Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Canard position and dihedral for boom reduction and pitch/directional control

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

US Patent 7416155 · Granted Aug 26, 2008

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Management of electronically published collections of content2025
Flagpole mounted lighting device2023
Remote control unit organizing wand2019
Flag pole light2017
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
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