John M. Morgenstern

Person

Palmdale, CA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Methods for configuring aircraft to meet performance goals and shoc...
- Patent number 8,473,254
- Issue date Jun 25, 2013
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Passive aerodynamic sonic boom suppression for supersonic aircraft
- Patent number 7,546,977
- Issue date Jun 16, 2009
- Lockheed-Martin Corporation
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing employing leading edge flaps and winglets to achieve improved...
- Patent number 7,475,848
- Issue date Jan 13, 2009
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Canard position and dihedral for boom reduction and pitch/direction...
- Patent number 7,416,155
- Issue date Aug 26, 2008
- Supersonie Aerospace International, LLC
- Robert S. Cuccias
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Methods for incorporating area ruled surfaces in a supersonic aircraft
- Patent number 7,311,287
- Issue date Dec 25, 2007
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing gull integration nacelle clearance, compact landing gear stowa...
- Patent number 7,216,830
- Issue date May 15, 2007
- Supersonic Aerospace International, LLC
- Brian Quayle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft thickness/camber control device for low sonic boom
- Patent number 7,070,146
- Issue date Jul 4, 2006
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Passive aerodynamic sonic boom suppression for supersonic aircraft
- Patent number 6,959,896
- Issue date Nov 1, 2005
- Lockheed Martin Corporation
- Tom Hartmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Mach weighted area ruling for supersonic vehicles
- Patent number 6,942,178
- Issue date Sep 13, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft lift device for low sonic boom
- Patent number 6,935,592
- Issue date Aug 30, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Supersonic aircraft with channel relief control
- Patent number 6,921,045
- Issue date Jul 26, 2005
- Supersonic Aerospace International, LLC
- Ming Chang
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft with active center of gravity control
- Patent number 6,913,228
- Issue date Jul 5, 2005
- Supersonic Aerospace International, LLC
- Howard Lee
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System and method for controlling the acoustic signature of a device
- Patent number 6,905,091
- Issue date Jun 14, 2005
- Supersonic Aerospace International, LLC
- Barry L. Berson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle integration with reflexed wing for sonic boom reduction
- Patent number 6,854,687
- Issue date Feb 15, 2005
- Supersonic Aerospace International, Inc.
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft tail configuration for sonic boom reduction
- Patent number 6,824,092
- Issue date Nov 30, 2004
- Supersonic Aerospace International, LLC
- Walter M. Franklin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Supersonic business jet
- Patent number D428381
- Issue date Jul 18, 2000
- Lockheed Martin Corporation
- Thomas M. Hartmann
- D12 - Transportation
Information Patent Grant
Supersonic business jet
- Patent number D417184
- Issue date Nov 30, 1999
- Lockheed Martin Corporation
- Tom Hartmann
- D12 - Transportation

Patents Applicationslast 30 patents

Information Patent Application
WING EMPLOYING LEADING EDGE FLAPS AND WINGLETS TO ACHIEVE IMPROVED...
- Publication number 20070262207
- Publication date Nov 15, 2007
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Canard position and dihedral for boom reduction and pitch/direction...
- Publication number 20060237580
- Publication date Oct 26, 2006
- Robert S. Cuccias
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Adjoint-based design variable adaptation
- Publication number 20060058985
- Publication date Mar 16, 2006
- Supersonic Aerospace International, LLC
- Alan E. Arslan
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
Methods for incorporating area rules surfaces in a supersonic aircraft
- Publication number 20050224640
- Publication date Oct 13, 2005
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Mach weighted area ruling for supersonic vehicles
- Publication number 20050121555
- Publication date Jun 9, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Area ruling for vertical stabilizers
- Publication number 20050116107
- Publication date Jun 2, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Wing employing leading edge flaps and winglets to achieve improved...
- Publication number 20050116116
- Publication date Jun 2, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
System, apparatus, and method for redistributing forces to meet per...
- Publication number 20050116108
- Publication date Jun 2, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
SUPERSONIC AIRCRAFT WITH CHANNEL RELIEF CONTROL
- Publication number 20050103929
- Publication date May 19, 2005
- Supersonic Aerospace International, LLC
- Ming Chang
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
SYSTEM AND METHOD FOR CONTROLLING THE ACOUSTIC SIGNATURE OF A DEVICE
- Publication number 20050098681
- Publication date May 12, 2005
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G01 - MEASURING TESTING
Information Patent Application
Wing gull integration nacelle clearance, compact landing gear stowa...
- Publication number 20050067526
- Publication date Mar 31, 2005
- Supersonic Aerospace International, LLC
- Brian Quayle
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Aircraft thickness/camber control device for low sonic boom
- Publication number 20050067525
- Publication date Mar 31, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Aircraft with active center of gravity control
- Publication number 20050051666
- Publication date Mar 10, 2005
- Supersonic Aerospace International, LLC
- Howard Lee
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Aircraft lift device for low sonic boom
- Publication number 20050045763
- Publication date Mar 3, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Canard position and dihedral for boom reduction and pitch/direction...
- Publication number 20050045764
- Publication date Mar 3, 2005
- Supersonic Aerospace International, LLC
- John M. Morgenstern
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Passive aerodynamic sonic boom suppression for supersonic aircraft
- Publication number 20040245380
- Publication date Dec 9, 2004
- Lockheed Martin Corporation
- Tom Hartmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Passive aerodynamic sonic boom suppression for supersonic aircraft
- Publication number 20040065774
- Publication date Apr 8, 2004
- Lockheed Martin Corporation
- Tom Hartmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS

John M. Morgenstern

Person

Patents Grantslast 30 patents

Methods for configuring aircraft to meet performance goals and shoc...

Passive aerodynamic sonic boom suppression for supersonic aircraft

Wing employing leading edge flaps and winglets to achieve improved...

Canard position and dihedral for boom reduction and pitch/direction...

Methods for incorporating area ruled surfaces in a supersonic aircraft

Wing gull integration nacelle clearance, compact landing gear stowa...

Aircraft thickness/camber control device for low sonic boom

Passive aerodynamic sonic boom suppression for supersonic aircraft

Mach weighted area ruling for supersonic vehicles

Aircraft lift device for low sonic boom

Supersonic aircraft with channel relief control

Aircraft with active center of gravity control

System and method for controlling the acoustic signature of a device

Nacelle integration with reflexed wing for sonic boom reduction

Aircraft tail configuration for sonic boom reduction

Supersonic business jet

Supersonic business jet

Patents Applicationslast 30 patents

WING EMPLOYING LEADING EDGE FLAPS AND WINGLETS TO ACHIEVE IMPROVED...

Canard position and dihedral for boom reduction and pitch/direction...

Adjoint-based design variable adaptation

Methods for incorporating area rules surfaces in a supersonic aircraft

Mach weighted area ruling for supersonic vehicles

Area ruling for vertical stabilizers

Wing employing leading edge flaps and winglets to achieve improved...

System, apparatus, and method for redistributing forces to meet per...

SUPERSONIC AIRCRAFT WITH CHANNEL RELIEF CONTROL

SYSTEM AND METHOD FOR CONTROLLING THE ACOUSTIC SIGNATURE OF A DEVICE

Wing gull integration nacelle clearance, compact landing gear stowa...

Aircraft thickness/camber control device for low sonic boom

Aircraft with active center of gravity control

Aircraft lift device for low sonic boom

Canard position and dihedral for boom reduction and pitch/direction...

Passive aerodynamic sonic boom suppression for supersonic aircraft

Passive aerodynamic sonic boom suppression for supersonic aircraft