P

Inventor

KOSTKA JR STANISLAV

US22 patents
⚠️ This page may combine multiple inventors who share the name “KOSTKA JR STANISLAV”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

UNITED TECHNOLOGIES CORP

20 patents
US10598379B2Mar 24, 2020

Film cooled multi-walled structure with one or more indentations

UNITED TECHNOLOGIES CORP7 citations84
US10502422B2Dec 10, 2019

Cooling a quench aperture body of a combustor wall

UNITED TECHNOLOGIES CORP7 citations84
US9976743B2May 22, 2018

Dilution hole assembly

UNITED TECHNOLOGIES CORP11 citations84
US10753608B2Aug 25, 2020

Turbine engine multi-walled structure with internal cooling element(s)

UNITED TECHNOLOGIES CORP3 citations73
US10533745B2Jan 14, 2020

Film cooling a combustor wall of a turbine engine

UNITED TECHNOLOGIES CORP2 citations73
US10443848B2Oct 15, 2019

Grommet assembly and method of design

UNITED TECHNOLOGIES CORP6 citations73
US10386066B2Aug 20, 2019

Turbine engine multi-walled structure with cooling element(s)

UNITED TECHNOLOGIES CORP5 citations73
US10386068B2Aug 20, 2019

Cooling a quench aperture body of a combustor wall

UNITED TECHNOLOGIES CORP3 citations73
US10378768B2Aug 13, 2019

Combustor quench aperture cooling

UNITED TECHNOLOGIES CORP2 citations73
US10317079B2Jun 11, 2019

Cooling an aperture body of a combustor wall

UNITED TECHNOLOGIES CORP6 citations73
US10094287B2Oct 9, 2018

Gas turbine engine component with vascular cooling scheme

UNITED TECHNOLOGIES CORP4 citations73
US10794595B2Oct 6, 2020

Stepped heat shield for a turbine engine combustor

UNITED TECHNOLOGIES CORP4 citations72
US10352566B2Jul 16, 2019

Gas turbine engine combustor liner panel

UNITED TECHNOLOGIES CORP6 citations72
US11320146B2May 3, 2022

Film cooling a combustor wall of a turbine engine

UNITED TECHNOLOGIES CORP0 citations62
US11226098B2Jan 18, 2022

Film-cooled multi-walled structure with one or more indentations

UNITED TECHNOLOGIES CORP0 citations62
US10697636B2Jun 30, 2020

Cooling a combustor heat shield proximate a quench aperture

UNITED TECHNOLOGIES CORP1 citations62
US11112115B2Sep 7, 2021

Contoured dilution passages for gas turbine engine combustor

UNITED TECHNOLOGIES CORP0 citations52
US10088161B2Oct 2, 2018

Gas turbine engine wall assembly with circumferential rail stud architecture

UNITED TECHNOLOGIES CORP1 citations51
US10317078B2Jun 11, 2019

Cooling a multi-walled structure of a turbine engine

UNITED TECHNOLOGIES CORP0 citations41
US10480787B2Nov 19, 2019

Combustor wall cooling channel formed by additive manufacturing

UNITED TECHNOLOGIES CORP0 citations36

RAYTHEON TECH CORP

2 patents