Abstract: Apparatus for producing hydrogen gas comprise a container adapted to contain an aqueous electrolyte solution containing hydrogen, at least one first electrode, wherein the at least one first electrode is adapted to be in contact with a solution, at least one second electrode, wherein the at least one second electrode is adapted to be in contact with a solution, and wherein the at least one first electrode is a cylindrically-shaped cathode and the at least one second electrode is a cylindrically-shaped hollow anode capable of accommodating the cylindrically-shaped cathode within it, and wherein the cylindrically-shaped cathode is located along the central axis of the cylindrically-shaped hollow anode.

Abstract: Embodiments of the invention are directed to apparatus and methods for separating and extracting one or more desired elements and/or compounds from a source feedstock comprising the steps of providing a cavitation-assisted electrolytic purification apparatus comprising an electrolyte and a source feedstock in a reaction zone; introducing oxidizing agents and reducing agents to the source feedstock; causing an electric current to flow through the reaction zone; causing cavitation within the reaction zone; and optionally modifying the temperature of the reaction zone.

Abstract: A digital airborne situational awareness system and method. The system is installed on multiple aircraft to generate an airborne network providing collision avoidance without ground control. A global positioning system (GPS) receiver unit is coupled to a microprocessor in each aircraft equipped with the system. A software engine receives the raw GPS data and determines location, speed, flight path direction, and altitude. The software engine conditions the GPS data for display on a cockpit display panel. The conditioned data orients the display with the heading, speed, and altitude data of the host system aircraft. A transceiver section provides data transmission to other airborne receiving units within the approximately forty mile range of the airborne network. The transceiver transmits data packets including reconditioned location (track), altitude, and an aircraft class identifier to other aircraft in the network.