Irwin D. Singer
6Patents
5h-index
11Co-inventors
60Inventor score
Filing activity: Mar 11, 1977 → Dec 27, 2012
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US4151710A | Lubrication cooling system for aircraft engine accessory | Emerging Cross-Sectional Technologies | 69 | Expired |
| US5827043A | Coolable airfoil | Emerging Cross-Sectional Technologies | 42 | Expired |
| US7871245B2 | Method for forming turbine blade with angled internal ribs | Mechanical Engineering; Lighting; Heating | 11 | Active |
| US7569172B2 | Method for forming turbine blade with angled internal ribs | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US7862325B2 | Apparatus for forming turbine blade with angled internal ribs | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9476308B2 | Gas turbine engine serpentine cooling passage with chevrons | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.