Inventor · disambiguated record
John M. Morgenstern
Also filed as: MORGENSTERN JOHN M
19 granted patents·4 pending applications·514 citations·filing 1994–2005
96Inventor score
Files withSUPERSONIC AEROSPACE INT14LOCKHEED CORP5MORGENSTERN JOHN M2MC DONNELL DOUGLAS CORP1SUPERSONIE AEROSPACE INTERNATI1
Top patents by PatentIndex Score
23 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
- 0290USD417184SSupersonic business jetLOCKHEED CORP·Filed 1999·Granted Nov 30, 1999·48 cites·1 claims
- 0387USD428381SSupersonic business jetLOCKHEED CORP·Filed 1998·Granted Jul 18, 2000·40 cites·1 claims
- 0486US6913228B2Aircraft with active center of gravity controlSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 5, 2005·62 cites·20 claims
- 0578US5740984ALow sonic boom shock control/alleviation surfaceMC DONNELL DOUGLAS CORP·Filed 1994·Granted Apr 21, 1998·56 cites·14 claims
- 0677US6729577B2Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boomLOCKHEED CORP·Filed 2001·Granted May 4, 2004·30 cites·47 claims
- 0776US6905091B2System and method for controlling the acoustic signature of a deviceSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jun 14, 2005·49 cites·28 claims
- 0876US6854687B1Nacelle integration with reflexed wing for sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted Feb 15, 2005·34 cites·21 claims
- 0975US6824092B1Aircraft tail configuration for sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted Nov 30, 2004·34 cites·20 claims
- 1072US6921045B2Supersonic aircraft with channel relief controlSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 26, 2005·29 cites·7 claims
- 1157US7070146B2Aircraft thickness/camber control device for low sonic boomSUPERSONIC AEROSPACE INT·Filed 2003·Granted Jul 4, 2006·13 cites·21 claims
- 1255US7546977B2Passive aerodynamic sonic boom suppression for supersonic aircraftLOCKHEED CORP·Filed 2005·Granted Jun 16, 2009·4 cites·24 claims
- 1355US6942178B2Mach weighted area ruling for supersonic vehiclesSUPERSONIC AEROSPACE INT·Filed 2003·Granted Sep 13, 2005·11 cites·10 claims
- 1454US7416155B2Canard position and dihedral for boom reduction and pitch/directional controlSUPERSONIE AEROSPACE INTERNATI·Filed 2005·Granted Aug 26, 2008·6 cites·20 claims
- 1553US6959896B2Passive aerodynamic sonic boom suppression for supersonic aircraftLOCKHEED CORP·Filed 2003·Granted Nov 1, 2005·11 cites·16 claims
- 1651US7216830B2Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reductionSUPERSONIC AEROSPACE INT·Filed 2003·Granted May 15, 2007·9 cites·20 claims
- 1749US7311287B2Methods for incorporating area ruled surfaces in a supersonic aircraftSUPERSONIC AEROSPACE INT·Filed 2005·Granted Dec 25, 2007·4 cites·11 claims
- 1847US6935592B2Aircraft lift device for low sonic boomSUPERSONIC AEROSPACE INT·Filed 2003·Granted Aug 30, 2005·6 cites·17 claims
- 1942US2006058985A1Adjoint-based design variable adaptationSUPERSONIC AEROSPACE INT·Filed 2004·Application pending·0 cites
- 2037US2005116116A1Wing employing leading edge flaps and winglets to achieve improved aerodynamic performanceSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
- 2136US8473254B2Methods for configuring aircraft to meet performance goals and shock wave disturbance constraintsMORGENSTERN JOHN M·Filed 2003·Granted Jun 25, 2013·3 cites·22 claims
- 2235US2005045764A1Canard position and dihedral for boom reduction and pitch/directional controlSUPERSONIC AEROSPACE INT·Filed 2003·Application pending·0 cites
- 2332US2005116107A1Area 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 →