaft gas turbine engineROLLS ROYCE CORP·Filed 2013·Granted Apr 4, 2017·9 cites·7 claims
- 0587US11236701B2Convergent divergent exit nozzle for a gas turbine engineRAYTHEON TECH CORP·Filed 2018·Granted Feb 1, 2022·3 cites·8 claims
- 0687US11027827B2Method for separated flow detectionUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 8, 2021·4 cites·20 claims
- 0786US11994089B2After-fan system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2020·Granted May 28, 2024·2 cites·20 claims
- 0884US11085371B2Turbofan with motorized rotating inlet guide vaneUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 10, 2021·2 cites·19 claims
- 0982US11028779B2Gas turbine engine bypass drainage systemsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 8, 2021·3 cites·20 claims
- 1082US10371092B2Convergent divergent exit nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·3 cites·13 claims
- 1173US12123309B2After-fan system with electrical motor for gas turbine enginesRTX CORP·Filed 2023·Granted Oct 22, 2024·0 cites·4 claims
- 1273US11046445B2NacelleUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 29, 2021·2 cites·18 claims
- 1366US11408369B2NacelleRAYTHEON TECH CORP·Filed 2020·Granted Aug 9, 2022·0 cites·4 claims
- 1465US12510438B2Method of inlet distortion prediction and monitoringRAYTHEON TECH CORP·Filed 2023·Granted Dec 30, 2025·0 cites·20 claims
- 1565US11548652B2NacelleRAYTHEON TECH CORP·Filed 2021·Granted Jan 10, 2023·0 cites·4 claims
- 1662US9249731B2Nacelle bifurcation for gas turbine engineSIDELKOVSKIY DMITRIY B·Filed 2012·Granted Feb 2, 2016·3 cites·18 claims
- 1761US11846196B2After-fan system with electrical motor for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2020·Granted Dec 19, 2023·0 cites·15 claims
- 1856US10422280B2Fan flutter suppression systemUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 24, 2019·0 cites·15 claims
- 1955US2025376990A1Gas turbine engine with split variable fan exit guide vanes and airflow radial total pressure profile re-distributionRTX CORP·Filed 2024·Application pending·0 cites
- 2052US2025376931A1Gas turbine engine with variable fan exit guide vanesRTX CORP·Filed 2024·Application pending·0 cites
- 2151US10767596B2NacelleUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 8, 2020·0 cites·19 claims
- 2250US11585294B2High bypass ratio engine bypass duct nozzle with controlled nozzle areaRAYTHEON TECH CORP·Filed 2020·Granted Feb 21, 2023·0 cites·16 claims
- 2347US10450898B2Track fairing assembly for a turbine engine nacelleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 22, 2019·0 cites·16 claims
- 2442US2014216005A1Gas Turbine Engine Assembly Including A Thrust ReverserUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 2533US2010193643A1Lift fan systemSIDELKOVSKIY DMITRIY B·Filed 2009·Application pending·0 cites
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