Gallagher
Andrew John Gallagher, Castle Hill AU
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20100208550 | VIBRATION ISOLATION SECTION - According to the present invention there is provided a vibration isolation section for use in a seismic streamer system, the section including: | 08-19-2010 |
Brad S. Gallagher, Estero, FL US
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20140124386 | Bang Box - The invention is a compact type 3 explosive storage magazine. It has an approximate external measure of 4.75″ wide, 7.87″ long and 8.69″ high. This design is one quarter the size of the nearest comparable type 3 magazine and has an integrated locking mechanism rather than a hinged hasp locking mechanism which is unique among type 3 magazines. The hinged hasp represents the easiest access point for theft and most likely security component to fail. | 05-08-2014 |
Brian Gallagher, Greenville, SC US
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20130008172 | Systems and Methods for Modified Wobbe Index Control With Constant Fuel Temperature - The present application provides a gas turbine engine system for combusting a flow of fuel. The gas turbine engine system may include a combustor and a fuel system for providing the flow of fuel to the combustor. The fuel system may include a fuel heat exchanger so as to provide the flow of fuel to the combustor at a substantially constant temperature. | 01-10-2013 |
Brian James Gallagher, Litchfield, NH US
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20140158586 | PULP SCREEN ROTOR WITH SLURRY PASSAGES AROUND AND THROUGH THE ROTOR - A rotor adapted for mounting for rotation within a screen of a pulp screening apparatus, and for defining a screening space between the rotor and the screen so that pulp suspension flows into the screening space, with accepted pulp passing through the screen to a stock outlet and rejected pulp passing along a screen inlet surface in a screening flow direction to a rejects outlet. The rotor has an interior, and an exterior with pressure impulse protuberances thereon for rotation with the rotor in close proximity to the inlet surface. A stock inlet communicates with the screening space and the rotor interior. And the rotor has at least one opening extending in the screening flow direction from its interior to its exterior for over at least a fourth of screening flow length of the rotor for admitting a substantial portion of pulp suspension from the stock inlet and the rotor interior into the screening space. | 06-12-2014 |
Chad Gallagher, Baltimore, MD US
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20150213504 | SYSTEMS AND METHODS FOR AD-SUPPORTED MOBILE DATA PLANS OR IN-APP PURCHASES - Methods are disclosed for providing an ad-supported mobile data plan, where ad display may be tied to data usage levels and user input. A method includes receiving, using at least one processor, user interaction with advertisement content displayed on a device; retrieving, using the at least one processor, a data usage limit associated with the device; and causing a change in the data usage limit based on the user interaction with the advertisement content displayed on the device. | 07-30-2015 |
Cheri A. Gallagher, St. Louis, MO US
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20160089412 | REMEDIAL TONIC - A medicinal tonic has a unique combination of ingredients. The tonic is composed, proportionally, of approximately 66 fluid ounces of organic Aloe juice, 60 ounces of organic Aloe gel, 16 grams be weight of wild lapacho bark extract, and 20 milliliters each of organic hyssop, organic or wild milk thistle extract and organic, naturally farmed olive leaf extract. The ingredients produce a new and medicinal compound that prevents or alleviates natural occurring diseases or conditions and helps heal wounds and other ailments and has other salutary effects on the human body. | 03-31-2016 |
Christopher Timothy Gallagher, Ft. Thomas, KY US
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20140058644 | METHOD, SYSTEM, AND APPARATUS FOR REDUCING A TURBINE CLEARANCE - A method for reducing a turbine clearance between a plurality of rotor blades of a turbine engine and a shroud of the turbine engine is provided. Said method includes determining, with a flight operation controller, that an airplane is in a first flight condition, wherein the first flight condition is associated with a first turbine clearance and a first engine responsiveness level, determining, with the flight operation controller, that the airplane is in a second flight condition, adjusting an engine responsiveness level from the first engine responsiveness level to a second engine responsiveness level based on determining the airplane is in the second flight condition, and adjusting the turbine clearance from the first turbine clearance to a second turbine clearance based on the engine responsiveness level. | 02-27-2014 |
Dennis Gallagher, Boulder, CO US
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20130105925 | Integrated Die-Level Cameras And Methods Of Manufacturing The Same | 05-02-2013 |
20140220725 | Integrated Die-Level Cameras And Methods Of Manufacturing The Same - An integrated die-level camera system and method of making the camera system include a first die-level camera formed at least partially in a die. A second die level camera is also formed at least partially in the die. Baffling is formed to block stray light between the first and second die-level cameras. | 08-07-2014 |
Dennis Joseph Gallagher, Boulder, CO US
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20130301011 | ADVANCED LIGHTPIPE HOMOGENIZER - A faceted lightpipe arrangement and method have been described for use with an imaging projector system. A plurality of facets can be arranged to receive beams of light and to converge the beams of light while traveling from an input end to an output end of the lightpipe. The faceted lightpipe provides for a high degree of color mixing and a high degree of intensity uniformity. | 11-14-2013 |
Edward Gallagher, Bellevue, WA US
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20140155861 | EXTRUSION METHODS AND DEVICES FOR DRUG DELIVERY - Disclosed herein are devices and methods for delivering agents to a solid tissue. | 06-05-2014 |
Edward J. Gallagher, West Hartford, CT US
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20130008144 | EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES - A gas turbine engine includes a spool, a turbine coupled to drive the spool and a propulsor that is coupled to be driven by the turbine through the spool. A gear assembly is coupled between the propulsor and the spool such that rotation of the spool drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extends from the hub. The row includes no more than 16 of the propulsor blades. | 01-10-2013 |
20130008146 | EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES - A gas turbine engine includes a spool, a turbine coupled to drive the spool, and a propulsor that is coupled to be driven by the turbine through the spool. A gear assembly is coupled between the propulsor and the spool such that rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extends from the hub. The row includes no more than 20 of the propulsor blades. | 01-10-2013 |
20130008170 | SUBSONIC SWEPT FAN BLADE - A gas turbine engine includes a spool, a turbine coupled to drive the spool, a propulsor coupled to be driven at a at a design speed by the turbine through the spool, and a gear assembly coupled between the propulsor and the spool. Rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extend from the hub. Each of the propulsor blades includes an airfoil body. The leading edge of the airfoil body has a swept profile such that, at the design speed, a component of a relative velocity vector of a working gas that is normal to the leading edge is subsonic along the entire radial span. | 01-10-2013 |
20130011266 | FAN STAGGER ANGLE FOR DIRT REJECTION - A gas turbine engine includes a spool, a turbine coupled to drive the spool, a propulsor coupled to be rotated about an axis by the turbine through the spool, and a gear assembly coupled between the propulsor and the spool such that rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extend from the hub. Each of the propulsor blades has a span between a root at the hub and a tip, and a chord between a leading edge and a trailing edge. The chord forms a stagger angle α with the axis, and the stagger angle α is less than 15° at a position along the propulsor blade that is within an inboard 20% of the span. | 01-10-2013 |
20130189117 | ROTOR WITH FLATTENED EXIT PRESSURE PROFILE - A rotor blade comprises an airfoil extending radially from a root section to a tip section and axially from a leading edge to a trailing edge, the leading and trailing edges defining a curvature therebetween. The curvature determines a relative exit angle at a relative span height between the root section and the tip section, based on an incident flow velocity at the leading edge of the airfoil and a rotational velocity at the relative span height. In operation of the rotor blade, the relative exit angle determines a substantially flat exit pressure ratio profile for relative span heights from 75% to 95%, wherein the exit pressure ratio profile is constant within a tolerance of 10% of a maximum value of the exit pressure ratio profile. | 07-25-2013 |
20130340406 | FAN STAGGER ANGLE FOR GEARED GAS TURBINE ENGINE - A gas turbine engine includes a spool, a turbine coupled with the spool, a propulsor coupled to be rotated about an axis by the turbine through the spool and a gear assembly coupled between the propulsor and the spool such that rotation of the spool results in rotation of the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extends from the hub. Each of the propulsor blades has a span between a root at the hub and a tip, and a chord between a leading edge and a trailing edge such that the chord forms a stagger angle α with the axis. The stagger angle α is less than 62° at all positions along the span, with said hub being at 0% of the span and the tip being at 100% of the span. | 12-26-2013 |
20150233250 | GAS TURBINE ENGINE AIRFOIL - An airfoil of a turbine engine includes, pressure and suction sides extending in a radial direction from a 0% span to a 100% span position. The airfoil has a relationship between a gap/chord ratio and span position that defines a curve with a gap/chord ratio of less than 0.80 from 80% span to 100% span. | 08-20-2015 |
20150233251 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a stacking offset and a span position that is at least a third order polynomial curve that includes at least one positive and negative slope. The positive slope crosses an initial axial stacking offset that corresponds to the 0% span position at a zero-crossing position. A first axial stacking offset X | 08-20-2015 |
20150233252 | GAS TURBINE ENGINE AIRFOIL - An airfoil of a turbine engine includes pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a tangential stacking offset and a span position that is at least a third order polynomial curve that includes at least one positive and negative slope. The positive slope leans toward the suction side and the negative slope leans toward the pressure side. An initial slope starting at the 0% span position is either zero or positive. The first critical point is in the range of 5-15% span. | 08-20-2015 |
20150233323 | GAS TURBINE ENGINE AIRFOIL - A gas turbine engine includes a fan section, a compressor section and a turbine section, one of which includes an airfoil. The airfoil includes pressure and suction sides extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a maximum chord length projection that is not in an axial view. | 08-20-2015 |
20150260051 | GEARED LOW FAN PRESSURE RATIO FAN EXIT GUIDE VANE STAGGER ANGLE - A fan exit guide vane assembly for a gas turbine engine includes a plurality of guide vanes having a pressure side and a suction side extending between a leading edge and a trailing edge. The vanes further include a span extending between a root and tip with a stagger angle defined as an angle between a longitudinal axis parallel to an engine axis of rotation and a line connecting the leading edge and the trailing edge that is less than about 15°. | 09-17-2015 |
20150354362 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a total chord length and a span position and corresponds to a curve that has an increasing total chord length from the 0% span position to a first peak. The first peak occurs in the range of 45-65% span position, and the curve either remains generally constant or has a decreasing total chord length from the first peak to the 100% span position. The total chord length is at the 0% span position in the range of 8.2-10.5 inches (20.8-26.7 cm). | 12-10-2015 |
20150354363 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes an airfoil having pressure and suction sides extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a curve corresponding to a relationship between a trailing edge sweep angle and a span position. The trailing edge sweep angle is in a range of 10° to 20° in a range of 40-70% span position. The trailing edge sweep angle is positive from 0% span to at least 95% span. | 12-10-2015 |
20150354364 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes an airfoil that has pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a curve that corresponds to a relationship between a trailing edge sweep angle and a span position. The trailing edge sweep angle is in a range of 10° to 20° in a range of 40-70% span position, and the trailing edge sweep angle is positive from 0% span to at least 95% span. The airfoil has a relationship between a leading edge dihedral and a span position. The leading edge dihedral is negative from the 0% span position to the 100% span position. A positive dihedral corresponds to suction side-leaning, and a negative dihedral corresponds to pressure side-leaning. | 12-10-2015 |
20150354367 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes an airfoil having pressure and suction sides extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a leading edge dihedral and a span position. The leading edge dihedral is negative from the 0% span position to the 100% span position. A positive dihedral corresponds to suction side-leaning, and a negative dihedral corresponds to pressure side-leaning. | 12-10-2015 |
20150361797 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a stacking offset and a span position that is at least a third order polynomial curve that includes at least one positive and negative slope. The positive slope leans aftward and the negative slope leans forward relative to an engine axis. The positive slope crosses an initial axial stacking offset corresponding to the 0% span position at a zero-crossing position. A first axial stacking offset X | 12-17-2015 |
20160024929 | GAS TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes an airfoil that has pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a leading edge dihedral and a span position. The leading edge dihedral is negative from the 0% span position to the 100% span position. A positive dihedral corresponds to suction side-leaning, and a negative dihedral corresponds to pressure side-leaning. The airfoil is a fan blade for a gas turbine engine. The airfoil has a relationship between a trailing edge dihedral and a span position. The trailing edge dihedral is positive from the 0% span position to the 100% span position. A positive dihedral corresponds to suction side-leaning and a negative dihedral corresponds to pressure side-leaning. | 01-28-2016 |
20160032728 | GAS TURBINE ENGINE AIRFOIL - An airfoil of a turbine engine includes pressure and suction sides that extend in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a relationship between a tangential stacking offset and a span position that is at least a third order polynomial curve that includes at least one positive and negative slope. The positive slope leans toward the suction side and the negative slope leans toward the pressure side. An initial slope starts at the 0% span position is either zero or positive. The first critical point is less than 15% span. | 02-04-2016 |
20160069187 | GAS TURBINE ENGINE AIRFOIL - An airfoil of a turbine engine according to an example of the present disclosure includes, among other things, pressure and suction sides extending in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between a gap/chord ratio and span position that defines a curve with a gap/chord ratio having a portion with a negative slope. | 03-10-2016 |
20160076380 | INCIDENCE-TOLERANT, HIGH-TURNING FAN EXIT STATOR - A gas turbine engine component is described. The gas turbine engine component includes an inner diameter edge, an outer diameter edge, a trailing edge and a leading edge. The leading edge has a positive (aft) aerodynamic sweep across substantially an entire span of the leading edge. The gas turbine engine component has a camber angle greater than 50 degrees across substantially an entire span of the component. The gas turbine engine component may have asymmetrical tangential stacking of the component in the radial direction. | 03-17-2016 |
Emerson R. Gallagher, Vancouver CA
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20080220154 | METHOD OF FORMING FLUID FLOW FIELD PLATES FOR ELECTROCHEMICAL DEVICES - A method of making graphite articles for electrochemical fuel cells, such as fluid flow field plates, by partially impregnating a porous, self-supporting expanded graphite sheet with a first binder comprising a first liquid resin to form a partially impregnated graphite sheet; mechanically deforming at least one surface of the impregnated graphite sheet to form an intermediate fluid flow field plate; impregnating the mechanically deformed intermediate fluid flow field plate with a second binder comprising a second liquid resin to form an impregnated fluid flow field plate; and curing at least the second resin to form a substantially fluid impermeable fluid flow field plate. | 09-11-2008 |
20080241606 | METHOD AND APPARATUS FOR HUMIDIFYING A GAS IN FUEL CELL SYSTEMS - A membrane exchange humidifier for use with a fuel cell system, fuel cell or fuel cell stack includes at least one wet chamber, a plurality of dry chambers, a water permeable sheet membrane; wherein each of the plurality of dry chambers is separated from one or more of the at least one wet chambers by the water permeable sheet membrane, whereby water is capable of being transferred across the water permeable sheet membrane; and a variable flow cross section restriction device fluidly connects to at least one of the plurality of dry chambers. | 10-02-2008 |
20120034542 | SEAL FOR SOLID POLYMER ELECTROLYTE FUEL CELL - In solid polymer fuel cells employing framed membrane electrode assemblies, a conventional anode compliant seal is employed in combination with a cathode non-compliant seal to provide for a thinner fuel cell design, particularly in the context of a fuel cell stack. This approach is particularly suitable for fuel cells operating at low pressure. | 02-09-2012 |
20150030960 | SEAL FOR SOLID POLYMER ELECTROLYTE FUEL CELL - In solid polymer fuel cells employing framed membrane electrode assemblies, a conventional anode compliant seal is employed in combination with a cathode non-compliant seal to provide for a thinner fuel cell design, particularly in the context of a fuel cell stack. This approach is particularly suitable for fuel cells operating at low pressure. | 01-29-2015 |
Eric A. Gallagher, Kalamazoo, MI US
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20140251378 | DISHWASHER WITH RECHARGEABLE COMPONENTS - A dishwasher for treating dishes according to an automatic cycle of operation having a tub that at least partially defines a treating chamber, a slidable dish holder, an electricity-consuming component having a rechargeable battery, and a battery charging system to recharge the rechargeable battery of the electricity-consuming component when the dish holder is in the treating position. | 09-11-2014 |
Gregory John Gallagher, Cape Town ZA
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20100201524 | INFANT MONITOR - A method and device ( | 08-12-2010 |
20150305653 | MOTION MONITOR - A method and device ( | 10-29-2015 |
Ian Stuart Gallagher, Hamilton NZ
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20080308299 | Connection Apparatus - A connection apparatus ( | 12-18-2008 |
20120138883 | Taut Wire Fence System - An apparatus and method of detecting a change in tension of a taut wire fence system, where the system includes a connector including a main body member having a first attachment portion at one end of the member and a second attachment portion at the opposite end of the member and a sensor located on the main body between and aligned with the first and second attachment portions, the method including the steps of attaching a first wire of the fence to the first attachment portion and attaching the second attachment portion of the connector either to an end support mount for the fence, or to a second wire of the fence system such that the connector is held independently of direct contact with any fence support, and such that the first wire, the sensor on the main body of the connector and the second attachment portion respectively, are aligned. | 06-07-2012 |
20130187784 | FENCING - A wire fence accessory is provided including a connector configured to secure the accessory to a support post of a wire fence system; and a tension sensor configured to measure tension in a wire connected to the accessory and output a signal indicative of the tension, wherein the accessory includes an indicator configured to output, at the accessory, an indication of the tension in the wire according to the signal output by the tension sensor. | 07-25-2013 |
James Gallagher, Minneapolis, MN US
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20150148507 | MONOMERS, POLYMERS AND ARTICLES CONTAINING THE SAME FROM SUGAR DERIVED COMPOUNDS - Disclosed herein are monomers formed by reacting a sugar derived compound(s) comprising a lactone and two hydroxyls with a compound(s) comprising an isocyanate and an acrylate or methacrylate. Polymers formed from such monomers, and articles formed from the polymers are also disclosed. | 05-28-2015 |
James Gallagher, Savannah, GA US
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20130197739 | METHODS AND SYSTEMS FOR AIRCRAFT HEALTH AND TREND MONITORING - The disclosed embodiments relate to methods and systems for monitoring sub-systems of an aircraft to detect an abnormal condition, and for identifying one or more sources that are causing the abnormal condition. In response to detecting a trigger event during flight of the aircraft, data for a plurality of relevant parameters is measured and stored in a parameter file. The parameter file is transmitted from the aircraft over a wireless communication link, and relayed to a ground support network. At the ground support network, the measured data for the plurality of the relevant parameters is then used to identify the one or more sources that are causing the abnormal condition. | 08-01-2013 |
James Joseph Gallagher, New Carrollton, MD US
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20130041439 | Cold cap - The purpose of this invention is to extend life. When a person's heart stops beating through any number of causes, the lack of oxygen carried by the blood to the brain occurs, causing the condition of suspended animation. The deterioration of the brain cells will result and the spark of life is forever extinguished. The Cold Cap is intended to extend the time between the end of suspended animation and the beginning of the deterioration of the brain cells. | 02-14-2013 |
James L. Gallagher, Little Compton, RI US
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20140332110 | FLEXIBLE HIGH-PRESSURE PIPE STRUCTURE - A pipe structure includes a carcass made from an arrangement of hoop segments that join to form a series of articulating joints. A hard yet flexible outer shell is formed around the carcass. The hoop segments are reinforced with fiber to increase strength and reduce weight. The shell anchors to the carcass at intervals along its length to hold the hoop segments together, while providing the flexibility needed for deep water and other high pressure pipe applications. | 11-13-2014 |
Jamie T. Gallagher, South Burlington, VT US
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20130275532 | Electronic Message Content Party Restriction System and Method - Electronic messaging system and method with a determination of message content information that includes a restricted indication of a sender and/or a recipient. A message content that includes a restricted indication of a sender and/or recipient may be rejected. A rejected message content may be limited in deliverability from a sender's computer. A rejected message content may also prompt a warning and/or be modifiable to allow for transmission. | 10-17-2013 |
Jim Gallagher, Savannah, GA US
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20130197725 | METHODS AND SYSTEMS FOR REQUESTING AND RETRIEVING AIRCRAFT DATA DURING FLIGHT OF AN AIRCRAFT - The disclosed embodiments relate to methods and systems for requesting and retrieving aircraft data during flight of an aircraft. This aircraft data can be used to perform additional monitoring of aircraft sub-systems to detect an abnormal condition, and/or to identify one or more sources that are causing the abnormal condition. In one embodiment, aircraft data for one or more relevant parameters can be requested from the ground, measured on-board the aircraft, and stored in a data file that is then communicated back to personnel on the ground. The real-time aircraft data for one or more relevant parameters can then be analyzed to identify the one or more sources that are causing the abnormal condition. | 08-01-2013 |
20140309820 | METHODS AND SYSTEMS FOR REQUESTING AND RETRIEVING AIRCRAFT DATA DURING FLIGHT OF AN AIRCRAFT - The disclosed embodiments relate to methods for requesting and retrieving aircraft data during flight of an aircraft. This aircraft data can be used to perform additional monitoring of aircraft sub-systems to detect an abnormal condition, and/or to identify one or more sources that are causing the abnormal condition. In one embodiment, aircraft data for one or more relevant parameters can be requested from the ground, measured on-board the aircraft, and stored in a data file that is then communicated back to personnel on the ground. The real-time aircraft data for one or more relevant parameters can then be analyzed to identify the one or more sources that are causing the abnormal condition. | 10-16-2014 |
John Gallagher, Goffstown, NH US
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20130033968 | Sparker Array Source - A sparker array includes a plurality of sparker sources of sound and light emissions, the plurality of sparker sources arranged in a geometric pattern with respect to a region, the array configured to deliver a maximal acoustic output to the region. Sparker sources may include reflectors. A single electrical source to drive a sparker array may be employed. A sparker system may include two or more sparker arrays. A time delay may be employed to trigger electrical circuits of the sparker arrays. Sparker arrays may be used to deliver shock waves with increased operational life, consistency and efficacy for specific applications. | 02-07-2013 |
John Paul Gallagher, Hockessin DE
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20100305902 | Method for characterizing hiding of coating compositions and apparatus used therefor - The present invention is directed to an apparatus and a method that characterizes the hiding of coating compositions, such as automotive OEM and refinishes paints. The method is directed to sequentially storing in a computing device hiding data obtained by measuring the color difference (ΔRGB) in reflections of light and dark portions of target areas of a monotonic coating resulting from a coating composition applied over hiding test panel and by measuring coating thicknesses of the monotonic coating that correspond to the target areas, classifying the type of the hiding data, selecting fitting equations applicable to the classified hiding data, fitting the selected equation to match the classified hiding data and locating a hiding thickness on the monotonic coating that corresponds to the threshold value of the color difference at that location to determine the hiding thickness of the coating composition. | 12-02-2010 |
Joseph V. Gallagher, Newport, RI US
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20160100018 | CROSS CHANNEL IN-VEHICLE MEDIA CONSUMPTION MEASUREMENT AND ANALYSIS - The invention provides a novel and unique system and method for cross channel in-vehicle media consumption measurement and analysis. Real-time measurement and analysis of all applicable forms of media that a driver or passenger may consume inside of an automobile can be achieved. This includes AM/FM radio, Satellite Digital Audio Radio Service (SDARS), stored media such as CDs, MP3s & DVDs, streaming media, internet radio, audio books, podcasts, text-to-speech content, use of hands-free calling and other forms of audio, including content routed to the In Vehicle Entertainment (IVE) system through integration with a smartphone, media player or other similar external Consumer Electronic (CE) device via wired or wireless connectivity, including but not limited to USB, Bluetooth, Wi-Fi, and the like, and also including integration platforms such as Apple CarPlay, Google Android Auto, Harman Aha Radio, Panasonic Aupeo, Pioneer Zypr, Ford Sync, MirrorLink, Airbiquity Choreo, and the like). | 04-07-2016 |
Joyce Gallagher, Milltown, NJ US
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20140050700 | EX-VIVO TREATMENT OF PERIPHERAL BLOOD LEUKOCYTES WITH IFN-Lambda - The present invention provides a method of treating Th2-associated diseases and disorders by modulating the expression or secretion of IL-4, IL-5 and IL-13 using interferon lambda (IFN-λ). For Th2-associated diseases and disorders, cells of a patient having a Th2-associated disease or disorder are treated ex vivo, with IFN-λ and returned to the patient. The present invention also provides a method of ex vivo treatment, in conjunction with co-administration of IFN-λ | 02-20-2014 |
Luke Jeremy Gallagher, Auckland NZ
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20090065119 | METHOD OF FORMING A CONDUIT - A method of continuously forming heated conduit includes performing a tape for winding onto a spiral pipeline former. At least one conductor is positioned adjacent to the centreline of and parallel with a thin polymer ribbon. The ribbon is folded in half to encapsulate the conductors. The folded ribbon is thermally welded to itself, The folded, welded, ribbon is passed through a creaser, which forms a crease midway across the folded ribbon. The creased pre-formed ribbon is formed into a conduit in a continuous process on a spiral pipeline former. | 03-12-2009 |
20090260737 | METHOD OF FORMING A CONDUIT - A method of continuously forming heated conduit includes performing a tape for winding onto a spiral pipeline former. At least one conductor is positioned adjacent to the centreline of and parallel with a thin polymer ribbon. The ribbon is folded in half to encapsulate the conductors. The folded ribbon is thermally welded to itself. The folded, welded, ribbon is passed through a creaser, which forms a crease midway across the folded ribbon. The creased pre-formed ribbon is formed into a conduit in a continuous process on a spiral pipeline former. | 10-22-2009 |
Matthew Steven Gallagher, South Paris, ME US
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20150141103 | TOPIC RELATED PHRASE GAME - The techniques described herein determine a game topic for a phrase game. Players of the phrase game may take turns submitting a phrase to a game board to earn a turn score (e.g., points or other form of value) which is added to a total, running game score. A submitted phrase played may be determined to be associated with the game topic determined for the phrase game. For instance, the game topic may include a topic phrase list that lists a plurality of phrases individually assigned a value based on an association between a phrase and the game topic. The assigned value provides an adjustment for a player turn score. For instance, the value may comprise bonus points added to regular turn points that result from the player turn score. Or, the value may be a bonus multiplier that multiplies (e.g., doubles, triples, etc.) the regular turn points. | 05-21-2015 |
Neil Gallagher, Basel CH
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20120289528 | METHOD OF TREATING PROLIFERATIVE DISORDERS AND OTHER PATHOLOGICAL CONDITIONS MEDIATED BY BCR-ABL, C-KIT, DDR1, DDR2 OR PDGF-R KINASE ACTIVITY - The present invention relates to a regimen for the administration of a pyrimidylaminobenzamide of formula I | 11-15-2012 |
Niall Gallagher, Cambridge CA
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20080301930 | Apparatus for Manufacture of electronic Assemblies - A electronic apparatus manufacturing cell defining an electronic apparatus manufacturing cell envelope having a first side and having a second side opposite the first side. According to one aspect, the electronic apparatus manufacturing cell comprises an infeed conveyor, a pass conveyor and a reject conveyor. The infeed conveyor extends from a point outside of the electronic apparatus manufacturing cell envelope on the first side to a point inside of the envelope. The pass conveyor extends from a point inside the electronic apparatus manufacturing cell envelope to a point outside of the electronic apparatus manufacturing cell envelope on the second side. The reject conveyor extends from a point inside the electronic apparatus manufacturing cell envelope to a point outside of the electronic apparatus manufacturing cell envelope on the first side. | 12-11-2008 |
20090121020 | COMBINED BATTERY AND SMART CARD - An apparatus for seating within a battery compartment and a smart card compartment of a device, including a battery component and a smart card component. The battery component is coupled to the smart card component. The smart card component is configured to seat within a smart card compartment of a device. The apparatus is configured to be inserted into a smart card compartment of a smart card containing device substantially simultaneously with the insertion of the battery component into a battery compartment of the device. The smart card component may be a test smart card, and the battery component may be a battery emulator. | 05-14-2009 |
Patricia E. Gallagher, Lewisville, NC US
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20140296143 | Angiotensin-(1-7) As A Chemoprevention Agent - Disclosed is the use of angiotensin-(1-7) peptide as an anti-cancer and chemoprevention therapeutic. Embodiments of the present invention comprise methods and compositions to prevent cancer or to reduce the risk of cancer in an individual comprising administering to the individual a pharmaceutically effective amount of an agonist for the angiotensin-(1-7) receptor to inhibit at least one of formation of a tumor (tumorigenesis), the proliferation of tumor cells, the growth of tumor cells, or metastasis of tumor cells in the individual. Cancers treated using the methods and compositions described herein may include cancers having an angiotensin-(1-7) receptor, including, but not limited to, breast cancer, colon cancer, glioblastoma, and lung cancer. | 10-02-2014 |
Penny Ellen Gallagher, Windsor CA
Peter M. Gallagher, Fishers, IN US
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20140020147 | WELDING HELMET - A welding helmet comprises a face cover, a first pane and a second pane. The face cover comprises a panel extending across an entire face of a person. The first pane comprises auto darkening material supported by the face cover panel so as to extend in a first flat plane. A second pane comprises auto darkening material supported by the face cover panel so as to extend in a second flat plane oblique to the first flat plane. | 01-23-2014 |
Phil Gallagher, Petaling Jaya MY
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20150114996 | BULK STORAGE CONTAINER AND BULK MATERIAL HANDLING ASSEMBLY THEREWITH - An intermediate bulk storage container for the storage or transport of particulate catalyst material includes a vessel having an inner wall defining a containment volume for particulate catalyst material. The vessel has a cylindrical wall section, a top panel closing the upper end of the cylindrical wall section and a conical base section connected to and tapering inwardly away from the lower end of the cylindrical wall section. An opening in the top panel of the container receives the catalyst material and a closure member closes the opening. An air tight seal is formed when the opening is closed by the closure member. A gas duct is in fluid connection with the vessel for supplying an inert gas to the sealed container or removing gas from the vessel to place the container under a vacuum. The gas duct is closed by a valve for transit or storage. | 04-30-2015 |
Robert L. Gallagher, Weston, FL US
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20150273544 | Process For Soil Remediation - A method of remediating a contaminant from soil is provided. According to the present method, clean (uncontaminated) soil is mixed with contaminated soil in a ratio that provides for remediation of the contaminant. The soil mixing method utilizes soil vibration and water as a hydraulic medium to achieve mixing of the clean and contaminated soil such that the contaminated soil is distributed homogeneously throughout the mixed soil to bring the level of contamination of the soil contaminant to within an acceptable level. | 10-01-2015 |
Ronald Gallagher, Atwell AU
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20090016954 | AGGLOMERATION OF ALUMINA AND BINDER THEREFOR - A method for the agglomeration of alumina particles, the method comprising the steps of comminuting a plurality of alumina particles having a soda content of less than approximately 0.4% by weight to a D | 01-15-2009 |
Sam Gallagher, Western Australia AU
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20100048450 | Sumoylation Control Agent and Uses Thereof - The present invention relates to novel agents that are useful for controlling sumoylation. In particular, the present invention relates to a sumoylation control agent comprising: (i) a pharmaceutically-effective amount of a HLS-5 polypeptide, isoform thereof, functional fragment thereof, or pharmaceutical composition thereof; or (ii) a compound or composition capable of modulating the endogenous levels of HLS-5 or its activity; or (iii) combinations thereof. | 02-25-2010 |
Sam Gallagher, Woodlands AU
Patent application number | Description | Published |
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20130330738 | Sumoylation Control Agent and Uses Thereof - The present invention relates to novel agents that are useful for controlling sumoylation. In particular, the present invention relates to a sumoylation control agent comprising: (i) a pharmaceutically-effective amount of a HLS-5 polypeptide, isoform thereof, functional fragment thereof, or a pharmaceutical composition thereof; or (ii) a compound or composition capable of modulating the endogenous levels of HLS-5 or its activity; or (iii) combinations thereof. | 12-12-2013 |
Shannon K. Gallagher, Lakewood, OH US
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20150050066 | MARKER WITH DECORATIVE FLUID SLEEVE - A dual chamber container includes an inner hollow body containing a marker fluid which is adapted to be dispensed. The inner hollow body is at least partially surrounded by an outer hollow body containing a decorative fluid which is retained in the container as the marker fluid is dispensed. | 02-19-2015 |
Shawn Gallagher, Melbourne, FL US
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20140206303 | SYSTEM AND METHOD OF TRANSMITTING DATA FROM AN AIRCRAFT - A system and method of transmitting data from an aircraft includes a PC card that acquires aircraft data and transmits the aircraft data over a radio frequency communications signal into the skin of the aircraft, which radiates the radio frequency communications signal to a location remote from the aircraft. | 07-24-2014 |
Shawn H. Gallagher, Melbourne, FL US
Patent application number | Description | Published |
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20150363981 | SYSTEM AND METHOD OF TRANSMITTING DATA FROM AN AIRCRAFT - A system for transmitting aircraft data from an aircraft includes a Data Acquisition Unit (DAU) that records aircraft data. A PC card is interfaced to the DAU and stores the aircraft data from the DAU. A processor retrieves aircraft data from the memory. A first wireless transceiver is controlled by the processor and receives and transmits the aircraft data along a wireless communications signal. A wireless local area network (LAN) communications unit is configured as an access point and positioned within the aircraft and transmits and receives wireless communications signals to and from the PC card. A second wireless transceiver is mounted within the aircraft and receives the wireless communications signal from the wireless LAN communications unit for transmitting the aircraft data from the aircraft. | 12-17-2015 |
Sheryl Suzanne Gallagher, Rotorua NZ
Patent application number | Description | Published |
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20100058607 | Wood drying - A process for removing water and solutes from the lumens of green wood, while leaving the cell walls throughout the wood uniformly fully swollen, comprises subjecting the green wood to supercritical carbon dioxide. | 03-11-2010 |
20140041248 | WOOD DRYING - A process for removing water and solutes from the lumens of green wood, while leaving the cell walls throughout the wood uniformally fully swollen, comprises subjecting the green wood to supercritical carbon dioxide. | 02-13-2014 |
Stephen William Gallagher, Bloomfield Hills, MI US
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20140123495 | BONDING OF ROOF PANELS - A method for attaching a roof panel to a roof rail of a vehicle bodyside frame, wherein the roof rail prohibiting access to an underside of an area at which the roof panel attaches to the roof panel, can include applying a single-component adhesive to a roof rail or to a portion of a roof panel that rests on the roof rail, placing the roof panel onto the roof rail, attaching the roof panel to the roof rail using single-sided spot welds, and heating the roof panel and vehicle bodyside frame to a temperature that cures the single-component adhesive. | 05-08-2014 |
20150375806 | CAST LOAD STRUCTURE FOR VEHICLE BODY TO FRAME MOUNT - A mounting member for securing a vehicle body to a chassis frame includes a horizontal base wall defining a mounting hole used to assemble the body to a receptacle on the frame. The mounting member further includes a plurality of side walls extending from the base wall to connect to a floor panel of the vehicle body. A boss protrudes from the base wall to the floor panel and includes a bore aligned with the mounting hole. The mounting member also includes at least one gusset extending from the boss to the base wall. The base wall, side walls, boss, and the at least one gusset are integrally formed as a single unitary body. | 12-31-2015 |
Stuart John Gallagher, Leichhardt AU
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20150283136 | PHARMACEUTICAL COMBINATION COMPRISING A B-RAF INHIBITOR AND A HISTONE DEACETYLASE INHIBITOR AND THEIR USE IN THE TREATMENT OF PROLIFERATIVE DISEASES - A pharmaceutical combination comprising (a) a B-Raf inhibitor and (b) a histone deacetylase inhibitor; the uses of such combination in the treatment of proliferative diseases; and methods of treating a subject suffering from a proliferative disease comprising administering a therapeutically effective amount of such combination. | 10-08-2015 |
Tara M. Gallagher, Bay Village, OH US
Thomas P. Gallagher, Belle Mead, NJ US
Patent application number | Description | Published |
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20150058195 | SYSTEM AND METHOD FOR MONITORING AN EQUITY RIGHTS TRANSACTION FOR STRATEGIC INVESTORS IN A SECURITIES EXCHANGE - A system and method for monitoring an equity rights transaction for strategic investors in a securities exchange. More specifically, a technological infrastructure which monitors an equity rights program in which units representing the right to acquire equity in an exchange or an exchange's parent holding company are issued to a participating member in exchange for a cash payment and the achievement of certain volume thresholds on the exchange over a specified period. | 02-26-2015 |
Thomas Patrick Gallagher, Redmond, WA US
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20130198294 | DYNAMIC CROSS-SITE REQUEST FORGERY PROTECTION IN A WEB-BASED CLIENT APPLICATION - A canary value is used to validate a message from a non-web browser client application to a web server providing web services to mitigate cross-site forgery attacks. The canary value is generated by the server in party by applying a hash function to a user identifier and a time stamp. The server provides the canary value to the client application in response to receiving a message that does not have a canary or has an expired canary. The client application upon receiving an error message with a canary message will resend the prior message with the canary value present. The client application caches the canary value for subsequent messages until a new canary value is received. The canary value allows the server to ignore messages generated by the client application under control of an attacker. | 08-01-2013 |
Tim Gallagher, Highlands Ranch, CO US
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20130198075 | PROCESSING MONITOR SYSTEM AND METHOD - Systems and methods for monitoring transaction data and providing an indication regarding a performance parameter to a payment processing entity. Transaction data associated with a plurality of transactions conducted during a time interval is received. A server computer determines that the received transaction data meets a threshold. It is further determined whether a previous indication that the threshold has been met was provided to a payment processing entity, the previous indication being associated with a plurality of previous transactions conducted during a previous time interval. If the previous indication was not provided, an indication that the threshold has been met is provided to the payment processing entity, the indication including information regarding a performance parameter of the payment processing entity. | 08-01-2013 |
Timothy Gallagher, Highlands Ranch, CO US
Patent application number | Description | Published |
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20130073859 | SYSTEMS AND METHODS TO SECURE USER IDENTIFICATION - In one aspect, a computing apparatus is configured to verify a digital signature applied on a set of data received from a user device, including an user ID assigned by a partner system to uniquely identify a user of the user device among customers of the partner system, and a user device identifier identifying the user device. The digital signature is generated via applying a cryptographic one-way hash function on a combination of the set of data and a secret, shared between the computing apparatus and the partner system via a secure communication channel separate from a channel used to receive the set of data. | 03-21-2013 |
20130332255 | SYSTEMS AND METHODS TO PROCESS REFERRALS BETWEEN OFFER CAMPAIGNS - In one aspect, a computing apparatus is configured with a mechanism to automate and regulate referrals across multiple programs, such as offer campaigns, loyalty programs, coupon programs, etc. The specification of a first program is configured with the identification of referral opportunities that correspond to activities of users in the first program. A set of selection criteria can be used to select a subset of users engaging in the respective activities. The subset of users is provided with the offer from the second program. If a user accepts the offer, the data about the user in the first program is used to automate the enrollment of the user in the second program. The second program may be configured with referral configuration parameters to match with the referral opportunities provided by other programs, if the second program is also hosted on the computing apparatus. | 12-12-2013 |
20140359298 | SYSTEMS AND METHODS TO SECURE USER IDENTIFICATION - A computing apparatus configured to verify a digital signature applied on a set of data received from a user device, including a user ID assigned by a partner system to uniquely identify a user of the user device among customers of the partner system, and a user device identifier identifying the user device. The digital signature is generated via applying a cryptographic one-way hash function on a combination of the set of data and a secret, shared between the computing apparatus and the partner system via a secure communication channel separate from a channel used to receive the set of data. | 12-04-2014 |
Timothy P. Gallagher, Granite Falls, WA US
Patent application number | Description | Published |
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20150108283 | Wingtip Control System - A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip. | 04-23-2015 |
Timothy S. Gallagher, Lumberton, NJ US
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20140048284 | Drill Rod Break-Out Wrench and Method of Use - A drill rod break-out wrench is utilized to disengage and remove drill rods from a drill string. The wrench has a lower body section with a flat, cut-out cavity configured to receive the upper end of the topmost drill rod in a drill string. The upper body section of the wrench is configured to be connected to the drill head. Rotation of the drill head rotates the wrench and the drill rod located within the wrench to threadably disengage the drill rod from the adjacent drill rod below. | 02-20-2014 |
Warren Gallagher, Richmond CA
Patent application number | Description | Published |
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20090024674 | AUTOMATIC FILE VERSIONING - A method and system are provided to automatically and transparently version files across many desktop applications without requiring the user to take specific action to cause the versioning to occur. Previous versions and versioning information can both be stored using hard links, and the versioning information can be used to determine a version history for a file. Embodiments of the present invention do not require applications to be modified to support this versioning method. Further, using one approach, the application does not even know that the versioning is occurring. The present invention provides an automatic versioning solution that is completely transparent to the user, which causes overwrite operations to be seamlessly co-opted into versioning operations which retain previous document versions instead of overwriting them. | 01-22-2009 |
20090049108 | METHOD AND APPARATUS FOR WORKFLOW VERSIONING - A method and system are provided for automatic workflow versioning. A workflow database can include metadata describing the relationships between data files, a workflow association and version/timestamp information such that relationships can be tracked against time and file versions. A system is provided to visualize a workflow and how it changes over time. A workflow navigator can be provided to allow a user to graphically “slide” back and forth in time between different workflow versions or points. Date/Time stamp information can be displayed and the workflow relationships and graphical thumbnails can change as the user hits dates/times where changes occurred. Further controls can be provided that allow the user to choose a previous version of a workflow from the timeline, and to bring forward in time the associated files and relationship information. | 02-19-2009 |
Wayne J. Gallagher, Flemington, NJ US
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20140249281 | METHOD FOR PREPARATION OF PLATINUM-CARBONYL-SILOXANE COMPOUNDS - The invention relates to a method for preparation of platinum siloxane compounds containing at least one CO ligand molecule (Pt carbonyl siloxanes). The method comprises reacting gaseous carbon monoxide (CO) with a platinum siloxane compound, preferably a platinum vinyl-cyclosiloxane compound, in solution with an organic solvent. The method is straightforward and applicable to industrial scale. With this method, specific isomers of platinum carbonyl vinylcyclosiloxanes are prepared, in which the two η-2-ethenyl groups coordinated to the Pt atom are bonded in trans-configuration relative to the cyclosiloxane backbone. The Pt compounds obtained by the method are used as catalysts for hydrosilylation and for crosslinking and curing of siloxanes and silanes. | 09-04-2014 |
William P. Gallagher, Clarksburg, NJ US
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20160060252 | 5-METHYLURIDINE METHOD FOR PRODUCING FESTINAVIR - The NRTI compound festinavir is made using 5-methyluridine as a starting material, followed by Claisen rearrangement. | 03-03-2016 |