Eric W. Malmborg
35Patents
5h-index
34Co-inventors
69Inventor score
Filing activity: Mar 27, 2000 → Dec 22, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6339878B1 | Method of repairing an airfoil | Emerging Cross-Sectional Technologies | 28 | Expired |
| US7811053B2 | Fan rotor design for coincidence avoidance | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US6766639B2 | Acoustic-structural LPC splitter | Mechanical Engineering; Lighting; Heating | 9 | Expired |
| US6881032B2 | Exit stator mounting | Mechanical Engineering; Lighting; Heating | 7 | Expired |
| US8540483B2 | Turbine engine rotating cavity anti-vortex cascade | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US10557353B2 | Hollow fan blade constrained layer damper | Emerging Cross-Sectional Technologies | 4 | Active |
| US9145771B2 | Rotor assembly disk spacer for a gas turbine engine | Emerging Cross-Sectional Technologies | 4 | Active |
| US10077663B2 | Gas turbine engine rotor stack assembly | Emerging Cross-Sectional Technologies | 4 | Active |
| US8465252B2 | Turbine engine rotating cavity anti-vortex cascade | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US11174737B2 | Airfoil with cover for gas turbine engine | Emerging Cross-Sectional Technologies | 4 | Active |
| US8177503B2 | Turbine engine rotating cavity anti-vortex cascade | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US11033993B2 | Method of forming gas turbine engine components | Emerging Cross-Sectional Technologies | 3 | Active |
| US11014190B2 | Hollow airfoil with catenary profiles | Emerging Cross-Sectional Technologies | 3 | Active |
| US10995632B2 | Damped airfoil for a gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US11248477B2 | Hybridized airfoil for a gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10502064B2 | Power beam welded cavity-back titanium hollow fan blade | Emerging Cross-Sectional Technologies | 2 | Active |
| US11236619B2 | Multi-cover gas turbine engine component | Emerging Cross-Sectional Technologies | 2 | Active |
| US8550784B2 | Gas turbine engine rotor construction | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US8540482B2 | Rotor assembly for gas turbine engine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9080449B2 | Gas turbine engine seal assembly having flow-through tube | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10808541B2 | Fan blade for a gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10793943B2 | Method of producing a gas turbine engine component | Emerging Cross-Sectional Technologies | 2 | Active |
| US8162615B2 | Split disk assembly for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10443613B2 | Hollow fan blade with structural ribs | Emerging Cross-Sectional Technologies | 1 | Active |
| US10612387B2 | Airfoil damping assembly for gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.