Supersonic Aerospace International, LLC

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Las Vegas, NV, US

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Patents Grantslast 30 patents

Information Patent Grant
System and method for customizing multiple windows of information o...
- Patent number 8,484,576
- Issue date Jul 9, 2013
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G01 - MEASURING TESTING
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
System and method for mounting sensors and cleaning sensor aperture...
- Patent number 7,982,767
- Issue date Jul 19, 2011
- Supersonic Aerospace International, LLC
- Barry L. Berson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Display system for operating a device with reduced out-the-window v...
- Patent number 7,312,725
- Issue date Dec 25, 2007
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G06 - COMPUTING CALCULATING COUNTING
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
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
Forward inboard retracting main landing gear
- Patent number 6,942,182
- Issue date Sep 13, 2005
- Supersonic Aerospace International, LLC
- Brian Quayle
- 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
Automatic takeoff thrust management system
- Patent number 6,880,784
- Issue date Apr 19, 2005
- Supersonic Aerospace International, LLC
- Todd Wilkinson
- 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

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
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
FORWARD INBOARD RETRACTING MAIN LANDING GEAR
- Publication number 20050178900
- Publication date Aug 18, 2005
- Supersonic Aerospace International, LLC
- Brian Quayle
- 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 mounting sensors and cleaning sensor aperture...
- Publication number 20050099433
- Publication date May 12, 2005
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G06 - COMPUTING CALCULATING COUNTING
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
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
System and method for providing out-the-window displays for a device
- Publication number 20050007386
- Publication date Jan 13, 2005
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
Display system for operating a device with reduced out-the-window v...
- Publication number 20050007261
- Publication date Jan 13, 2005
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
System and method for customizing multiple windows of information o...
- Publication number 20040210847
- Publication date Oct 21, 2004
- Supersonic Aerospace International, LLC
- Barry L. Berson
- G06 - COMPUTING CALCULATING COUNTING

Supersonic Aerospace International, LLC

Organization

Patents Grantslast 30 patents

System and method for customizing multiple windows of information o...

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

System and method for mounting sensors and cleaning sensor aperture...

Display system for operating a device with reduced out-the-window v...

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

Mach weighted area ruling for supersonic vehicles

Forward inboard retracting main landing gear

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

Automatic takeoff thrust management system

Nacelle integration with reflexed wing for sonic boom reduction

Aircraft tail configuration for sonic boom reduction

Patents Applicationslast 30 patents

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

Adjoint-based design variable adaptation

FORWARD INBOARD RETRACTING MAIN LANDING GEAR

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 mounting sensors and cleaning sensor aperture...

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

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

System and method for providing out-the-window displays for a device

Display system for operating a device with reduced out-the-window v...

System and method for customizing multiple windows of information o...

Trademarklast 30 trademarks