Eric Schroeder
17Patents
5h-index
36Co-inventors
66Inventor score
Filing activity: Jun 29, 1993 → Nov 2, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7070641B1 | Carbon media filter element | Emerging Cross-Sectional Technologies | 63 | Expired |
| US9840930B2 | Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoil | Mechanical Engineering; Lighting; Heating | 22 | Active |
| US5340348A | Doll with patch and cover for releasably engaging a removable item | Emerging Cross-Sectional Technologies | 13 | Expired |
| US9863256B2 | Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil usable in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US8926267B2 | Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8926283B2 | Turbine blade angel wing with pumping features | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9181816B2 | Seal assembly including grooves in an aft facing side of a platform in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9920646B2 | Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern | Emerging Cross-Sectional Technologies | 4 | Active |
| US10253637B2 | Method and system for improving turbine blade performance | Emerging Cross-Sectional Technologies | 3 | Active |
| US10227778B2 | Sheet, board or panel | Emerging Cross-Sectional Technologies | 3 | Active |
| US9017014B2 | Aft outer rim seal arrangement | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10934858B2 | Method and system for improving turbine blade performance | Emerging Cross-Sectional Technologies | 1 | Active |
| US11970979B2 | Turbine engine with shockwave attenuation | Emerging Cross-Sectional Technologies | 0 | Active |
| US10697306B2 | Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11994041B2 | Advanced aero diffusers for turbine frames and outlet guide vanes | Emerging Cross-Sectional Technologies | 0 | Active |
| US10363562B2 | Apparatus to reduce size of material | Performing Operations; Transporting | 0 | Active |
| US11519333B2 | Turbine engine with shockwave attenuation | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.