Assignee
SUPERSONIC AEROSPACE INT
US·13 granted patents·4 pending applications·465 citations·filing 2003–2005
Top patents by PatentIndex Score
17 records- 0194US6880784B1Automatic takeoff thrust management systemSUPERSONIC AEROSPACE INT·Filed 2003·Granted Apr 19, 2005·133 cites·25 claims
- 0289US7312725B2Display system for operating a device with reduced out-the-window visibilitySUPERSONIC AEROSPACE INT·Filed 2003·Granted Dec 25, 2007·69 cites·43 claims
- 0386US6913228B2Aircraft with active center of gravity controlSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 5, 2005·62 cites·20 claims
- 0476US6905091B2System and method for controlling the acoustic signature of a deviceSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jun 14, 2005·49 cites·28 claims
- 0576US6854687B1Nacelle integration with reflexed wing for sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted Feb 15, 2005·34 cites·21 claims
- 0675US6824092B1Aircraft tail configuration for sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted Nov 30, 2004·34 cites·20 claims
- 0772US6921045B2Supersonic aircraft with channel relief controlSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 26, 2005·29 cites·7 claims
- 0857US7070146B2Aircraft thickness/camber control device for low sonic boomSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 4, 2006·13 cites·21 claims
- 0955US6942178B2Mach weighted area ruling for supersonic vehiclesSUPERSONIC AEROSPACE INT·Filed 2003·Granted Sep 13, 2005·11 cites·10 claims
- 1053US6942182B2Forward inboard retracting main landing gearSUPERSONIC AEROSPACE INT·Filed 2003·Granted Sep 13, 2005·12 cites·25 claims
- 1151US7216830B2Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted May 15, 2007·9 cites·20 claims
- 1249US7311287B2Methods for incorporating area ruled surfaces in a supersonic aircraftSUPERSONIC AEROSPACE INT·Filed 2005·Granted Dec 25, 2007·4 cites·11 claims
- 1347US6935592B2Aircraft lift device for low sonic boomSUPERSONIC AEROSPACE INT·Filed 2003·Granted Aug 30, 2005·6 cites·17 claims
- 1442US2006058985A1Adjoint-based design variable adaptationSUPERSONIC AEROSPACE INT·Filed 2004·Application pending·0 cites
- 1537US2005116116A1Wing employing leading edge flaps and winglets to achieve improved aerodynamic performanceSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
- 1635US2005045764A1Canard position and dihedral for boom reduction and pitch/directional controlSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
- 1732US2005116107A1Area ruling for vertical stabilizersSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
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