Jeffrey S. Beattie
26Patents
5h-index
35Co-inventors
65Inventor score
Filing activity: Sep 13, 2004 → May 31, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7121800B2 | Turbine blade nested seal damper assembly | Mechanical Engineering; Lighting; Heating | 53 | Expired |
| US8356978B2 | Turbine airfoil platform cooling core | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US8240987B2 | Gas turbine engine systems involving baffle assemblies | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US9279331B2 | Gas turbine engine airfoil with dirt purge feature and core for making same | Emerging Cross-Sectional Technologies | 6 | Active |
| US10364682B2 | Platform cooling core for a gas turbine engine rotor blade | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9932834B2 | Rotor blade with a conic spline fillet at an intersection between a platform and a neck | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10907481B2 | Platform cooling core for a gas turbine engine rotor blade | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9938837B2 | Gas turbine engine airfoil trailing edge passage and core for making same | Emerging Cross-Sectional Technologies | 3 | Active |
| US9587495B2 | Mistake proof damper pocket seals | Emerging Cross-Sectional Technologies | 3 | Active |
| US10180067B2 | Mate face cooling holes for gas turbine engine component | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10100648B2 | Damper seal installation features | Emerging Cross-Sectional Technologies | 2 | Active |
| US8942837B2 | Method for inspecting a manufacturing device | Emerging Cross-Sectional Technologies | 2 | Active |
| US9422817B2 | Turbine blade root with microcircuit cooling passages | Emerging Cross-Sectional Technologies | 2 | Active |
| US9243500B2 | Turbine blade platform with U-channel cooling holes | Emerging Cross-Sectional Technologies | 2 | Active |
| US10227875B2 | Gas turbine engine component with combined mate face and platform cooling | Emerging Cross-Sectional Technologies | 1 | Active |
| US10253642B2 | Gas turbine engine with disk having periphery with protrusions | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9546556B2 | Turbine blade root profile | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8257045B2 | Platforms with curved side edges and gas turbine engine systems involving such platforms | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10533453B2 | Engine component having platform with passageway | Emerging Cross-Sectional Technologies | 0 | Active |
| US10563525B2 | Blade feature to support segmented coverplate | Emerging Cross-Sectional Technologies | 0 | Active |
| US10822952B2 | Feature to provide cooling flow to disk | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10301958B2 | Gas turbine engine with seal having protrusions | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10167722B2 | Disk outer rim seal | Emerging Cross-Sectional Technologies | 0 | Active |
| US10203196B2 | Inspecting one or more apertures of a component using moldable material | Physics | 0 | Active |
| US10226814B2 | Cast component having corner radius to reduce recrystallization | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.