P

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 patents
US10107128B2Oct 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

ROMANOV DMITRIY A

1 patent

THIBODEAU ANNE-MARIE B

1 patent

RAYTHEON TECH CORP

1 patent

RTX CORP

1 patent