Bret M. Teller
24Patents
4h-index
32Co-inventors
59Inventor score
Filing activity: Feb 3, 2004 → Feb 7, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7478994B2 | Airfoil with supplemental cooling channel adjacent leading edge | Emerging Cross-Sectional Technologies | 59 | Expired |
| US7131818B2 | Airfoil with three-pass serpentine cooling channel and microcircuit | Emerging Cross-Sectional Technologies | 44 | Expired |
| US7097424B2 | Micro-circuit platform | Mechanical Engineering; Lighting; Heating | 29 | Expired |
| US10337332B2 | Airfoil having pedestals in trailing edge cavity | Emerging Cross-Sectional Technologies | 5 | Active |
| US10180067B2 | Mate face cooling holes for gas turbine engine component | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9243500B2 | Turbine blade platform with U-channel cooling holes | Emerging Cross-Sectional Technologies | 2 | Active |
| US9797260B2 | Engine component with wear surface protection | Emerging Cross-Sectional Technologies | 2 | Active |
| US10406596B2 | Core arrangement for turbine engine component | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11041390B1 | Turbine airfoil having film cooling hole arrangement | Emerging Cross-Sectional Technologies | 2 | Active |
| US10408071B2 | BOAS thermal protection | Emerging Cross-Sectional Technologies | 1 | Active |
| US10502067B2 | Dual-fed airfoil tip | Emerging Cross-Sectional Technologies | 1 | Active |
| US10641100B2 | Gas turbine engine airfoil cooling passage configuration | Emerging Cross-Sectional Technologies | 1 | Active |
| US10508552B2 | Internally cooled airfoil | Emerging Cross-Sectional Technologies | 1 | Active |
| US10871083B2 | Turbine vane for gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10844729B2 | Turbine vane for gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10830054B2 | Internally cooled airfoil | Emerging Cross-Sectional Technologies | 1 | Active |
| US10227875B2 | Gas turbine engine component with combined mate face and platform cooling | Emerging Cross-Sectional Technologies | 1 | Active |
| US11143037B1 | Turbine blade cooling hole arrangement | Emerging Cross-Sectional Technologies | 0 | Active |
| US11168571B2 | Airfoil having dead-end tip flag cavity | Emerging Cross-Sectional Technologies | 0 | Active |
| US10364680B2 | Gas turbine engine component having platform trench | Emerging Cross-Sectional Technologies | 0 | Active |
| US11148191B2 | Core arrangement for turbine engine component | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10815803B2 | BOAS thermal protection | Emerging Cross-Sectional Technologies | 0 | Active |
| US11661852B2 | Turbine blade trailing edge cooling feed | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10677071B2 | Turbine vane for gas turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.