Inventor · disambiguated record
Bret M. Teller
Also filed as: TELLER BRET · TELLER BRET M
24 granted patents·214 citations·filing 2004–2020
94Inventor score
Files withUNITED TECHNOLOGIES CORP20BEATTIE JEFFREY S1RAYTHEON TECH CORP1TELLER BRET M1ZELESKY MARK F1
Top patents by PatentIndex Score
24 records- 0194US10406596B2Core arrangement for turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 10, 2019·4 cites·11 claims
- 0292US7131818B2Airfoil with three-pass serpentine cooling channel and microcircuitUNITED TECHNOLOGIES CORP·Filed 2004·Granted Nov 7, 2006·66 cites·32 claims
- 0390US11041390B1Turbine airfoil having film cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 22, 2021·6 cites·10 claims
- 0490US10337332B2Airfoil having pedestals in trailing edge cavityUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 2, 2019·6 cites·19 claims
- 0590US7478994B2Airfoil with supplemental cooling channel adjacent leading edgeUNITED TECHNOLOGIES CORP·Filed 2004·Granted Jan 20, 2009·74 cites·31 claims
- 0684US10502067B2Dual-fed airfoil tipUNITED TECHNOLOGIES CORP·Filed 2016·Granted Dec 10, 2019·4 cites·15 claims
- 0781US7097424B2Micro-circuit platformUNITED TECHNOLOGIES CORP·Filed 2004·Granted Aug 29, 2006·38 cites·25 claims
- 0876US11148191B2Core arrangement for turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 19, 2021·0 cites·20 claims
- 0975US10871083B2Turbine vane for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Dec 22, 2020·2 cites·18 claims
- 1075US9797260B2Engine component with wear surface protectionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 24, 2017·2 cites·16 claims
- 1174US11143037B1Turbine blade cooling hole arrangementUNITED TECHNOLOGIES CORP·Filed 2020·Granted Oct 12, 2021·1 cites·20 claims
- 1273US10830054B2Internally cooled airfoilUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 10, 2020·1 cites·10 claims
- 1370US10844729B2Turbine vane for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 24, 2020·1 cites·18 claims
- 1465US10508552B2Internally cooled airfoilUNITED TECHNOLOGIES CORP·Filed 2016·Granted Dec 17, 2019·1 cites·8 claims
- 1562US10815803B2BOAS thermal protectionUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 27, 2020·0 cites·20 claims
- 1662US10641100B2Gas turbine engine airfoil cooling passage configurationUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 5, 2020·1 cites·18 claims
- 1762US9243500B2Turbine blade platform with U-channel cooling holesZELESKY MARK F·Filed 2012·Granted Jan 26, 2016·2 cites·15 claims
- 1860US10227875B2Gas turbine engine component with combined mate face and platform coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 12, 2019·2 cites·14 claims
- 1960US10180067B2Mate face cooling holes for gas turbine engine componentBEATTIE JEFFREY S·Filed 2012·Granted Jan 15, 2019·2 cites·19 claims
- 2058US10408071B2BOAS thermal protectionUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 10, 2019·1 cites·20 claims
- 2152US10677071B2Turbine vane for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 9, 2020·0 cites·20 claims
- 2251US11661852B2Turbine blade trailing edge cooling feedRAYTHEON TECH CORP·Filed 2020·Granted May 30, 2023·0 cites·21 claims
- 2343US11168571B2Airfoil having dead-end tip flag cavityUNITED TECHNOLOGIES CORP·Filed 2020·Granted Nov 9, 2021·0 cites·14 claims
- 2442US10364680B2Gas turbine engine component having platform trenchTELLER BRET M·Filed 2012·Granted Jul 30, 2019·0 cites·19 claims
Join the waitlist — get patent alerts
Get an alert when Bret M. Teller files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →