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 patentsUS10598379B2Mar 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