Patents Examined by Tyrone Davis
  • Patent number: 4450544
    Abstract: The acoustical energy absorbing baffle has a pair of restricted orifice screens rigidly secured in parallel, spaced relation by a lattice stiffener. The screen-stiffener assembly is immersed in a viscous fluid contained within a tank sealed with an elastic diaphragm. Incident acoustical energy is transmitted through the diaphragm and translated into energy absorbing motion of the fluid through the restrictive screens. A compliant mass is acoustically coupled to the fluid to augment fluid particle velocity through the screens and to further absorb energy.
    Type: Grant
    Filed: November 16, 1981
    Date of Patent: May 22, 1984
    Assignee: Sperry Corporation
    Inventors: Alfred Denaro, George Rand
  • Patent number: 4449211
    Abstract: A plurality of transducers, closely conforming to the surface of a low-drag ose, are baffle mounted in close pack configurations to eliminate grating lobes. The baffle assembly is mounted outside a pressure hull within a thin acoustically transparent fairing. A plurality of pressure compensators also attach outside the pressure hull. The cavity between pressure hull and fairing is filled with pressure compensating acoustic fluid. Larger portions of unused volume are first filled with a syntactic foam to minimize the amount of fluid required. The pressure compensators balance fluid pressure against external sea pressure to prevent fairing collapse. This array maximizes available nearby internal nose volume thus allowing beamforming electronics to be located within the pressure hull in close proximity to the array elements, connecting thereto via a plurality of short coaxial cables.
    Type: Grant
    Filed: July 6, 1982
    Date of Patent: May 15, 1984
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Richard L. Schmidt, Edmund J. Sullivan, Bernard J. Myers, Edward G. Liszka
  • Patent number: 4449210
    Abstract: Apparatus is provided including a light source, a transducer and a detector, which is capable of detecting applied acoustic signals. The transducer employs first and second ridged members which have parallel rippled surfaces which contact opposite sides of a fiber optic waveguide. Each rippled surface has a different predetermined ripple pitch which provides for variable sensitivity along one dimension of the transducer. Modulation of the position of the ridged members relative to one another by means of applied acoustic signals causes microbend attenuation of light transmitted through the waveguide. The modulation of the light provides an indication of the presence of the acoustic signals. The variation in dimensional sensitivity provided by the transducer allows for a determination of the direction of arrival of the acoustic signals. Appropriate selection of pitch and pitch ratio of the two rippled surfaces provides any desired spatial sensitivity distribution of the hydrophone.
    Type: Grant
    Filed: December 21, 1981
    Date of Patent: May 15, 1984
    Assignee: Hughes Aircraft Company
    Inventor: Jon H. Myer
  • Patent number: 4446795
    Abstract: A metallic projectile body with a plastic rotating band comprising a band seat zone on such projectile body coated with a sprayed metallic coating, and a polymer molded over said sprayed metallic coating to form a plastic rotating band.
    Type: Grant
    Filed: December 31, 1981
    Date of Patent: May 8, 1984
    Assignee: Honeywell Inc.
    Inventors: Stephen J. Price, Charles R. Hargreaves
  • Patent number: 4445436
    Abstract: A projectile for a gun-vane centrifugal launching device is disclosed, of the type with an ogival head, a body and a tail of decreasing section. The body is cylindrical and the weight of the tail is chosen in such a way that the center of gravity of the projectile lays in the plane where the body joins the tail or in the immediate vicinity of this plane. The shape of the said tail is such that no point of the surface of the latter touches the wall of the gun-vane, particularly during the ejection of the projectile.
    Type: Grant
    Filed: November 30, 1981
    Date of Patent: May 1, 1984
    Inventor: Leon L. Rutten
  • Patent number: 4444119
    Abstract: An impulse generator for providing an impulsive force substantially normal o the axis of a missile to provide the missile with the desired angle of attack. The device includes radial explosive paths to its periphery and from each point on the periphery detonation is transferred to the periphery of the main charge causing it to implode.
    Type: Grant
    Filed: July 2, 1982
    Date of Patent: April 24, 1984
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventor: Elso R. Caponi
  • Patent number: 4441429
    Abstract: A retainer for attaching a rotating band to a projectile during handling ramming of the projectile. The retainer cooperates with a groove on the projectile and is discarded during firing of the projectile by the force of the charge. An interlocking double split ring forms the retainer with an outer ring having an L-shaped cross-section and an inner ring shaped to fit into the L-shape of the outer ring. Each ring is provided with a split or opening to allow for expansion of the ring over the projectile and into the projectile groove. The outer ring split may be cut at an angle of less than 90.degree. to minimize deflection of the outer ring. The inner and outer rings are assembled with their splits together and then clocked 180.degree. apart. The inner ring is then locked to the outer ring by a locking notch. Hoop stress of the outer ring prevents the inner ring from deflecting at the split such that the retainer is forced to behave as a continuous single ring.
    Type: Grant
    Filed: December 23, 1981
    Date of Patent: April 10, 1984
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Abner B. Price, William S. Burnley, III
  • Patent number: 4434718
    Abstract: A discarding sabot projectile for shotgun of unique construction whereby the separation of the projectile and sabot is enhanced by opposing air pressure and the unique construction of the sabot. The sabot as utilized herein comprises a plastic body firmly encompassing, but not completely encapsulating a subcaliber projectile. The plastic body includes a plurality of longitudinally extending slots forming symmetrical segments and further, segment having longitudinally extending grooves for reducing friction between the barrel bore and the sabot. The segments are further defined at the other end thereof by longitudinal tapered edges. The sabot, upon exiting the launching device begins to separate from the enclosed projectile beginning at the uppermost front end of the sabot as a result of air pressure flowing in the opposite direction of the sabot.
    Type: Grant
    Filed: September 11, 1981
    Date of Patent: March 6, 1984
    Inventors: Paul J. Kopsch, Donald F. Ward, Jay Graber, Omer Nichols
  • Patent number: 4430943
    Abstract: A fin-stabilized projectile having a sabot which forms a practice projectile with a sub-caliber projectile including a sabot whose base includes a passageway for propellant charge gases and a projectile component which is displaceable by the gases.
    Type: Grant
    Filed: July 24, 1981
    Date of Patent: February 14, 1984
    Assignee: Diehl GmbH & Co.
    Inventors: Erich Bock, Wolfgang Mosig
  • Patent number: 4432080
    Abstract: A compact subwavelength size monopole underwater sound radiator has chararistics to maximize resistive radiation impedance, minimize reactive radiation impedance, facilitate heat dissipation and minimize compensating air usage. This results in improved efficiency, bandwidth and use factor. The underwater sound radiator uses two back-to-back mounted, frustum shaped, hollow, radiating shells to achieve radiation characteristics approximating those of an equivalent sized pulsating sphere. An elliptically shaped, uniform cross-section magnetostrictive ring crossed by a linear piezoelectric spreader comprises a compact eclectic driver. Both the magnetostrictive ring and the piezoelectric stack contribute to the output through inverse phase cyclic changes in their respective lengths those changes being added and amplified by the flexural-bow type action of the elliptically shaped magnetostrictive ring.
    Type: Grant
    Filed: October 1, 1981
    Date of Patent: February 14, 1984
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: William F. Wardle
  • Patent number: 4430942
    Abstract: An improved missile/canister support pad control system wherein rods having a flexible curved section are interconnected to the support pads and are detachably held parallel to the missile by releasing means. Upon command, after the missile leaves the canister, the releasing means allows the rods to spring away from the missile. The resultant wind in combination with the spring rods lifts and rotates the system away from the missile so as not to recontact the missile surface.
    Type: Grant
    Filed: November 5, 1981
    Date of Patent: February 14, 1984
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Roy J. Heyman
  • Patent number: 4428294
    Abstract: A finless non-spinning round is able to maintain range accuracy and reduced un tube wear by the use of a single base cool burning propellant, an improved shape wear liner, and a warhead projectile configured to position the center of gravity of the warhead so that it is equal to or greater than 0.5 calibers forward of the warhead's aerodynamic center of pressure.
    Type: Grant
    Filed: August 16, 1982
    Date of Patent: January 31, 1984
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventors: Edmund W. Falkowski, Michael J. Kolasa
  • Patent number: 4421033
    Abstract: Exercise projectile substantially of a configuration defined by a pointed head prolonged by a tail-piece, characterized in that the projectile contains at least one explosive charge and an associated device for delayed firing, the duration of the delay substantially corresponding to the statistical flight time of the projectile from its starting time to the end of its intended useful trajectory.
    Type: Grant
    Filed: August 31, 1981
    Date of Patent: December 20, 1983
    Assignee: s.a. PRB, societe anonyme
    Inventor: Gerard E. Dupont