The present application relates to the technical field of a wheel, and particularly to a stored energy transmission mechanism and stored energy-driven wheel. In particular, a stored energy transmission mechanism is integrated with a rotating component, which is used to drive the rotating component. The stored energy transmission mechanism includes a center shaft, an elastic component, a transmission cover, a flywheel, and a flywheel seat. The elastic component is sleeved outside the center shaft and positioned in the transmission cover, with one end being fixedly connected with the center shaft and the other end being fixedly connected with the transmission. When the transmission cover is rotated and fitted with the center shaft, it can tighten the elastic component to store energy.

The present application relates to the technical field of a wheel, and particularly to a stored energy transmission mechanism and stored energy-driven wheel. In particular, a stored energy transmission mechanism is integrated with a rotating component, which is used to drive the rotating component. The stored energy transmission mechanism includes a center shaft, an elastic component, a transmission cover, a flywheel, and a flywheel seat. The elastic component is sleeved outside the center shaft and positioned in the transmission cover, with one end being fixedly connected with the center shaft and the other end being fixedly connected with the transmission. When the transmission cover is rotated and fitted with the center shaft, it can tighten the elastic component to store energy.

A stacked lamination endplate for a rotor that includes a number of adjacent laminations, stacked one on top of another, wherein each lamination has an identical shape, the shape having a central region, symmetric about a center axis, and a number of spokes, each spoke emanating radially outward from the central region, where each spoke includes a through-hole at its distal end, and wherein the laminations are stacked one on top of another and aligned, enabling, for each spoke, a bolt to be inserted through a corresponding through-hole of each lamination.

A stacked lamination endplate for a rotor that includes a number of adjacent laminations, stacked one on top of another, wherein each lamination has an identical shape, the shape having a central region, symmetric about a center axis, and a number of spokes, each spoke emanating radially outward from the central region, where each spoke includes a through-hole at its distal end, and wherein the laminations are stacked one on top of another and aligned, enabling, for each spoke, a bolt to be inserted through a corresponding through-hole of each lamination.

Disclosed are systems for converting rotational momentum into linear propulsion. A propulsion system includes one or more thrust units with masses controllably driven by actuators to generate inertia that thrusts a vehicle with the propulsion system in a desired direction. The propulsion system can be configured to have multiple units, each configured to generate thrust in a desired direction and counteract or neutralize thrust in other directions. The propulsion system can generate thrust via two operational cycles and/or through continuous operation. The propulsion system may comprise two mirroring units, each configured to operate in mirrored synchrony to generate a net thrust in a desired direction and counteract or neutralize thrust in other or undesired directions.

Disclosed are systems for converting rotational momentum into linear propulsion. A propulsion system includes one or more thrust units with masses controllably driven by actuators to generate inertia that thrusts a vehicle with the propulsion system in a desired direction. The propulsion system can be configured to have multiple units, each configured to generate thrust in a desired direction and counteract or neutralize thrust in other directions. The propulsion system can generate thrust via two operational cycles and/or through continuous operation. The propulsion system may comprise two mirroring units, each configured to operate in mirrored synchrony to generate a net thrust in a desired direction and counteract or neutralize thrust in other or undesired directions.

A flywheel assembly, including a cylinder including a first end and a second end, a first piston non-rotatably connected to the cylinder, the first piston being slidably engaged in the cylinder proximate the first end, a first biasing element operatively arranged in the cylinder to bias the first piston in a first axial direction, a first arm non-rotatably connected to the first piston, a second arm non-rotatably connected to the first piston, a first mass connected to the first arm, and a second mass connected to the second arm.

A flywheel assembly, including a cylinder including a first end and a second end, a first piston non-rotatably connected to the cylinder, the first piston being slidably engaged in the cylinder proximate the first end, a first biasing element operatively arranged in the cylinder to bias the first piston in a first axial direction, a first arm non-rotatably connected to the first piston, a second arm non-rotatably connected to the first piston, a first mass connected to the first arm, and a second mass connected to the second arm.

The gyroscopic impulse motor rigidly attaches to a superstructure. The gyroscopic impulse motor transfers a plurality of independent torqueing forces to the superstructure. By independent is meant the amount of force applied by any first independent torqueing force is independent of the amount of torqueing force applied by any second independent torqueing force generated by the gyroscopic impulse motor. By independent is further meant that the selected direction any first independent torqueing force is independent of the selected direction of any second independent torqueing force generated by the gyroscopic impulse motor. By controlling the amount and direction of the plurality of independent torqueing forces applied by the gyroscopic impulse motor to the superstructure, the superstructure can be rotated. By properly aligning the amount and direction of the plurality of independent torqueing forces applied by the gyroscopic impulse motor, a net propulsive force can further be generated.

The gyroscopic impulse motor rigidly attaches to a superstructure. The gyroscopic impulse motor transfers a plurality of independent torqueing forces to the superstructure. By independent is meant the amount of force applied by any first independent torqueing force is independent of the amount of torqueing force applied by any second independent torqueing force generated by the gyroscopic impulse motor. By independent is further meant that the selected direction any first independent torqueing force is independent of the selected direction of any second independent torqueing force generated by the gyroscopic impulse motor. By controlling the amount and direction of the plurality of independent torqueing forces applied by the gyroscopic impulse motor to the superstructure, the superstructure can be rotated. By properly aligning the amount and direction of the plurality of independent torqueing forces applied by the gyroscopic impulse motor, a net propulsive force can further be generated.