Inventor
OLS JOHN T
US22 patents
⚠️ This page may combine multiple inventors who share the name “OLS JOHN T”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
16 patentsUS7093441B2Aug 22, 2006
Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
UNITED TECHNOLOGIES CORP79 citations95
US7954325B2Jun 7, 2011
Gas turbine combustor
UNITED TECHNOLOGIES CORP43 citations92
US7665307B2Feb 23, 2010
Dual wall combustor liner
UNITED TECHNOLOGIES CORP19 citations92
US9982548B2May 29, 2018
Turbine vanes with variable fillets
UNITED TECHNOLOGIES CORP10 citations82
US10328526B2Jun 25, 2019
Laser powder deposition weld rework for gas turbine engine non-fusion weldable nickel castings
UNITED TECHNOLOGIES CORP7 citations81
US9920641B2Mar 20, 2018
Gas turbine engine mid-turbine frame configuration
UNITED TECHNOLOGIES CORP5 citations73
US9850771B2Dec 26, 2017
Gas turbine engine sealing arrangement
UNITED TECHNOLOGIES CORP3 citations73
US10344603B2Jul 9, 2019
Gas turbine engine turbine vane ring arrangement
UNITED TECHNOLOGIES CORP1 citations62
US10641114B2May 5, 2020
Turbine vane with non-uniform wall thickness
UNITED TECHNOLOGIES CORP1 citations61
US11111801B2Sep 7, 2021
Turbine vane with platform pad
UNITED TECHNOLOGIES CORP0 citations60
US10619496B2Apr 14, 2020
Turbine vane with variable trailing edge inner radius
UNITED TECHNOLOGIES CORP0 citations52
US10408088B2Sep 10, 2019
Mid-turbine frame stator with repairable bushing and retention pin
UNITED TECHNOLOGIES CORP0 citations52
US11021976B2Jun 1, 2021
Hardware geometry for increasing part overlap and maintaining clearance
UNITED TECHNOLOGIES CORP0 citations51
US10107118B2Oct 23, 2018
Flow discourager for vane sealing area of a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations51
US9945236B2Apr 17, 2018
Gas turbine hub
UNITED TECHNOLOGIES CORP0 citations50
US10808936B2Oct 20, 2020
Interrupted midrail for combustor panel
UNITED TECHNOLOGIES CORP0 citations41
RAYTHEON TECH CORP
4 patentsUS11021980B2Jun 1, 2021
Gas turbine engine turbine vane ring arrangement
RAYTHEON TECH CORP1 citations62
US11959422B2Apr 16, 2024
Combustor to vane sealing assembly and method of forming same
RAYTHEON TECH CORP1 citations60
US11619174B2Apr 4, 2023
Combustor to vane sealing assembly and method of forming same
RAYTHEON TECH CORP0 citations60
US11698005B2Jul 11, 2023
Flow diverter for mid-turbine frame cooling air delivery
RAYTHEON TECH CORP0 citations44