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.

An apparatus including a stator configured to be stationarily connected to a housing; and a rotor configured to have a robot arm connected thereto. The rotor includes a shaft and an robot arm mount adjustably connected to the shaft. The stator and the rotor include mechanical reference locators to temporarily stationarily locate the robot arm mount to the stator for subsequently stationarily fixing the robot arm mount to the shaft.

The present invention discloses a power generation device, a power generation assembly and a method of generation of power. The power generation device includes a housing; a leadscrew, a first end of the leadscrew is connected to the top of the housing, and a second end of the leadscrew extends toward the bottom of the housing; a magnetic stator and a magnetic rotor, the magnetic stator is arranged at the bottom of the housing, and the magnetic rotor is mounted at the second end of the leadscrew; a shaft sleeve, a threaded hole is provided on the shaft sleeve, and the leadscrew is in screw joint within the threaded hole; a connecting shaft and a pressing plate.

Various embodiments may include a drone for triggering sea mines by means of an external magnetic field. For example a drone may include: a drive having an electric motor; the electric motor comprising a stator and a rotor mounted on a shaft. The stator includes a stator winding arranged on a first carrier. The rotor includes a second carrier and a magnetic or electromagnetic element arranged on the second carrier. The element may be configured to magnetically interact with the stator winding to form a superordinate magnetic field during operation of the electric motor. During operation, the electric motor forms an external magnetic field outside of the electric motor with a magnetic flux density of at least 0.5 mT.

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.

Provided is a microgenerator of a flat design including a base plate having an external side and an internal side; a stator which is a circular multipole metal stator coil for producing an electric voltage, which stator is fixedly positioned on the internal side of the base plate; a rotor wheel including a circular multipole magnetic array, which rotor wheel is rotatably positioned on the internal side of the base plate; and an actuating system for rotating the rotor wheel. The actuating system includes an input mechanism provided at an external side of the base plate which input mechanism is preferably movable in two directions, and a rotatable rotor shaft which has a concentric orientation to the rotor wheel. The rotor shaft is drivingly engaged with the input mechanism either in a direct or indirect manner. A first side of the rotor shaft is provided with a rotor gear wheel that is in driving engagement with the input mechanism either in a direct or indirect manner, and a second side of the rotor shaft is drivingly connected to the rotor wheel. The actuating system is provided with at least one clutch system to establish a unidirectional driving engagement of the actuating system with the rotor wheel.

As is scientifically well know 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.

A time-varying current from a DC voltage-source, flows through a primary winding of a magnetic circuit containing permanent magnets, induces more inductive voltages across different windings. The windings are wrapped around the main, sub-magnetic paths of different forms and constructions of the Tran-generators. The invention when combined with any one of recovering the utilized electric charge, using the (hybrid) soft magnetic wires, applying the Voltage-Doubler circuits, and using the transfer of high-potential electric charge to generate more electric energy, make the tran-generators useful.

A time-varying current from a DC voltage-source, flows through a primary winding of a magnetic circuit containing permanent magnets, induces more inductive voltages across different windings. The windings are wrapped around the main, sub-magnetic paths of different forms and constructions of the Tran-generators. The invention when combined with any one of recovering the utilized electric charge, using the (hybrid) soft magnetic wires, applying the Voltage-Doubler circuits, and using the transfer of high-potential electric charge to generate more electric energy, make the tran-generators useful.