Alan E. Arslan
11Patents
6h-index
12Co-inventors
52Inventor score
Filing activity: Aug 29, 2003 → Jun 7, 2005
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7475848B2 | Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance | Emerging Cross-Sectional Technologies | 46 | Expired |
| US6854687B1 | Nacelle integration with reflexed wing for sonic boom reduction | Emerging Cross-Sectional Technologies | 22 | Expired |
| US6824092B1 | Aircraft tail configuration for sonic boom reduction | Performing Operations; Transporting | 18 | Expired |
| US6921045B2 | Supersonic aircraft with channel relief control | Emerging Cross-Sectional Technologies | 17 | Expired |
| US7070146B2 | Aircraft thickness/camber control device for low sonic boom | Emerging Cross-Sectional Technologies | 9 | Expired |
| US6942178B2 | Mach weighted area ruling for supersonic vehicles | Emerging Cross-Sectional Technologies | 6 | Expired |
| US7216830B2 | Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction | Emerging Cross-Sectional Technologies | 6 | Expired |
| US7416155B2 | Canard position and dihedral for boom reduction and pitch/directional control | Emerging Cross-Sectional Technologies | 5 | Active |
| US6935592B2 | Aircraft lift device for low sonic boom | Emerging Cross-Sectional Technologies | 4 | Expired |
| US7311287B2 | Methods for incorporating area ruled surfaces in a supersonic aircraft | Performing Operations; Transporting | 3 | Expired |
| US8473254B2 | Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints | Emerging Cross-Sectional Technologies | 1 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.