The invention relates to power engineering and to power generation as a whole, in the field of electrical machines for converting electrical energy into mechanical energy or vice versa, and can be used in many spheres of human activity. In order to increase the efficiency and effectiveness of converting electrical energy into mechanical energy or vice versa and to expand additional functional capabilities, the primary Newtonian laws of mechanics and the law of conservation of energy are fulfilled, and conformity with the International Standard Unit of measurement for work is provided. A previously unknown method for operating electromechanical motors and electromechanical machines is proposed. The new method for operating an electromechanical motor and the motor make it possible to achieve the actual energy properties of electromechanical machines. The work performed or the power generated by the proposed invention is always higher than in the prior art.

A sphere-on-sphere chassis system is disclosed. The sphere-on-sphere chassis system may include a first hollow sphere having a first diameter and a second hollow sphere positioned inside of the first sphere to form a channel therebetween. The second hollow sphere may have a second diameter. The second diameter is less than the first diameter. The sphere-on-sphere chassis system may further include a liquid filling at least a portion of the channel. The liquid may be a conductive solution. Each of the hollow spheres include a component layer with pockets for housing electromagnets, and may house wireless energy transmission devices such as resonant inductive chargers and resonant inductive receivers. The spherical device is designed so that electromagnets may be configured to emit positive and negative electromagnetic waves inwardly and outwardly with respect to the center of each sphere to create relative movement between the inner sphere and the outer sphere.

The invention relates to a motor with a stator (2, 2) and a rotor (1, 1), which can be driven about an axial direction (4). The invention is characterized in that at least one of the stator and the rotor, in particular the stator, which has a winding arrangement that can be supplied with a current, can be radially compressed and expanded.

A driving apparatus comprises a stator (21), a rotor (22) and a deformation connector (23). The rotor is connected to the stator through the deformation connector. An external driving force drives the deformation connector to have deformation so that the rotor changes its position with respect to the stator. Under the condition that no external driving force is applied, the deformation connector remains at a force balanced position (x0). The force on the deformation connector comprises a deformation force (F1) of the deformation connector and a first primitive force (F2) in opposite direction to the deformation force (F1). Also provided is a device fabrication method. Because the deformation connector keeps balance under the effect of the deformation force and the first primitive force, a small external driving force is required when the driving apparatus operates near the balance point, hereby reducing power consumption.

A device for generating thrust using the dynamic Casimir effect comprising: an epitaxial stack of closely spaced parallel semiconductor laminae; and a voltage source; wherein each said semiconductor lamina is connected to said voltage source such that said voltage source can apply voltage to each semiconductor lamina.

A solid-state electromagnetic rotor, including a plurality of salient pole pieces arranged around a supporting structure, wherein a first end of each salient pole piece is attached to the support structure and a second end of each salient pole piece points outward away from the sup-porting structure. The wires wound around each salient pole piece, wherein when the wires of the plurality of salient pole pieces are sequentially excited by an excitation circuit. The salient pole pieces are energized to provide a moving polar magnetic field in the form of distinct magnetic poles as desired to accomplish power generation.

A magnetic drive enhancement is provided to offset kinetic forces found in a rotational system to improve the mechanical efficiency of the rotational system. A housing includes rotationally biased magnetic fields in which a central axle or driveshaft may rotate. The magnetic fields are generated, shaped, and rotationally biased by a plurality of driving magnets and magnetic shields. Attached to the driveshaft are magnetic receivers, which are influenced by the rotationally biased magnetic fields at varying strengths as they orbit within the housing. The magnetic fields are shaped to provide increasing and decreasing strength of flux to counteract the physical forces experienced by the driveshaft to thereby increase the efficiency of the rotational system.

The invention relates to a motor with a stator (2, 2) and a rotor (1, 1), which can be driven about an axial direction (4). The invention is characterized in that at least one of the stator and the rotor, in particular the stator, which has a winding arrangement that can be supplied with a current, can be radially compressed and expanded.

As is scientifically well known, magnetic flux is a physical force (i.e. the Lorentz force and Ampere's force). The invention utilizes a plurality of electromagnetic and or plasma coils to create high pressure, high velocity magnetic flux directed through variable exhaust nozzles or a cone shaped electrical coil to create thrust for spacecraft. Electrically charged ions or electrons are collected and propelled along the created magnetic flux lines through the variable exhaust nozzles or electrical coils to create thrust.

As is scientifically well known, magnetic flux is a physical force (i.e. the Lorentz force and Ampere's force). The invention utilizes a plurality of electromagnetic and or plasma coils to create high pressure, high velocity magnetic flux directed through variable exhaust nozzles or a cone shaped electrical coil to create thrust for spacecraft. Electrically charged ions or electrons are collected and propelled along the created magnetic flux lines through the variable exhaust nozzles or electrical coils to create thrust.