Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Aircraft thickness/camber control device for low sonic boom

Aircraft thickness/camber control device for low sonic boom

US Patent 7070146 · Granted Jul 4, 2006

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Methods for configuring aircraft to meet performance goals and shock wave distur2013
Methods for configuring aircraft to meet performance goals and shock wave distur2013
Passive aerodynamic sonic boom suppression for supersonic aircraft2009
Wing employing leading edge flaps and winglets to achieve improved aerodynamic p2009
Wing employing leading edge flaps and winglets to achieve improved aerodynamic p2009
Canard position and dihedral for boom reduction and pitch/directional control2008
Canard position and dihedral for boom reduction and pitch/directional control2008
Methods for incorporating area ruled surfaces in a supersonic aircraft2007
Methods for incorporating area ruled surfaces in a supersonic aircraft2007
Wing gull integration nacelle clearance, compact landing gear stowage, and sonic2007
Wing gull integration nacelle clearance, compact landing gear stowage, and sonic2007
Passive aerodynamic sonic boom suppression for supersonic aircraft2005