Patents Represented by Attorney W. T. Skeer
  • Patent number: 4603422
    Abstract: A method of obtaining a long-lived flashpumped laser dye with an output equivalent to commercial dyes and a low threshold of lasing using the N-methyl tosylate salt of 2-(4-pyridyl)-5-(4-methoxyphenyl) oxazole.
    Type: Grant
    Filed: September 26, 1984
    Date of Patent: July 29, 1986
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Aaron N. Fletcher
  • Patent number: 4448373
    Abstract: An elastomeric sway bracing and ejector system for aircraft is provided by wo different apparatus. In one, an elastomeric cushion is placed on the aircraft in a position to be crushed by a carried aircraft store. In the other, an elastomeric bladder is filled with gas, which is compressed to the sway brace store. This acts as a cushion between the aircraft and the store. In both apparatus, the release of the store permits it to be ejected by the compressed force of the elastomeric material. Insertion of pressurized sections in the elastomeric cushion permit both the cushion and the bladder to be inflated by different air pressures to control the resilient force exerted against the store.
    Type: Grant
    Filed: December 15, 1980
    Date of Patent: May 15, 1984
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Jack R. Bates, John W. Holtrop
  • Patent number: 4418610
    Abstract: An electrohydraulic control system with mechanical position sensing feedb is presented. A movable flight control canard is rotatably operated for providing flight control of the missile. A hydraulically powered actuator is mounted to the airframe with the canard being secured to the actuator shaft for controlled rotation of the canard. Hydraulic fluid under pressure enters the actuator at its base controlled via a rotary valve. A stepper motor is mounted to the canard and is geared to drive the rotary valve as determined by digital control signals generated by the missile guidance computer. When the stepper motor receives a train of pulses, the stepper motor rotor rotatingly moves the rotary valve from the null or closed position to an open position admitting hydraulic fluid into the rotary actuator causing the canard to turn.
    Type: Grant
    Filed: September 8, 1980
    Date of Patent: December 6, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: John W. Holtrop
  • Patent number: 4408334
    Abstract: Thermally induced stress birefringence in laser resonators is eliminated by inserting a waveplate in the resonating cavity. The waveplate is chosen by matching its polarization transmission matrix to the polarization transmission matrices of the laser rod and a Porro prism used as an end reflector in the resonating cavity. This produces a total polarization transmission matrix in the resonating cavity which is independent of ray coordinates. Additional control of the polarization transmission matrix is provided using a Porro prism as a cavity reflector that has an antireflection coating on its roof to change the required phase advance angle of the waveplate.
    Type: Grant
    Filed: March 13, 1981
    Date of Patent: October 4, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Eric A. Lundstrom
  • Patent number: 4402775
    Abstract: A hybrid gun propellant containing an oxidizer rich liquid monopropellant d an oxidizer deficient single based solid propellant.
    Type: Grant
    Filed: June 24, 1982
    Date of Patent: September 6, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Stanley E. Wood
  • Patent number: 4398978
    Abstract: A method for preparation of high density, high energy, low viscosity liquid ydrocarbon fuel by catalytic treatment of tetrahydrodimethyldicyclopentadiene (RJ-4) synthetic fuel. Endo-isomers within the fuel stock are isomerized to exo-isomers by treatment of the fuel stock with catalysts such as aluminum chloride, nickel, or pulverized, acid treated firebrick resulting in a fuel having a lower viscosity than the original RJ-4.
    Type: Grant
    Filed: April 26, 1982
    Date of Patent: August 16, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: George W. Burdette, Abraham I. Schneider
  • Patent number: 4395001
    Abstract: A line cutter or discharge valve responsive to aircraft attitude is posited on an aircraft ejection seat to interrupt the gas initiated sustainer rocket system. During inverted ejections, the cutter or valve will either sever or discharge pressure from a tube which leads from the firing squib to the sustainer rocket. Preventing sustainer rocket ignition enhances inverted ejection survivability by reducing crew member velocity toward the ground, thereby lengthening the time available for parachute deployment.
    Type: Grant
    Filed: March 27, 1978
    Date of Patent: July 26, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: W. James Stone, Vernon D. Burklund, Robert B. Dillinger, Dennis M. Sorges, David A. Reeve
  • Patent number: 4392895
    Abstract: A solid ramjet fuel composition comprising a hydroxyl-terminated or carbo-terminated fluorocarbon binder, a polybutadiene prepolymer, a curative cross-linking compound, and a metal selected from the group consisting of aluminum, zirconium, amorphous boron or magnesium.
    Type: Grant
    Filed: November 9, 1981
    Date of Patent: July 12, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Russell Reed, Jr., George W. Burdette, Gary W. Meyers, William R. Vuono
  • Patent number: 4391515
    Abstract: Optical detection apparatus is provided which includes a coherent light sce for generating a beam of coherent light. The apparatus further includes a unitized or discrete optical component which receives the generated beam, and projects light thereof which has a particular polarization characteristic into a specified environment. The optical component also functions to receive or absorb light from the environment which has the particular polarization characteristic, and to directably reflect light from the environment which does not have the polarization characteristic. A lens or other light collecting device focuses light reflected by the discrete optical component upon a light detection element. A light conducting path is provided between the coherent light source and the light detecting element to enable generated coherent light to be mixed with the reflected light upon the light detecting element to provide data signals which indicate the presence of an object in the environment.
    Type: Grant
    Filed: May 7, 1981
    Date of Patent: July 5, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Howard M. Forrester, John R. Crisler
  • Patent number: 4380634
    Abstract: A laser dye, 2-keto-4,6,8,8-tetramethyl-8,9-dihydro-2H-pyrano(3,2-g) quinoline, is prepared by mixing m-aminophenol and ethyl acetoacetate and heating the mixture.
    Type: Grant
    Filed: October 5, 1981
    Date of Patent: April 19, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Ronald L. Atkins
  • Patent number: 4375522
    Abstract: A solid propellant restrictor for preventing erosive burning in solid prolant grain critical areas is described. The restrictor is a mixture of hydroxyl-terminated polybutadiene with 1% by weight of dissolved 2,2'-methylene-bis(4-methyl-6-tert-butyl) phenol, dioctyl adipate, triethanolamine, ferric acetylacetonate, carbon black, aluminum oxide, silicon oxide, and toluene diisocyanate, curing at room temperature and illustrates superior hardening, adhesive, and application properties.
    Type: Grant
    Filed: July 21, 1980
    Date of Patent: March 1, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: John D. Braun
  • Patent number: 4375192
    Abstract: A programmable fuze for initiating weapon warhead detonation. The deacceltion of the weapon warhead is measured by an accelerometer. The output of the accelerometer is integrated to obtain velocity and subsequently digitized and stored in a microcomputer or microprocessor. A zero-slope detector indicates to the microcomputer or microprocessor if the forward velocity component is constant for a given time. This indicates whether the weapon warhead has entered a cavity in the target. The microcomputer or microprocessor has an algorithm programmed into it so that it determines whether certain dynamic variables have exceeded threshold values thus initiating a detonating signal to a firing circuit. The dynamic variables are the distance of travel of the weapon warhead into the target, the deceleration level of the weapon warhead in the target, the transverse velocity component of the weapon warhead in the target, and the number of cavities entered.
    Type: Grant
    Filed: April 3, 1981
    Date of Patent: March 1, 1983
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Patrick A. Yates, Richard M. Swenson, George N. Hennings
  • Patent number: 4362583
    Abstract: A new azido compound 1,9-diazido-2,4,6,8-tetranitro-2,4,6,8-tetrazanonane is disclosed, and a method of preparation is disclosed wherein 1,9-dichloro-2,4,6,8-tetranitro-2,4,6,8-tetrazanonane or 1,9-dinitroxy-2,4,6,8-tetranitro-2,4,6,8-tetrazanonane is reacted with sodium azide and dimethylformamide. This new azido compound is useful as an explosive, propellant, or component thereof to modify properties.
    Type: Grant
    Filed: April 21, 1981
    Date of Patent: December 7, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Ronald A. Henry, William P. Norris
  • Patent number: 4360816
    Abstract: A direction finding antenna for accurate direction finding over broad conuous frequency spectrums, independently of polarization, comprising a phased array of six log-periodic dipole antennas with loaded elements.
    Type: Grant
    Filed: July 21, 1971
    Date of Patent: November 23, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Robert G. Corzine
  • Patent number: 4358327
    Abstract: A gas generant propellant composition having low flame temperatures comprng (a) an elastomeric binder consisting of a mixture of polyethylene capped polypropylene glycol and a dihydroxy tetrazole selected from the group having the formulas: ##STR1## (b) a curative agent such as the biuret trimer of hexamethylene diisocyanate; (c) a plasticizer agent such as 1-methyl-5 (methoxyethyl) tetrazole; (d) a coolant agent such as oxamide; and (e) a deflagrating agent selected from the group consisting of: dihydrazinium 3,6-bis(5-tetrazolyl)-1,2-dihydrotetrazine, dinitrosopentamethylenetetramine, the reaction product of glyoxal and hydrazine and the ammonium salt of 5-nitramino tetrazole.
    Type: Grant
    Filed: October 14, 1980
    Date of Patent: November 9, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Russell Reed, Jr., Benjamin Y. S. Lee, Ronald A. Henry
  • Patent number: 4357856
    Abstract: A mixture of aqueous nitric acid (about 90 volume percent HNO.sub.3 and 10 volume percent H.sub.2 O) and Decalin are used as a propellant for a liquid propellant gun.
    Type: Grant
    Filed: November 12, 1976
    Date of Patent: November 9, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Stanley E. Wood, James T. Bryant
  • Patent number: 4350959
    Abstract: A feedback signal amplifier circuit having switchable closed loop gain in sponse to the output signal level of the amplifier for limiting the output signal level is presented. The feedback ratio of the circuit is switched by output signal level responsive diodes which derive signal level determining bias from both an unregulated power supply and the output terminal of the amplifier. A bias compensation network deriving bias from the unregulated power supply is connected to a bias sensitive input of the amplifier for tracking changes in power supply voltage which are reflected into the output of the amplifier for keeping the signal level determining bias of the diodes essentially constant and independent of changes of power supply voltage.
    Type: Grant
    Filed: April 14, 1980
    Date of Patent: September 21, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Erik Rosenbaum
  • Patent number: 4350542
    Abstract: The present invention relates to an improved propellant or explosive and hod for making it having increased energy yet having increased toughness and hazard properties. More specifically, an HMX or RDX material is coated with a nitrocellulose, poly-hydroxyethyl acrylate or poly-hydroxymethyl acrylate for bonding hydroxyl groups that subsequently allows reaction with amine silane/s or a polymer of the type ##STR1## wherein n is an integer of 3 or 4, m is an integer of 2 or 3, and R is methyl or ethyl. Further coating of the product is then carried out with a primary hydroxyl forming material and then curing the product in the presence of an isocyanate.
    Type: Grant
    Filed: March 31, 1980
    Date of Patent: September 21, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: John F. Kincaid, Russell Reed, Jr.
  • Patent number: 4139897
    Abstract: Two dimensional optical or electrical images are processed through a storage tube designed to yield the correlation function between the input images and stored images. By generating a series of stored images representing sine and cosine components of the Fourier transform, a fast, two-dimensional transform of the image is obtained.
    Type: Grant
    Filed: March 18, 1977
    Date of Patent: February 13, 1979
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Keith L. Gardner, Henry N. Adaniya
  • Patent number: 4137966
    Abstract: An oven with temperature-independent sections permits objects placed within t to experience the uneven heating and temperature gradient problems associated with real life conditions. The number of sections can vary depending on the gradients desired.
    Type: Grant
    Filed: April 19, 1977
    Date of Patent: February 6, 1979
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Richard D. Ulrich, Crill Maples, Howard C. Schafer