Inventor
ROMANOV DMITRIY A
US21 patents
⚠️ This page may combine multiple inventors who share the name “ROMANOV DMITRIY A”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
17 patentsUS10107128B2Oct 23, 2018
Cooling channels for gas turbine engine component
UNITED TECHNOLOGIES CORP29 citations94
US10006367B2Jun 26, 2018
Self-opening cooling passages for a gas turbine engine
UNITED TECHNOLOGIES CORP8 citations84
US9926799B2Mar 27, 2018
Gas turbine engine components, blade outer air seal assemblies, and blade outer air seal segments thereof
UNITED TECHNOLOGIES CORP9 citations84
US9784125B2Oct 10, 2017
Blade outer air seals with channels
UNITED TECHNOLOGIES CORP11 citations83
US10077680B2Sep 18, 2018
Blade outer air seal assembly and support
UNITED TECHNOLOGIES CORP7 citations81
US10443425B2Oct 15, 2019
Blade outer air seal fin cooling assembly and method
UNITED TECHNOLOGIES CORP5 citations73
US10221767B2Mar 5, 2019
Actively cooled blade outer air seal
UNITED TECHNOLOGIES CORP2 citations73
US11131199B2Sep 28, 2021
Impingement cooling with impingement cells on impinged surface
UNITED TECHNOLOGIES CORP5 citations72
US10309255B2Jun 4, 2019
Blade outer air seal cooling passage
UNITED TECHNOLOGIES CORP2 citations72
US9856748B2Jan 2, 2018
Probe tip cooling
UNITED TECHNOLOGIES CORP5 citations65
US10920601B2Feb 16, 2021
Blade outer air seal fin cooling assembly and method
UNITED TECHNOLOGIES CORP0 citations62
US10914192B2Feb 9, 2021
Impingement cooling for gas turbine engine component
UNITED TECHNOLOGIES CORP0 citations51
US10584607B2Mar 10, 2020
Ring-shaped compliant support
UNITED TECHNOLOGIES CORP0 citations51
US10196931B2Feb 5, 2019
Tortuous cooling passageway for engine component
UNITED TECHNOLOGIES CORP0 citations51
US10077672B2Sep 18, 2018
Ring-shaped compliant support
UNITED TECHNOLOGIES CORP0 citations51
US10145257B2Dec 4, 2018
Blade outer air seal
UNITED TECHNOLOGIES CORP0 citations42
US10060288B2Aug 28, 2018
Multi-flow cooling passage chamber for gas turbine engine
UNITED TECHNOLOGIES CORP0 citations41