Inventor
TELLER BRET M
US21 patents
⚠️ This page may combine multiple inventors who share the name “TELLER BRET M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
17 patentsUS11041390B1Jun 22, 2021
Turbine airfoil having film cooling hole arrangement
UNITED TECHNOLOGIES CORP6 citations82
US10502067B2Dec 10, 2019
Dual-fed airfoil tip
UNITED TECHNOLOGIES CORP4 citations72
US10406596B2Sep 10, 2019
Core arrangement for turbine engine component
UNITED TECHNOLOGIES CORP4 citations72
US10337332B2Jul 2, 2019
Airfoil having pedestals in trailing edge cavity
UNITED TECHNOLOGIES CORP6 citations72
US10871083B2Dec 22, 2020
Turbine vane for gas turbine engine
UNITED TECHNOLOGIES CORP2 citations71
US10227875B2Mar 12, 2019
Gas turbine engine component with combined mate face and platform cooling
UNITED TECHNOLOGIES CORP2 citations71
US9797260B2Oct 24, 2017
Engine component with wear surface protection
UNITED TECHNOLOGIES CORP2 citations70
US11148191B2Oct 19, 2021
Core arrangement for turbine engine component
UNITED TECHNOLOGIES CORP0 citations62
US11143037B1Oct 12, 2021
Turbine blade cooling hole arrangement
UNITED TECHNOLOGIES CORP1 citations62
US10844729B2Nov 24, 2020
Turbine vane for gas turbine engine
UNITED TECHNOLOGIES CORP1 citations62
US10408071B2Sep 10, 2019
BOAS thermal protection
UNITED TECHNOLOGIES CORP1 citations62
US10830054B2Nov 10, 2020
Internally cooled airfoil
UNITED TECHNOLOGIES CORP1 citations61
US10641100B2May 5, 2020
Gas turbine engine airfoil cooling passage configuration
UNITED TECHNOLOGIES CORP1 citations61
US10508552B2Dec 17, 2019
Internally cooled airfoil
UNITED TECHNOLOGIES CORP1 citations61
US11168571B2Nov 9, 2021
Airfoil having dead-end tip flag cavity
UNITED TECHNOLOGIES CORP0 citations51
US10815803B2Oct 27, 2020
BOAS thermal protection
UNITED TECHNOLOGIES CORP0 citations51
US10677071B2Jun 9, 2020
Turbine vane for gas turbine engine
UNITED TECHNOLOGIES CORP0 citations51