Patents Represented by Attorney W. Thom Skeer
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Patent number: 6914556Abstract: A pulsed magnetron is caused to emit a series of RF energy pulses which are phase coherent with an injection signal by supplying the magnetron with a pedestal pulse during low-power signal injection. The pedestal being of a magnitude and duration such that the slow-rise-time pedestal portion holds the magnetron in the Hartree region during the signal injection.Type: GrantFiled: May 31, 1977Date of Patent: July 5, 2005Assignee: The United States of America as represented by the Secretary of the NavyInventor: Reuben E. Nyswander
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Patent number: 6753802Abstract: An electronic circuit for use in an anti-radiation missile system of the type which uses the electromagnetic transmissions of a target radar for guidance information, detects when the missile has flown into a target null and is no longer receiving energy from one of the main lobes or side lobes of the target radar transmitter. When this condition is detected, the circuit causes an attenuation in the epsilon error guidance signal to momentarily prevent guidance commands based upon the now suspect epsilon error signals from being implemented.Type: GrantFiled: October 29, 1985Date of Patent: June 22, 2004Assignee: The United States of America as represented by the Secretary of the NavyInventors: Bruce M. Heydlauff, Ralph K. Beyer
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Patent number: 4755829Abstract: An antenna array for combining in space microwave energy from a number of cillators, such as IMPATT diodes, which are controllable by injection locking. The array has elements individually driven by the oscillators, but an injection locking signal is provided in the usual manner only to the oscillator of a central element. The other oscillator are injection locked through mutual coupling between the central element and the other elements so that coherent radiation is output by the array. The radiation may be steered by phase shifters between the elements and their oscillators.Type: GrantFiled: February 20, 1987Date of Patent: July 5, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventors: Robert J. Dinger, David J. White, Donald R. Bowling
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Patent number: 4754040Abstract: A method of preparing 4,6-dinitro-5,7-diaminobenzofuroxan from 4,6-dichloenzofuroxan.Type: GrantFiled: February 25, 1985Date of Patent: June 28, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventors: Andrew P. Chafin, Ronald L. Atkins
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Patent number: 4747673Abstract: An attenuator for high power laser beams, the attenuator has an annular b dump through which the beam passes diametrically and in which the beam passes successively through a pair of pivoting transmissive and reflective element. These elements are individually mounted on intermeshed gears so that the elements are adjustable through equal and opposite angles. At each element a portion of the beam is reflected toward the dump and a portion transmitted, the relative energy in each portion being determined by the angle of the elements to the beam so that adjustment of this angle determines the amount of attenuation. The beam is offset oppositely by refraction at each element so that the attenuator does not change the beam path. The elements are, preferably, elements commonly used as edge filters, that is, interference filters having an abrupt monotonic transition with wavelength from reflection to transmission.Type: GrantFiled: June 1, 1987Date of Patent: May 31, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventors: C. Denton Marrs, William N. Faith
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Patent number: H2069Abstract: A signal processor circuit has a phase-locked loop with a low-pass filter for removing phase-modulation components from a clock signal. The processor circuit has an isolated power supply for removing amplitude-modulation components from the same clock signal.Type: GrantFiled: December 21, 1984Date of Patent: July 1, 2003Assignee: The United States of America as represented by the Secretary of the NavyInventors: James L. Rieger, Paul H. Woodworth
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Patent number: H2076Abstract: An analog video processor is disclosed for coupling a CCD target acquisition and tracking seeker to a microcomputer via a video preprocessor, having a CCD automatic light control circuit, a video automatic gain control circuit, and a TV monitor/display circuit, and via a video processor, having a target acquisition mode gradient processor circuit, to detect target edge sharpness, a target tracking mode contrast processor circuit to detect targets via video amplitude, and an output control circuit, to convert analog and asynchronous target signatures to synchronous target edges for input to the microcomputer.Type: GrantFiled: January 27, 1986Date of Patent: August 5, 2003Assignee: The United States of America as represented by the Secretary of the NavyInventors: Greg A. Watson, Richard C. St. Clair, Steven C. Tenbrink
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Patent number: H476Abstract: The compound 7-amino-4,6-dinitrobenzofuroxan is synthesized by stirring monochloro-4,6-dinitrobenzofuroxan in CH.sub.2 Cl.sub.2 under an ammonia atmosphere. The position of the amino group is proved by reduction with triphenylphosphine to give 7-amino-4,6-dinitrobenzofurazan, a known compound.Type: GrantFiled: April 22, 1985Date of Patent: June 7, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventor: William P. Norris
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Patent number: H483Abstract: A binary solvent for liquid dye laser systems comprising a surfactant having a hydrophobic end and a hydrophilic end in a viscous polar solvent provides a method of improving the output, efficiency and lifetime of laser dyes, particularly in non-flowing liquid dye laser systems.Type: GrantFiled: April 3, 1987Date of Patent: June 7, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventors: Mark B. Moran, C. Denton Marrs
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Patent number: H492Abstract: A safe/arm device has a rotor that aligns or misaligns a path for an explve. The rotor is aligned by the effects of a fluid pressure differential acting upon a piston of the device. This pressure differential causes the piston to translationally move and this movement is transmitted to the rotor by a shaft. The shaft fits within an axial bore defined by the rotor. This axial bore in turn defines a helical groove. A ball, partially recessed within a well defined by the shaft, rides within this helical groove. As the shaft is translationally driven within the axial bore, the helical groove of the rotor tracks the ball. Translational movement of the shaft is thereby converted to rotational movement of the rotor. As a safeguard, the shaft is split into two sections, one in engagement with the piston and the other in engagement with the rotor. By this arrangement, a predetermined amount of movement of the piston is required before this movement is transmitted to the rotor.Type: GrantFiled: January 15, 1988Date of Patent: July 5, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventors: Jerome A. Kong, David L. Riggs
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Patent number: H503Abstract: A method of obtaining data for mathematical characterization of a wave surface by transmitting a beam toward the surface so that the beam is reflected from an element of the surface in a direction determined by the instantaneous, two dimensional slope of the element. The reflected beam impinges on a screen as a spot whose time varying coordinates correspond to the time varying slope of the element. These coordinates are captured by scanning the screen with a raster scan which controls counters identifying the spot position. The instantaneous distance is measured by a capacitance probe to relate the captured coordinates to the corresponding angles of reflection by appropriate trigonometric relations.Type: GrantFiled: February 26, 1988Date of Patent: August 2, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventor: David J. Keller
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Patent number: H523Abstract: A double base propellant grain inhibitor is comprised of a hydroxyl-termied polybutadiene polymer having from 2 to about 3 hydroxyl groups per average molecule and an approximate molecular weight of 2800 to 3600, an inert filler, a cross-linking agent, a thickening agent, an antioxidant, a curative, and a catalyst. When properly applied to the surface of a propellant grain, the inhibitor bond does not weaken with age and the inhibitor produces planar, no-cone grain burning having a constant chamber pressure during the burning of the propellant grain. A 1,4-butylene oxide-type polyether barrier layer consisting of a poly-1,4-butylene oxide diisocyanate with an approximate molecular weight of 850 to 1000, a diol curative, a triol cross-linker, and antioxidant and a cure catalyst can be added between the propellant grain and inhibitor to reduce propellant plasticizer migration.Type: GrantFiled: August 20, 1987Date of Patent: September 6, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventor: John D. Braun
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Patent number: H541Abstract: A ballistic damage tolerant, lightweight hydraulic actuator has a cylindrl liner with opposite open ends each surrounded by conical, outwardly extending projections of the liner. Each end receives a head which is detachably connected to the liner centrally of the projections by an element circumscribing the head. Resin impregnated filaments are wrapped about and extend between the projections at the opposite liner ends so that the filament reinforce the liner against axial forces but do not impede removal of the heads.Type: GrantFiled: August 25, 1987Date of Patent: November 1, 1988Assignee: The United States of America as represented by the Secretary of the NavyInventor: James J. Childress
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Patent number: H593Abstract: A setback motivated element has its movement to an armed position control by an electromechanical escapement which permits arming only upon the reception of a predetermined number of electrical pulses of opposite polarity to provide protection against improper arming due to either electronic or mechanical failure.Type: GrantFiled: April 11, 1988Date of Patent: March 7, 1989Assignee: The United States of America as represented by the Secretary of the NavyInventors: George E. Cooksey, James V. McVay
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Patent number: H710Abstract: A horizon reference system has a plurality of microwave radiation sensors which are selectively connected by a controller to a superheterodyne receiver. The output signals of the receiver are processed in conjunction with antenna selection data to provide roll angle with reference to the horizon and roll angle rate data about any particular axis of the platform on which the sensors are mounted.Type: GrantFiled: November 2, 1984Date of Patent: November 7, 1989Assignee: The United States of America as represented by the Secretary of the NavyInventors: John O. Hooper, Bruce M. Heydlauff, Robert B. Dillinger
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Patent number: H969Abstract: A practical, castable plastic bonded explosive (PBX) is disclosed that is sistant to fire, aerodynamic heating, and mechanical stimuli-impact. The binder is composed of 2-ethylhexyl acrylate, dioctylmaleate, N-vinyl pyrrolidone, Aerosol R-972, t-butyl perbenzoate, cobaltous acetylacetonate, and triethyleneglycoldimethylacrylate, utilizing RDX/HMX as an explosive filler.Type: GrantFiled: March 28, 1988Date of Patent: October 1, 1991Assignee: The United States of America as represented by the Secretary of the NavyInventor: Tucker T. Yee
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Patent number: H1007Abstract: In a solid fuel ramjet in which a fluid flow boundary layer extends along a urning fuel grain and receives combustible material liberated from the grain, exciting oscillations in air flowing toward the grain so that oscillations continue in the boundary layer and promote vortices in the layer to mix the air and the combustible material.Type: GrantFiled: May 24, 1985Date of Patent: January 7, 1992Assignee: The United States of America as represented by the Secretary of the NavyInventors: Klaus C. Schadow, Ephraim Gutmark, Kenneth J. Wilson
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Patent number: H1008Abstract: In a combustor in which a flow area for fuel and air increases suddenly at dump so as to generate vortices which mix the fuel and air for combustion downstream of the dump, the improvement in which the flow cross section upstream of the dump is noncircular, as triangular or rectangular, causing flow downstream of the dump to be noncoherent so that mixing by the vortices is aperiodic with the result that heat release on mixing is uniform in time and does not drive oscillations in the combustor.Type: GrantFiled: May 28, 1985Date of Patent: January 7, 1992Assignee: The United States of America as represented by the Secretary of the NavyInventors: Klaus C. Schadow, Ephraim Gutmark, James E. Crump, Kenneth J. Wilson
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Patent number: H1234Abstract: The invention discloses an air-turborocket having a single set of compres blades extending radially from a common rotor. A shroud ring encircles the outer periphery of the compressor blades and holds a plurality of turbine blades on the outer periphery thereof which are driven by hot expanding fuel rich gases obtained from the partial combustion of a solid propellant in a first combustion chamber external to a compressor housing. The hot expanding fuel rich gases drive the turbine blades which drive the compressor blades thereby providing compressed air which is forcibly mixed by a mixer/diffuser with the hot expanding fuel rich gases for further combustion to provide thrust in a second combustion chamber aft to the compressor.Type: GrantFiled: February 6, 1985Date of Patent: October 5, 1993Assignee: The United States of America as represented by the Secretary of the NavyInventor: Gary R. Burgner
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Patent number: H1384Abstract: A outer bail gimbal bearing having a closed loop filled with circulating ls is disclosed. The balls circulate about an axis parallel to the bail's axis of rotation. A shallow region within the loop allows the balls to emerge from the loop and engage a race made in the outer edge of the outer bail.Type: GrantFiled: August 28, 1986Date of Patent: December 6, 1994Assignee: The United States of America as represented by the Secretary of the NavyInventor: Steven A. Sievert