Jetzero, Inc.

Brent Tyler Scheneman

Blaine Knight Rawdon

Mark Allan Page

Myles Leonard Baker

Jay Fletcher Kempf

Daniel Tran

Daniel Sean Stuewe

Systems and methods for mechanically rotating an aircraft about its center-of-gravity (C) are disclosed. The system can enable the rear, or main, landing gear to squat, while the nose landing gear raises to generate a positive angle of attack for the aircraft for takeoff or landing. The system can also enable the nose gear and main gear to return to a relatively level fuselage attitude for ground operations. The system can include one or more hydraulically linked hydraulic cylinders to control the overall height of the nose gear and the main gear. Because the hydraulic cylinders are linked, a change on the length of the nose cylinder generates a proportional, and opposite, change in the length of the main cylinder, and vice-versa. A method and control system for monitoring and controlling the relative positions of the nose gear and main gear is also disclosed.

Tilting landing gear systems and methods

A coupled landing gear apparatus for an aircraft including at least a nose gear disposed forward of a neutral point of an aircraft by a first distance and at least a main gear disposed aft of the neutral point of the aircraft by a second distance. The at least a nose gear and the at least a main gear are in communication with one another.

Coupled landing gear and methods of use

Growing community of inventors

Redondo Beach, CA, United States of America

Brent Tyler Scheneman