Abstract: A fuel less pneumatic and hydraulic lift system flight system provides the following systemic components. A chassis supporting an electric battery and a pressurized base hydraulic cylinder, a hydraulic fluid pumping assembly fluidly coupled to the pressurized base hydraulic cylinder; a lift mechanism assembly providing an attractive levitation plate mounted to the chassis; and a repulsive levitation plate mounted to a carriage, wherein the repulsive levitation plate is disposed in a magnetic pole repulsive alignment relative to the attractive levitation plate causing a magnetic lift effect to the chassis; and a plurality of propulsions jets mounted to the chassis, wherein the plurality of propulsion jets enabling motive functionality using hydraulic fluid propulsion and pneumatic pressure via the hydraulic fluid pumping assembly in conjunction with the magnetic lift effect.

Abstract: An aerial craft and sealed force vectoring flight system is disclosed. The aerial craft includes a main body hull, lift jets, a generator, an electrical re-introduction circuit, a hydraulic pump, air flow compressors, an RPM sensor, a max speed limiter hydraulic draft by-pass valve, and a battery. The electrical re-introduction circuit throttles the generator into high-velocity rotation and yields excess electrical current to then be applied to the lift jets. The hydraulic pump pulls pressurized hydraulic fluid across a preceding hydraulic drive impellor such that the pressurized hydraulic fluid returns to confinement under pneumatic pressure faster than a discharge of hydraulic fluid. The air flow compressors generate electricity that is re-introduced into the lift electric motors. The RPM sensor and max speed limiter hydraulic draft by-pass valve speed regulate the generator. The battery initially powers the generator.

Abstract: An electric vehicle activation system provides at least one hand-manipulated lever pneumatically associated with a permanent magnet magneto generator for generating a start current electrically coupled to a generator system of the electric vehicle. The manipulation of each hand-manipulated lever enables air pressure to activate a pneumatic impeller causing a hydraulic draft cycle configured to generate the start current.

Abstract: A geomagnetic field amplifier device, system, and method is provided. The invention includes geosynchronously orbiting one or more satellites about a first magnetic pole of the planet; and transmitting, from each said satellite, a first mono-polarity magnetic field at the first magnetic pole, wherein the first mono-polarity magnetic field and first magnetic pole correspond in polarity.

Abstract: A fuel less pneumatic and hydraulic lift system flight system provides the following systemic components. A chassis supporting an electric battery and a pressurized base hydraulic cylinder, a hydraulic fluid pumping assembly fluidly coupled to the pressurized base hydraulic cylinder; a lift mechanism assembly providing an attractive levitation plate mounted to the chassis; and a repulsive levitation plate mounted to a carriage, wherein the repulsive levitation plate is disposed in a magnetic pole repulsive alignment relative to the attractive levitation plate causing a magnetic lift effect to the chassis; and a plurality of propulsions jets mounted to the chassis, wherein the plurality of propulsion jets enabling motive functionality using hydraulic fluid propulsion and pneumatic pressure via the hydraulic fluid pumping assembly in conjunction with the magnetic lift effect.

Abstract: An aerial craft and sealed force vectoring flight system is disclosed. The aerial craft includes a main body hull, lift jets, a generator, an electrical re-introduction circuit, a hydraulic pump, air flow compressors, an RPM sensor, a max speed limiter hydraulic draft by-pass valve, and a battery. The electrical re-introduction circuit throttles the generator into high-velocity rotation and yields excess electrical current to then be applied to the lift jets. The hydraulic pump pulls pressurized hydraulic fluid across a preceding hydraulic drive impellor such that the pressurized hydraulic fluid returns to confinement under pneumatic pressure faster than a discharge of hydraulic fluid. The air flow compressors generate electricity that is re-introduced into the lift electric motors. The RPM sensor and max speed limiter hydraulic draft by-pass valve speed regulate the generator. The battery initially powers the generator.

Abstract: This invention is directed toward an exercise band that is circular in shape, defining a central cavity with a diameter sufficient to allow average people to insert their legs into the cavity, and push in an outward direction to exercise the gluteus muscle groups. The exercise band has an inner core of a resiliently stretchable material, and an outer cover made from a material that is easily washed, to remove the sweat of the user. The connection of the two ends of the invention is accomplished through a three-fold sew-based connection. The band provides a simple, small, easily transported and stored exercise device for standing, sitting, squatting and prone exercises. Several of these bands, each with a different degree of resistance, can be combined in a set, allowing people to “work up” to ever-increasingly more resistant bands without having to adapt to a new shape of band.

Abstract: Systems and methods are provided for processing refinery residuals. In one embodiment, the system may include a gasifier configured to produce syngas from refinery residuals. A gas turbine engine may produce power from the syngas, and the power may be provided to a desalination system. A portion of the syngas may be provided to a shift reactor.