loadpatents
name:-0.010956048965454
name:-0.013341903686523
name:-0.00061988830566406
Arslan; Alan E. Patent Filings

Arslan; Alan E.

Patent Applications and Registrations

Patent applications and USPTO patent grants for Arslan; Alan E..The latest application filed is for "wing employing leading edge flaps and winglets to achieve improved aerodynamic performance".

Company Profile
0.11.11
  • Arslan; Alan E. - Santa Clarita CA US
*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.
Patent Activity
PatentDate
Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints
Grant 8,473,254 - Morgenstern , et al. June 25, 2
2013-06-25
Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
Grant 7,475,848 - Morgenstern , et al. January 13, 2
2009-01-13
Canard position and dihedral for boom reduction and pitch/directional control
Grant 7,416,155 - Cuccias , et al. August 26, 2
2008-08-26
Methods for incorporating area ruled surfaces in a supersonic aircraft
Grant 7,311,287 - Morgenstern , et al. December 25, 2
2007-12-25
Wing Employing Leading Edge Flaps And Winglets To Achieve Improved Aerodynamic Performance
App 20070262207 - Morgenstern; John M. ;   et al.
2007-11-15
Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction
Grant 7,216,830 - Quayle , et al. May 15, 2
2007-05-15
Canard position and dihedral for boom reduction and pitch/directional control
App 20060237580 - Cuccias; Robert S. ;   et al.
2006-10-26
Aircraft thickness/camber control device for low sonic boom
Grant 7,070,146 - Morgenstern , et al. July 4, 2
2006-07-04
Adjoint-based design variable adaptation
App 20060058985 - Arslan; Alan E. ;   et al.
2006-03-16
Methods for incorporating area rules surfaces in a supersonic aircraft
App 20050224640 - Morgenstern, John M. ;   et al.
2005-10-13
Mach weighted area ruling for supersonic vehicles
Grant 6,942,178 - Morgenstern , et al. September 13, 2
2005-09-13
Supersonic aircraft with channel relief control
Grant 6,921,045 - Chang , et al. July 26, 2
2005-07-26
Mach weighted area ruling for supersonic vehicles
App 20050121555 - Morgenstern, John M. ;   et al.
2005-06-09
Area ruling for vertical stabilizers
App 20050116107 - Morgenstern, John M. ;   et al.
2005-06-02
System, apparatus, and method for redistributing forces to meet performance goals and shock wave disturbance constraints
App 20050116108 - Morgenstern, John M. ;   et al.
2005-06-02
Supersonic Aircraft With Channel Relief Control
App 20050103929 - Chang, Ming ;   et al.
2005-05-19
Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction
App 20050067526 - Quayle, Brian ;   et al.
2005-03-31
Aircraft thickness/camber control device for low sonic boom
App 20050067525 - Morgenstern, John M. ;   et al.
2005-03-31
Canard position and dihedral for boom reduction and pitch/directional control
App 20050045764 - Morgenstern, John M. ;   et al.
2005-03-03
Nacelle integration with reflexed wing for sonic boom reduction
Grant 6,854,687 - Morgenstern , et al. February 15, 2
2005-02-15
Aircraft tail configuration for sonic boom reduction
Grant 6,824,092 - Franklin, III , et al. November 30, 2
2004-11-30

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