Marine Type Patents (Class 102/390)
  • Patent number: 10408586
    Abstract: A non-lethal projectile comprises a carrier with a deployable payload to allow for effective performance at both long and short ranges. The non-lethal projectile is fired from a launcher. At a predetermined range, the carrier opens thereby deploying the payload. The payload may further comprise a drogue chute to reduce the kinetic energy of the payload to a non-lethal level. Alternatively, the inherent drag coefficient of the payload may enable sufficient reduction of kinetic energy without the need for a drogue chute. The deployed petals of the carrier serve as drag surfaces for the carrier, thereby reducing the kinetic energy of the carrier to a non-lethal level.
    Type: Grant
    Filed: September 28, 2017
    Date of Patent: September 10, 2019
    Assignee: The United States of America as Represented by the Secretary of the Army
    Inventor: Mario E. DeAngelis
  • Patent number: 8222583
    Abstract: A drag-stabilized water-entry projectile having a projectile body, one or more drag-stabilizing elements, such as fins, flares or canards, and one or more attachment members adapted to hold the one or more drag-stabilizing elements to the projectile body. The one or more attachment members are coated with a thermally reactive material. A projectile and cartridge assembly has a shear pin, a projectile having a first cutout portion, the cutout portion sized to receive the shear pin. The assembly also includes a sabot configured to house the projectile and having a second cutout portion, the second cutout portion sized to receive the shear pin. The cutout portion is positioned to provide an offset region between an aft end of the projectile and a base of the sabot.
    Type: Grant
    Filed: March 23, 2009
    Date of Patent: July 17, 2012
    Assignee: Lockheed Martin Corporation
    Inventors: Jyun-Horng Fu, Antonio Paulic
  • Publication number: 20120152143
    Abstract: An artificial tsunami is a new type of beaching tactic capable of achieving the military goal with almost no losses among the invading forces.
    Type: Application
    Filed: January 30, 2011
    Publication date: June 21, 2012
    Inventor: Ching-Min Huang
  • Patent number: 8093487
    Abstract: A removable protective nose cover for a submersible structure having a nose section is disclosed. The removable protective nose cover can include a plurality of shell members, each of the shell members having a forward end and an aft end. Each shell member can also be dimensioned to fit adjacent to and around the nose section of the submersible structure and thereby form a protective shell. A central nose member having a locking member can also be included, the locking member being operable to attach the central nose member to each of the forward ends of the shell members. The aft ends of the shell members can be attached to each other using a plurality of attachment clips such that the attachment of the central nose member to each of the forward ends of the shell members and the attachment of the adjacent aft ends of the shell members form the removable protective nose cover for the submersible structure.
    Type: Grant
    Filed: January 28, 2009
    Date of Patent: January 10, 2012
    Assignee: The Penn State Research Foundation
    Inventor: Neil B. Kimerer, Jr.
  • Patent number: 6802260
    Abstract: A safety and arming device has first and second portions of an explosive train fixably supported in a housing. A third portion of the explosive train is fixable in a first position such that the first and second portions remain operably separated from one another, and is further movable to a second position such that the first and second portions are operably coupled to one another via the third portion. An integrated water sensor/actuator is coupled to the third portion to provide the motive force that moves the third portion to its second position. The water sensor/actuator is based on a fibrous cellulosic material having anisotropic moisture-absorbing properties such that dried-in strain of the cellulosic material is greatest along one axis thereof. In the invention, a plug of the dry and compressed fibrous cellulosic material has a powder material coated thereon and mixed therewith.
    Type: Grant
    Filed: April 30, 2001
    Date of Patent: October 12, 2004
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Robert Woodall, Felipe Garcia, Chris Doyle
  • Patent number: 5955698
    Abstract: A supercavitating water-entry projectile having empennage on the aft end ch provides both aerodynamic and hydrodynamic stability and a supercavitating nose section is provided. A representative projectile is a subcaliber munition adapted for use in a 25 mm weapon using a sabot currently in use with the M919 round. The projectile has circumferential grooves around its center section to match these sabots. A key feature in the invention is the size and shape of the nose section. The projectile has a novel high strength extended blunt nose section followed by a truncated conical section which angles towards the body of the projectile in the range of five degrees. During underwater trajectory, the entire projectile is contained within the cavitation bubble formed by the blunt nose tip. The projectile's aft empennage, which provides both aerodynamic and hydrodynamic stability, fits within the bore of the weapon.
    Type: Grant
    Filed: January 28, 1998
    Date of Patent: September 21, 1999
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Thomas K. Harkins, Howard K. Steves, Jacques E. Goeller
  • Patent number: 4788914
    Abstract: A nosepiece for the forward end of a missile that is launched into the atmosphere for a ballistic trajectory and a water entry impact comprises a frangible base and a separable nosecap, the base having multiple segments of rigid foam defining an axial bore into the base and a volume of soft cellular foam within the bore to protect the forward end of the missile. The nosecap is in seated relationship within the bore opening on the tip end of the base during airborne flight and separates therefrom to expose the axial bore opening prior to water entry impact such that upon impact the base is fractured by the force of water entering the exposed bore and thus separated from the missile.
    Type: Grant
    Filed: February 8, 1988
    Date of Patent: December 6, 1988
    Assignee: Loral Corporation
    Inventor: James T. Frater
  • Patent number: 4478148
    Abstract: An underwater communication system capable of being delivered by a missile or detonating a plurality of charges in a timed sequence. The system includes a main power supply, decelerometer means, separation switch means for electrically interconnecting and energizing the decelerometer means and said main power supply upon receipt of an arming signal from the missile, thermal battery means, means coupled to said decelerometer means for deploying a parachute and for energizing the thermal battery means, timer means for releasing the explosive charges in a predetermined sequence and means couples to the thermal battery means for energizing the timer means.
    Type: Grant
    Filed: December 30, 1963
    Date of Patent: October 23, 1984
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Albert Applebaum, Albert S. Will, Samuel A. Humphrey, Frank C. McLean, Sylvan Wolf, Carl R. Peterson, Harry J. Gauzza, John C. Hetzler
  • Patent number: 4433626
    Abstract: An underwater missile for use against submerged submarines has a missile housing with a magnetic contact surface (2) at a foremost end portion intended to contact a submerged submarine. The magnetic contact surface is provided by two magnets (2',2") located in adjacency and with reversed magnetic polarity. A magnetically operated switching means (5) is positioned adjacent to the magnetic leakage field of the magnets, and is arranged to be operated when the leakage field is increased by means of a metallic object located within the magnetic field of the magnets. The operation of the switching means first detonates a small propellant charge (6) to impose a force to cause complete adherence between the magnetic contact surface of the missile and the outer surface of a contacted submarine, and then detonates a main explosive charge (7) intended to penetrate the submarine.
    Type: Grant
    Filed: October 13, 1981
    Date of Patent: February 28, 1984
    Inventor: Sven Landstr/o/ m