Inventor
SIDELKOVSKIY DMITRIY B
US19 patents
⚠️ This page may combine multiple inventors who share the name “SIDELKOVSKIY DMITRIY B”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
11 patentsUS10738694B1Aug 11, 2020
Turbofan with motorized rotating inlet guide vane
UNITED TECHNOLOGIES CORP9 citations84
US11085371B2Aug 10, 2021
Turbofan with motorized rotating inlet guide vane
UNITED TECHNOLOGIES CORP2 citations73
US11028779B2Jun 8, 2021
Gas turbine engine bypass drainage systems
UNITED TECHNOLOGIES CORP3 citations73
US11046445B2Jun 29, 2021
Nacelle
UNITED TECHNOLOGIES CORP2 citations72
US11027827B2Jun 8, 2021
Method for separated flow detection
UNITED TECHNOLOGIES CORP4 citations72
US10371092B2Aug 6, 2019
Convergent divergent exit nozzle for a gas turbine engine
UNITED TECHNOLOGIES CORP3 citations72
US11994089B2May 28, 2024
After-fan system for a gas turbine engine
UNITED TECHNOLOGIES CORP2 citations71
US11846196B2Dec 19, 2023
After-fan system with electrical motor for gas turbine engines
UNITED TECHNOLOGIES CORP0 citations60
US10422280B2Sep 24, 2019
Fan flutter suppression system
UNITED TECHNOLOGIES CORP0 citations52
US10767596B2Sep 8, 2020
Nacelle
UNITED TECHNOLOGIES CORP0 citations51
US10450898B2Oct 22, 2019
Track fairing assembly for a turbine engine nacelle
UNITED TECHNOLOGIES CORP0 citations41
RAYTHEON TECH CORP
4 patentsUS11236701B2Feb 1, 2022
Convergent divergent exit nozzle for a gas turbine engine
RAYTHEON TECH CORP3 citations72
US11548652B2Jan 10, 2023
Nacelle
RAYTHEON TECH CORP0 citations62
US11408369B2Aug 9, 2022
Nacelle
RAYTHEON TECH CORP0 citations62
US11585294B2Feb 21, 2023
High bypass ratio engine bypass duct nozzle with controlled nozzle area
RAYTHEON TECH CORP0 citations51