Other

Joseph John Wagner

Karl F Milde, Jr

Anthony Stanley Pruszenski, Jr

Richard Keith Roese

A Voice over Internet Protocol (VoIP) targeted advertisement delivery method that is operable in a processor coupled to a memory. The method includes monitoring all outgoing communications on a server in order to identify a VoIP telephony signal. Upon detection of a VoIP telephony signal indicating that a VoIP call setup is in progress, the method determines whether a caller identifier associated with the VoIP telephony signal identifies an associated caller as a candidate for a targeted advertisement delivery. If the caller is a candidate for a targeted advertisement delivery, identifying and retrieving a targeted advertisement for presentation to the caller during the call setup.

System and method for directing targeted advertisements in IP telecommunications

An apparatus and method for coating an end of a stoppered beverage bottle in wax are provided. A cap assembly is positioned over a mouth of the bottle prior to coating the end of the bottle in wax. The cap assembly may facilitate removal of a portion of the wax from the bottle to allow removal of the stopper and dispensing of the beverage. In an implementation, the cap assembly includes a cap portion sized to be received over at least a portion of a bottle mouth and the stopper. A spike protrudes downwardly from the cap portion, and is configured to at least partially pierce a bottle stopper. A tear ring is frangibly attached to the cap portion by one or more regions of mechanical weakening. A pull tab extends outwardly from the tear ring to facilitate frangible separation of the tear ring from the cap portion.

Cap and tear ring for beverage bottle

A personal aircraft (PAC) capable of vertical take-off and landing (VTOL) comprises a fixed wing and a fuselage with a passenger compartment having a front, a rear and two sides, and a plurality of independently powered thrusters, preferably integrated into the wing, on each side of the fuselage. The aircraft has a lift to drag ratio equal to or greater than 2. The thrusters, which are ducted fan units capable of providing a vertically upward force to the aircraft, are provided with such redundancy that the aircraft can hover with at one thruster inoperative on each side of the fuselage. At least one thruster on each side of the fuselage preferably comprises a 'levitator' which creates lift from the airfoil-like air inlet as well as from the acceleration of air from inlet to outlet.

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St. Helena, CA, United States of America

Joseph John Wagner