Patents Assigned to Cerberus Institute for Research and Development, Inc.
  • Patent number: 7500433
    Abstract: A cartridge has a shell casing with a primer end and a projectile end. A projectile mounted in the projectile end is made of four segments held together by first and second retainer rings. In one form each segment contains shot. One form of the projectile has an air brake which is deployed as the projectile leaves the muzzle. The air brake is partially deployed or fully deployed, depending of the shredding of third and fourth retainer rings which hold the air brake. When the shredder is inserted in a barrel in a first position, the last horizontal retainer ring is shredded and the air brake is partially deployed. When the shredder blades are further positioned in the barrel, both retainer rings which hold the air brake are shredded and the air brake is fully deployed. Additional positions of the shredder ring first shred the second ring, releasing the segments, and then shred the first retainer ring, releasing the shot and other contents from the segments.
    Type: Grant
    Filed: June 2, 1995
    Date of Patent: March 10, 2009
    Assignee: Cerberus Institute for Research and Development (Inc.)
    Inventor: David Joel Forrester
  • Patent number: 7159823
    Abstract: A rapid deployment system has an inflatable landing tube with an inflatable exit slide coupled to an aircraft. Connectors couple the landing tube to the aircraft. Flexible retarders extend inward from the inner surface of the tube for retarding gravitational descent of cargo and/or personnel from the aircraft. The tube has tubular segments, with ribs and reinforcements, forming a continuous descent tube. A spine along the tube is retractable telescopically allowing for the tube to be retracted within the aircraft. The tube is connected to exterior edges of any exit port of the aircraft. A window coaming adapter is positioned around the exterior edges and a membrane extending between sides of the adapter expands with the landing tube as the landing tube is inflated. The membrane is of multiple layers with expansion cells between adjacent layers for allowing independent expansion of the layers. The entry port has a shield behind the membrane and connected to the aircraft for protecting the membrane.
    Type: Grant
    Filed: October 10, 2001
    Date of Patent: January 9, 2007
    Assignee: Cerberus Institute for Research and Development, Inc.
    Inventors: Paul W. Paustian, Jr., David J. Forrester
  • Patent number: 6111237
    Abstract: The present invention relates to an Atmospheric Energy Projection System for projecting electrical and thermal energy. The Microwave Facilitated Atmospheric Energy Projection System (MFAEPS) uses microwave energy at the resonant frequency or frequencies of oxygen and/or water to heat the atmosphere. This improves the potential conductivity of the air in the path of the microwave beam by heating the oxygen and water molecules in the air providing a favored pathway for breakdown. A voltage pulse generator discharges through an electrode positioned near the center of the microwave beam's recent path and creates an ionizing wave that follows the microwave beam's recent path. Alternatively, a laser can substitute for the electrode and project a high powered beam that is focused to create breakdown and thus create the ionizing pulse that travels down the favored pathway. The system can operate in an underwater environment operating at the resonant frequency of water.
    Type: Grant
    Filed: April 24, 1998
    Date of Patent: August 29, 2000
    Assignee: Cerberus Institute for Research and Development, Inc.
    Inventor: Philip J. Paustian
  • Patent number: 6054694
    Abstract: The Atmospheric Energy Projection System (AEPS) projects electrical/thermal energy using microwave radiation at the resonant frequency of oxygen. The radiation excites a column through the ambient atmosphere to a temperature such that air within the column is converted from an insulator to a conducting channel or focused medium. Electrical current is then applied to the channel to transmit an electric charge a predetermined distance. Rapid release of pulses of 60 GHz microwave radiation at a field strength below that for breakdown for the waveguide feeding the antenna or at the antenna aperture creates a channel without premature plasma generation. Once the channel is energized sufficiently, an electric charge is released into the channel and flows down it from the source to a solid the channel intersects. If no solid intrudes the charge diffuses harmlessly at the end of the heated channel as the channel cools back to the ambient temperature.
    Type: Grant
    Filed: April 16, 1997
    Date of Patent: April 25, 2000
    Assignee: Cerberus Institute for Research and Development, Inc.
    Inventor: Philip J. Paustian
  • Patent number: 5624592
    Abstract: The Atmospheric Energy Projection System (AEPS) is a means to project electrical/thermal energy using microwave radiation at the resonant frequency of oxygen. The radiation excites a column through the ambient atmosphere to a temperature such that air within the column is converted from an insulator to a conducting channel or focused medium. An electrical current is subsequently applied to the channel to transmit an electric charge a predetermined distance. Rapid release of pulses of 60 GHz microwave radiation at a field strength below that for breakdown for the waveguide feeding the antenna or at the antenna aperture creates a channel without premature plasma generation. Once the channel is energized sufficiently, an electric charge is released into the channel and flows down it from the source to whatever solid the channel intersects. If no solid intrudes the charge diffuses harmlessly at the end of the heated channel as the channel cools back to the ambient temperature.
    Type: Grant
    Filed: October 19, 1994
    Date of Patent: April 29, 1997
    Assignee: Cerberus Institute for Research and Development, Inc.
    Inventor: Philip J. Paustian
  • Patent number: 5620058
    Abstract: An emergency evacuation system uses three primary concepts--Retarded Free Fall, Temporary Structures and Energetics--to provide for rapid, safe rescue. An inflatable descent tube with entry ports is installed along the side of a structure or at the top of an elevator shaft. In emergency situations, a gas generator connected to the tube is activated and inflates the tube with gas. The interior surface of the tube includes energy absorption structures strategically positioned to retard the rate of fall. The structures absorb energy from falling bodies and translate some of the vertical force to horizontal force as the evacuee is temporarily deflected sideways in the tube. Friction strands cover the surfaces of the structures to further reduce velocities of falling evacuees. An inflatable exit ramp is positioned at the bottom of the tube to cushion the fall of the evacuee and lead the evacuee to safety.
    Type: Grant
    Filed: April 4, 1995
    Date of Patent: April 15, 1997
    Assignee: Cerberus Institute for Research and Development, Inc.
    Inventor: David J. Forrester
  • Patent number: 5479736
    Abstract: An augmented service pistol weapons system and ammunition has an extended barrel and an adapter sleeve and mount which supports the barrel and partially surrounds a forward end of the service pistol. Two hinged flaps have inward extending clamps which engage an inside of the front of a trigger guard on the pistol. A turn-to-release locking pin holds the two flaps together as the flaps are closed on the trigger guard. An arm rest extends laterally rearwardly along sides of the pistol and terminates in a curved rearward extension to support the augmented service pistol on an arm of the user. A fifty round magazine replaces the standard pistol handle magazine. Scopes and aiming devices are mounted above the extended barrel. A foregrip is removable and positionable at opposite lateral sides of the extended barrel and below the barrel. A variable power function assembly surrounds the barrel and allows selected release of gas to slow projectiles. A shredding device near the muzzle shreds bands on the projectile.
    Type: Grant
    Filed: January 6, 1994
    Date of Patent: January 2, 1996
    Assignee: Cerberus Institute for Research and Development, Inc.
    Inventor: David J. Forrester