Inventor · disambiguated record
Alan E. Arslan
Also filed as: ARSLAN ALAN · ARSLAN ALAN E
11 granted patents·3 pending applications·214 citations·filing 2003–2005
91Inventor score
Top patents by PatentIndex Score
14 records- 0194US7475848B2Wing employing leading edge flaps and winglets to achieve improved aerodynamic performanceMORGENSTERN JOHN M·Filed 2005·Granted Jan 13, 2009·65 cites·12 claims
- 0276US6854687B1Nacelle integration with reflexed wing for sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted Feb 15, 2005·34 cites·21 claims
- 0375US6824092B1Aircraft tail configuration for sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted Nov 30, 2004·34 cites·20 claims
- 0472US6921045B2Supersonic aircraft with channel relief controlSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 26, 2005·29 cites·7 claims
- 0557US7070146B2Aircraft thickness/camber control device for low sonic boomSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 4, 2006·13 cites·21 claims
- 0655US6942178B2Mach weighted area ruling for supersonic vehiclesSUPERSONIC AEROSPACE INT·Filed 2003·Granted Sep 13, 2005·11 cites·10 claims
- 0754US7416155B2Canard position and dihedral for boom reduction and pitch/directional controlSUPERSONIE AEROSPACE INTERNATI·Filed 2005·Granted Aug 26, 2008·6 cites·20 claims
- 0851US7216830B2Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted May 15, 2007·9 cites·20 claims
- 0949US7311287B2Methods for incorporating area ruled surfaces in a supersonic aircraftSUPERSONIC AEROSPACE INT·Filed 2005·Granted Dec 25, 2007·4 cites·11 claims
- 1047US6935592B2Aircraft lift device for low sonic boomSUPERSONIC AEROSPACE INT·Filed 2003·Granted Aug 30, 2005·6 cites·17 claims
- 1142US2006058985A1Adjoint-based design variable adaptationSUPERSONIC AEROSPACE INT·Filed 2004·Application pending·0 cites
- 1236US8473254B2Methods for configuring aircraft to meet performance goals and shock wave disturbance constraintsMORGENSTERN JOHN M·Filed 2003·Granted Jun 25, 2013·3 cites·22 claims
- 1335US2005045764A1Canard position and dihedral for boom reduction and pitch/directional controlSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
- 1432US2005116107A1Area ruling for vertical stabilizersSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →