Patents Represented by Attorney, Agent or Law Firm James J. McGroary
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Patent number: 7325749Abstract: A self-contained power controller having a power driver switch, programmable controller, communication port, and environmental parameter measuring device coupled to a controllable device. The self-contained power controller needs only a single voltage source to power discrete devices, analog devices, and the controlled device. The programmable controller has a run mode which, when selected, upon the occurrence of a trigger event changes the state of a power driver switch and wherein the power driver switch is maintained by the programmable controller at the same state until the occurrence of a second event.Type: GrantFiled: December 17, 2003Date of Patent: February 5, 2008Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jane C. Alexander, David E. Howard, Dennis A. Smith
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Patent number: 7320223Abstract: A system is provided to control the environment experienced by a child in a child safety seat. Each of a plurality of thermoelectric elements is individually controllable to be one of heated and cooled relative to an ambient temperature. A first portion of the thermoelectric elements are positioned on the child safety seat such that a child sitting therein is positioned thereover. A ventilator coupled to the child safety seat moves air past a second portion of the thermoelectric elements and filters the air moved therepast. One or more jets coupled to the ventilator receive the filtered air. Each jet is coupled to the child safety seat and can be positioned to direct the heated/cooled filtered air to the vicinity of the head of the child sitting in the child safety seat.Type: GrantFiled: January 28, 2005Date of Patent: January 22, 2008Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard W. Dabney, Susan V. Elrod
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Patent number: 7284792Abstract: A cushion system for use with a child safety seat has a plurality of bladders assembled to form a seat cushion that cooperates with the seat's safety harness. One or more sensors coupled to the safety harness sense tension therein and generate a signal indicative of the tension. Each of the bladders is individually pressurized by a pressurization system to define a support configuration of the seat cushion. The pressurization system is disabled when tension in the safety harness has attained a threshold level.Type: GrantFiled: January 28, 2005Date of Patent: October 23, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard W. Dabney, Susan V. Elrod
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Patent number: 7275675Abstract: A friction stir weld tool sleeve is supported by an underlying support pin. The pin material is preferably selected for toughness and fracture characteristics. The pin sleeve preferably has a geometry which employs the use of an interrupted thread, a plurality of flutes and/or eccentric path to provide greater flow through. Paddles have been found to assist in imparting friction and directing plastic metal during the welding process.Type: GrantFiled: August 20, 2004Date of Patent: October 2, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert W. Carter, Lewis N. Payton
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Patent number: 7265476Abstract: A microscopic translation device for a microelectromechanical system includes a pair of linear stator assemblies disposed in spaced relation to define an elongate channel. Each assembly is formed by a plurality of stators arranged in a row along the channel. A shuttle member is disposed between the stator assemblies for translating movement along the channel. The shuttle member includes a plurality of rotors extending outwardly from opposite sides. The shuttle is grounded through the stator assemblies and includes a mounting area for an object to be translated. Electrical lines are individually connected to alternate stators of a plurality of groups of the stators. A current supply sequentially supplies current through the electrical lines to the alternate stators so as to effect charging of the stators in a predetermined sequence. This produces a tangential capacitive force that causes translation of the shuttle.Type: GrantFiled: October 26, 2004Date of Patent: September 4, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mustafa A. G. Abushagur, Cynthia K. Ferguson, Gregory P. Nordin, Jennifer M. English
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Patent number: 7259981Abstract: A nonvolatile analog memory uses pairs of ferroelectric field effect transistors (FFETs). Each pair is defined by a first FFET and a second FFET. When an analog value is to be stored in one of the pairs, the first FFET has a saturation voltage applied thereto, and the second FFET has a storage voltage applied thereto that is indicative of the analog value. The saturation and storage voltages decay over time in accordance with a known decay function that is used to recover the original analog value when the pair of FFETs is read.Type: GrantFiled: November 29, 2005Date of Patent: August 21, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Todd C. MacLeod
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Patent number: 7228241Abstract: In some embodiments, systems and methods and apparatus are provided through which the equation of state is used to control a process through analyses of one or more properties of a fluid through an interactive modeler that models the equation of state for the fluid in the process based on measured signals and for selectively enabling the modeling of control changes to the process. In some embodiments, a device generates an indication of machine health based on variations on the equation of state for a fluid in a machine. In some embodiments, one or more properties for the fluid from at least one unmeasured machine parameter in the interactive modeler are determined for the machine at various operating states. In some embodiments, a difference between an expected one or more properties of the fluid beyond a set point indicates the health of the machine.Type: GrantFiled: June 13, 2005Date of Patent: June 5, 2007Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John P. Butas, Paul D. Van Buskirk
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Patent number: 7177164Abstract: A low power, high voltage power supply system includes a high voltage power supply stage and a preregulator for programming the power supply stage so as to produce an output voltage which is a predetermined fraction of a desired voltage level. The power supply stage includes a high voltage, voltage doubler stage connected to receive the output voltage from the preregulator and for, when activated, providing amplification of the output voltage to the desired voltage level. A first feedback loop is connected between the output of the preregulator and an input of the preregulator while a second feedback loop is connected between the output of the power supply stage and the input of the preregulator.Type: GrantFiled: March 10, 2006Date of Patent: February 13, 2007Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Douglas B. Bearden
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Patent number: 7174077Abstract: An optical fiber for evenly illuminating a target. The optical fiber is coupled to a laser emitting diode and receives laser light. The laser light travels through the fiber optic and exits at an exit end. The exit end has a diffractive optical pattern formed thereon via etching, molding or cutting, to reduce the Gaussian profile present in conventional fiber optic cables. The reduction of the Gaussian provides an even illumination from the fiber optic cable.Type: GrantFiled: July 30, 2003Date of Patent: February 6, 2007Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Richard T. Howard
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Patent number: 7134885Abstract: A miniature assembly is disclosed which includes a housing assembly with a cover configured to be sealably secured to a box-like receptacle. The receptacle comprises openings on opposing sides for the seating therein of communications connectors. Enclosed within housing is custom-sized circuit board for supporting, at least, a standard communications interface and at least one electronic device.Type: GrantFiled: July 20, 2005Date of Patent: November 14, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David E. Howard, Dennis A. Smith, Dean C. Alhorn
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Patent number: 7135684Abstract: The sky contains many active sources that emit X-rays, gamma rays, and neutrons. Unfortunately hard X-rays, gamma rays, and neutrons cannot be imaged by conventional optics. This obstacle led to the development of Fourier imaging systems. In early approaches, multiple grid pairs were necessary in order to create rudimentary Fourier imaging systems. At least one set of grid pairs was required to provide multiple real components of a Fourier derived image, and another set was required to provide multiple imaginary components of the image. It has long been recognized that the expense associated with the physical production of the numerous grid pairs required for Fourier imaging was a drawback. Herein one grid pair (two grids), with accompanying rotation and translation, can be used if one grid has one more slit than the other grid, and if the detector is modified.Type: GrantFiled: April 21, 2005Date of Patent: November 14, 2006Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Jonathan W. Campbell
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Patent number: 7118074Abstract: A tether system for providing thrust to or power subsystems of an artificial satellite in a low earth orbit. The tether has three main sections, an insulated section connected to the satellite, a conducting section connected to the insulating section for drawing in and releasing electrons from the space plasma and a non-conducting section for providing a tension to the other sections of the tether. An oxygen resistant coating is applied to the bare wire of the conducting section as well as the insulated wires of the insulated section that prevents breakdown during tether operations in the space plasma. The insulated and bare wire sections also surround a high tensile flexible polymer core to prevent any debris from breaking the tether during use.Type: GrantFiled: October 17, 2003Date of Patent: October 10, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Charles L. Johnson, Judy L. C. Ballance, Kenneth J. Welzyn, Jason A. Vaughn, Enrico Lorenzini, Peter S. Schuler
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Patent number: 7116098Abstract: A limit and position sensing system includes a sensor assembly and an emitter. The sensor assembly includes first and second electrical conductors arranged in opposing parallel planes. The first electrical conductor is coiled outwardly from either end thereof in a clockwise fashion to form a first coil region and a second coil region. The second electrical conductor forms a single coil with portions of the single coil's rings lying between the first end and second end of the first electrical conductor being parallel to an axis of the first electrical conductor's plane. Ferromagnetic material is aligned with the first and second electrical conductors and spans beyond (a) the first and second ends of the first electrical conductor, and (b) the portions of the rings of the second electrical conductor's single coil that lie between the first end and second end of the first electrical conductor.Type: GrantFiled: February 16, 2006Date of Patent: October 3, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Dean C. Alhorn, David E. Howard, Dennis A. Smith
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Patent number: 7106457Abstract: An achromatic shearing phase sensor generates an image indicative of at least one measure of alignment between two segments of a segmented telescope's mirrors. An optical grating receives at least a portion of irradiance originating at the segmented telescope in the form of a collimated beam and the collimated beam into a plurality of diffraction orders. Focusing optics separate and focus the diffraction orders. Filtering optics then filter the diffraction orders to generate a resultant set of diffraction orders that are modified. Imaging optics combine portions of the resultant set of diffraction orders to generate an interference pattern that is ultimately imaged by an imager.Type: GrantFiled: May 21, 2004Date of Patent: September 12, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: H. Philip Stahl, Chanda Bartlett Walker
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Patent number: 7095000Abstract: Apparatus and methods are provided through which a radio-frequency dielectric heater has a cylindrical form factor, a variable thermal energy deposition through variations in geometry and composition of a dielectric, and/or has a thermally isolated power input.Type: GrantFiled: September 13, 2004Date of Patent: August 22, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William Herbert Sims, III, Thomas J. Godfroy, Leo Bitteker
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Patent number: 7081730Abstract: A motor controller system uses a rotary sensor with a plurality of signal conditioning units, coupled to the rotary sensor. Each of these units, which is associated with a particular range of motor output shaft rotation rates, generate a feedback signal indicative of the position of the motor's output shaft. A controller (i) converts a selected motor output shaft rotation rate to a corresponding incremental amount of rotational movement for a selected fixed time period, (ii) selects, at periodic completions of the selected fixed time period, the feedback signal from one of the signal conditioning units for which the particular range of motor output shaft rotation rates associated therewith encompasses the selected motor output shaft rotation rate, and (iii) generates a motor drive signal based on a difference between the incremental amount of rotational movement and the feedback signal from the selected one of the signal conditioning units.Type: GrantFiled: May 21, 2004Date of Patent: July 25, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David E. Howard, Dean C. Alhorn, Dennis A. Smith, Kenneth R. Dutton, Mitchell Scott Paulson
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Patent number: 7051765Abstract: An orifice plate for use in a conduit through which fluid flows is defined by a central circular region having a radius R0 and a ring-shaped region surrounding the central circular region. The ring-shaped region has holes formed therethrough with those holes centered at each radius R thereof satisfying a relationship AR=a/(XRVRb) where AR is a sum of areas of those holes having centers at radius R, XR is a flow coefficient at radius R, VR is a velocity of the fluid that is to flow through the conduit at radius R, b is a constant selected to make at least one process variable (associated with the fluid that is to flow through the conduit) approximately equal at each radius R, and a is a constant that is equal to (XRARVRb) at each radius R.Type: GrantFiled: December 19, 2003Date of Patent: May 30, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Anthony R. Kelley, Paul D. Van Buskirk
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Patent number: 7050161Abstract: An apparatus controls positions of plural mirror segments in a segmented mirror with an edge sensor system and a controller. Current mirror segment edge sensor measurements and edge sensor reference measurements are compared with calculated edge sensor bias measurements representing a global radius of curvature. Accumulated prior actuator commands output from an edge sensor control unit are combined with an estimator matrix to form the edge sensor bias measurements. An optimal control matrix unit then accumulates the plurality of edge sensor error signals calculated by the summation unit and outputs the corresponding plurality of actuator commands. The plural mirror actuators respond to the actuator commands by moving respective positions of the mirror segments. A predetermined number of boundary conditions, corresponding to a plurality of hexagonal mirror locations, are removed to afford mathematical matrix calculation.Type: GrantFiled: August 6, 2003Date of Patent: May 23, 2006Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space AdministrationInventor: John M. Rakoczy
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Patent number: 7039207Abstract: An entertainment and pacification system for use with a child car seat has speakers mounted in the child car seat with a plurality of audio sources and an anti-noise audio system coupled to the child car seat. A controllable switching system provides for, at any given time, the selective activation of i) one of the audio sources such that the audio signal generated thereby is coupled to one or more of the speakers, and ii) the anti-noise audio system such that an ambient-noise-canceling audio signal generated thereby is coupled to one or more of the speakers. The controllable switching system can receive commands generated at one of first controls located at the child car seat and second controls located remotely with respect to the child car seat with commands generated by the second controls overriding commands generated by the first controls.Type: GrantFiled: March 18, 2003Date of Patent: May 2, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Susan Vinz Elrod, Richard W. Dabney
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Patent number: 7017812Abstract: A variable distance angular symbology reader utilizes at least one light source to direct light through a beam splitter and onto a target. A target may be angled relative to the impinging light beam up to and maybe even greater than 45°. A reflected beam from the target passes through the beam splitter and is preferably directed 90° relative to the light source through a telecentric lens to a scanner which records an image of the target such as a direct part marking code.Type: GrantFiled: November 26, 2003Date of Patent: March 28, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Harry F. Schramm, Jr., Eric L. Corder