Patent ID: 11939043
Assignee: JETZERO, INC.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 0:
1. A landing gear for an aircraft comprising:
at least a nose gear disposed longitudinally forward of a center of gravity of an aircraft by a first distance and comprising a nose actuator configured to produce a nose actuator force supportive of at least a portion of a weight of the aircraft;
at least a main gear disposed longitudinally aft of the center of gravity of the aircraft by a second distance and comprising a main actuator configured to produce a main actuator force supportive of at least a portion of the aircraft;
a fluidic arrangement disposed between the nose actuator and the main actuator and configured to provide fluidic communication between the nose actuator and the main actuator, the fluidic arrangement comprising a valve configured to selectably affect the fluidic communication between the nose actuator and the main actuator; and
wherein the nose actuator and the main actuator are configured to decrease torque required to rotate the aircraft longitudinally about the center of gravity, while the at least a nose gear and the at least a main gear are in a ground position.