Matthew A. Devore
66Patents
11h-index
55Co-inventors
77Inventor score
Filing activity: Dec 21, 2004 → Jun 17, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7775768B2 | Turbine component with axially spaced radially flowing microcircuit cooling channels | Mechanical Engineering; Lighting; Heating | 36 | Active |
| US8113780B2 | Castings, casting cores, and methods | Emerging Cross-Sectional Technologies | 27 | Active |
| US9296039B2 | Gas turbine engine airfoil impingement cooling | Emerging Cross-Sectional Technologies | 27 | Active |
| US10107128B2 | Cooling channels for gas turbine engine component | Emerging Cross-Sectional Technologies | 25 | Active |
| US8171978B2 | Castings, casting cores, and methods | Emerging Cross-Sectional Technologies | 24 | Active |
| US8137068B2 | Castings, casting cores, and methods | Emerging Cross-Sectional Technologies | 21 | Active |
| US8356978B2 | Turbine airfoil platform cooling core | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US7815414B2 | Airfoil mini-core plugging devices | Emerging Cross-Sectional Technologies | 19 | Active |
| US7779892B2 | Investment casting cores and methods | Performing Operations; Transporting | 16 | Active |
| US8911208B2 | Castings, casting cores, and methods | Emerging Cross-Sectional Technologies | 16 | Active |
| US7600966B2 | Turbine airfoil with improved cooling | Emerging Cross-Sectional Technologies | 13 | Active |
| US8449254B2 | Branched airfoil core cooling arrangement | Emerging Cross-Sectional Technologies | 9 | Active |
| US7465154B2 | Gas turbine engine component suction side trailing edge cooling scheme | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US7220934B2 | Method of producing cooling holes in highly contoured airfoils | Emerging Cross-Sectional Technologies | 8 | Expired |
| US9551228B2 | Airfoil and method of making | Emerging Cross-Sectional Technologies | 7 | Active |
| US9879546B2 | Airfoil cooling circuits | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8511994B2 | Serpentine cored airfoil with body microcircuits | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US10641099B1 | Impingement cooling for a gas turbine engine component | Emerging Cross-Sectional Technologies | 5 | Active |
| US7431559B2 | Dirt separation for impingement cooled turbine components | Mechanical Engineering; Lighting; Heating | 4 | Expired |
| US9670797B2 | Modulated turbine vane cooling | Emerging Cross-Sectional Technologies | 4 | Active |
| US9121290B2 | Turbine airfoil with body microcircuits terminating in platform | Emerging Cross-Sectional Technologies | 4 | Active |
| US8353329B2 | Ceramic core tapered trip strips | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10156144B2 | Turbine airfoil and method of cooling | Emerging Cross-Sectional Technologies | 3 | Active |
| US10605094B2 | Internal cooling cavity with trip strips | Emerging Cross-Sectional Technologies | 2 | Active |
| US10502065B2 | Gas turbine engine component with rib support | Mechanical Engineering; Lighting; Heating | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.