Patent ID: 11958592
Assignee: JETZERO, INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 6:
7. A rotating landing gear system for an aircraft, comprising:
a nose gear disposed proximate a front of the aircraft, the nose gear comprising:
a main strut/gear link;
a rotatable aft/retract link rotatably attached to the main strut/gear link;
a pivot-piston rotatably attached to the aft/retract link; and

two or more main gears disposed proximate a rear of the aircraft;
two or more main cylinders, each mechanically coupled to the two or more main gears to move the main gears between a third position, in which the main gears are extended, and a fourth position, in which the main gears are retracted; and

a hydraulic valve hydraulically coupling an upper master link, the pivot-piston, and the main cylinders to enable fluid to flow between a nose cylinder and the main cylinders to change a pitch angle of the aircraft with respect to the ground.