Inventor profile of:

John M. Morgenstern

City:

Lancaster, California

Country:

United States

Published Applications:

18

Last publication date:

2007-11-15

Top Assignees for applications by John M. Morgenstern

The entities that hold a legal rights for patent applications filed by inventor Morgenstern John M.:

Recent patent applications by Morgenstern John M.

John M. Morgenstern from Lancaster, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2007-11-15
US20070262207A1
Performing operations; transporting

Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance

#2 | 2007-11-01
US20070252028A1
Performing operations; transporting

Passive aerodynamic sonic boom suppression for supersonic aircraft

#3 | 2006-10-26
US20060237580A1
Performing operations; transporting

Canard position and dihedral for boom reduction and pitch/directional control

#4 | 2006-03-16
US20060058985A1
Physics

Adjoint-based design variable adaptation

#5 | 2005-11-01
US10614393
-

Passive aerodynamic sonic boom suppression for supersonic aircraft

#6 | 2005-10-13
US20050224640A1
Performing operations; transporting

Methods for incorporating area ruled surfaces in a supersonic aircraft

#7 | 2005-06-09
US20050121555A1
Performing operations; transporting

Mach weighted area ruling for supersonic vehicles

#8 | 2005-06-02
US20050116116A1
Performing operations; transporting

Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance

#9 | 2005-06-02
US20050116108A1
Performing operations; transporting

Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints

#10 | 2005-06-02
US20050116107A1
Performing operations; transporting

Area ruling for vertical stabilizers

#11 | 2005-05-19
US20050103929A1
Performing operations; transporting

Supersonic aircraft with channel relief control

#12 | 2005-05-12
US20050098681A1
Physics

System and method for controlling the acoustic signature of a device

#13 | 2005-03-31
US20050067526A1
Performing operations; transporting

Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction

#14 | 2005-03-31
US20050067525A1
Performing operations; transporting

Aircraft thickness/camber control device for low sonic boom

#15 | 2005-03-10
US20050051666A1
Performing operations; transporting

Aircraft with active center of gravity control

#16 | 2005-03-03
US20050045764A1
Performing operations; transporting

Canard position and dihedral for boom reduction and pitch/directional control

#17 | 2005-03-03
US20050045763A1
Performing operations; transporting

Aircraft lift device for low sonic boom

#18 | 2005-02-15
US10713515
-

Nacelle integration with reflexed wing for sonic boom reduction

InventorID:

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