Scott Richard
Scott Richard Baker, Greenville, SC US
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20140260312 | SYSTEMS AND METHODS FOR GAS TURBINE TUNING AND CONTROL - A method of tuning a gas turbine includes receiving a first plurality of operating parameters as the gas turbine engine is operated at a first operating state. Further, the method includes operating the gas turbine engine at a second operating state to measure a second plurality of operating parameters at the second operating state. In addition, the method includes operating the gas turbine engine at a third operating state to measure a third plurality of operating parameters at the third operating state, wherein the first, second, and third operating states are different from each other. Additionally, the method includes generating a correction factor based on the first, second, and third plurality of operating parameters. The method also includes adjusting the operation of the gas turbine engine based on the correction factor. | 09-18-2014 |
Scott Richard Breimon, Delano, MN US
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20110150034 | Sanitary clean in place thermowell - A resistance temperature detector (RTD) assembly ( | 06-23-2011 |
20130019701 | Sanitary clean in place microwave probe and sealing gasket assembly - A process seal ( | 01-24-2013 |
20130027059 | Microwave reference block assembly - A test waveguide ( | 01-31-2013 |
Scott Richard Dobert, Dearborn, MI US
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20090301071 | LOW RESTRICTION HYDROCARBON TRAP ASSEMBLY - A hydrocarbon adsorption assembly for an air induction system is disclosed. The hydrocarbon adsorption assembly includes a fluid conduit having an outer surface and a spaced apart inner surface to form a fluid path therein, the conduit including a recessed area formed in the inner surface thereof. A hydrocarbon trap is disposed in the recessed area of the fluid conduit to adsorb hydrocarbons passing through the conduit. The recessed area and the hydrocarbon trap cooperate to cause a portion of an air flowing through the flow path of the conduit to flow through the hydrocarbon trap to facilitate a purging thereof. | 12-10-2009 |
Scott Richard Gremmert, Redmond, WA US
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20140067171 | SYSTEMS AND METHODS FOR GRAPHICALLY INDICATING AIRCRAFT ASCENT AND DESCENT CAPABILITIES - Systems and methods are operable to present graphical information indicating capability of an aircraft to change altitude. An exemplary embodiment determines an altitude change capability of the aircraft; determines an altitude change capability icon based on the determined altitude change capability of the aircraft, wherein the altitude change capability icon is defined by at least a leading portion, a trailing portion, a top portion, and a bottom portion, wherein a slope of the leading portion of the altitude change capability icon corresponds to the determined altitude change capability of the aircraft, and wherein the leading portion and the trailing portion are separated by at least the top portion and the bottom portion; and communicates the altitude change capability icon to a display for presentation to the crew of the aircraft. | 03-06-2014 |
20150348421 | SYSTEMS AND METHODS FOR IN-TRAIL OPPORTUNITY WINDOW ESTIMATOR - Systems and methods are operable to identify and indicate opportunities for an In-Trail procedure (ITP) aircraft to make an ITP altitude change. An exemplary embodiment receives information corresponding to a desired ITP altitude for the ITP aircraft and a projected window period; estimates at least one ITP maneuver opportunity window based on the estimated location of each of the plurality of other aircraft and based on a current airspeed and a current altitude of the ITP aircraft; generates a screen shot that presents an ITP maneuver opportunity window icon, wherein the ITP maneuver opportunity window icon graphically indicates the soonest time and the latest time that the ITP aircraft may initiate the ITP maneuver, and wherein the ITP maneuver opportunity window icon indicates an altitude change made by the ITP aircraft will maintain minimum safe self-separation distances from the plurality of other aircraft during the ITP maneuver. | 12-03-2015 |
Scott Richard Johnson, Troy, NY US
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20140291276 | SEPTA - A system includes a cap having an opening, and a septum configured to engage with the cap. The septum includes a first portion having a first width, and a second portion having a second width smaller than the first width. The second portion is sized and shaped to be received by the opening of the cap. | 10-02-2014 |
Scott Richard Mattix, Kimberly CA
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20140360483 | HEIGHT ADJUSTABLE FIRE PIT GRATE ASSEMBLY WHOLLY CARRIED BY A FIRE PIT RING - A grate assembly for use over a fire, surrounded by a cylindrical fire pit ring, comprising: a) an inverted U shaped clamp having an inner and an outer opposite side, a central portion extending between, and connecting the two opposite side portions, wherein the outer opposite side portion further comprises a centrally positioned screwed hole and a screw, to tighten the clamp on the fire pit ring, an end portion of the central portion also has a centrally positioned screwed hole and a screw, to level the clamp when it is seated on the cylindrical fire pit ring; b) an upwardly extending post attached to the clamp; and, c) a grate, surrounded by a frame, said frame attached to, a cylindrical tube, sized to closely fit over the post, and further comprising grate-post attachment means to clamp the grate to the post at a preferred height. | 12-11-2014 |
Scott Richard Myers, La Mirada, CA US
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20150361831 | SYSTEM AND METHOD FOR THERMAL MANAGEMENT - A system includes a first unit. The first unit includes a condenser configured to condense a working fluid circulating in a Rankine cycle. The Rankine cycle includes an evaporator configured to evaporate the working fluid by absorbing heat from a heating fluid circulated in a heating fluid circuit. The first unit also includes a heat exchanger configured to transfer heat from a heat source to the heating fluid. The first unit further includes a driving pump configured to provide a driving force for circulating the heating fluid in the heating fluid circuit. The first unit still includes a common support structure. The condenser, the heat exchanger, and the driving pump are mounted on the common support structure. | 12-17-2015 |
Scott Richard Myers, La Miranda, CA US
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20150315935 | SYSTEM AND METHOD FOR INDUCTOR COOLING - A system includes a cooling system. The cooling system includes a Rankine cycle and an inductor coupled to the cooling system. The inductor generates heat when in operation. The Rankine cycle circulates a working fluid when in operation, and the working fluid is configured to cool the inductor and to facilitate absorbing heat generated by the inductor. | 11-05-2015 |
Scott Richard Pribyl, Overland Park, KS US
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20130211856 | SYSTEMS AND METHODS FOR GENERATING OUTCOME MEASURES - Systems and methods for automatic generation of one or more outcome measures are disclosed. The outcome measures may be displayed as a single one page summary, which may be provided to a specialty physician or other medical professionals. Additionally, the outcome measures summary may be reviewed independently, and/or integrated with existing electronic medical reports, and may be used to initiate other medical activities, such as e-prescriptions and/or medical insurance authorization. | 08-15-2013 |
Scott Richard Schuricht, Edwards, IL US
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20080238607 | Fan speed control system - A fan speed control system for a machine is disclosed. The control system may include a fan to provide a flow of coolant to the machine. The system may further include a first sensor configured to generate a first signal indicative of an operational parameter of the machine, a second sensor associated with the fan to generate a second signal indicative of an actual speed of the fan, and a controller communicatively coupled to the fan, the first sensor, and the second sensor. The controller may be configured to generate a third signal indicative of a desired fan speed based on the first signal, and a fourth signal indicative of a difference between the desired fan speed and the actual fan speed. The controller may drive the fan based on the third signal and the fourth signal. | 10-02-2008 |
Scott Richard Zearbaugh, Milford, OH US
Patent application number | Description | Published |
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20100013220 | EXTRUSION RESISTANT GASKET FACE SEAL - A seal assembly for a fluid coupling includes: (a) a generally planar, substantially rigid seal retainer with opposed first and second faces, having an annular first groove formed in the first face; (b) a first resilient seal disposed in the first groove; and (c) an annular first backup ring positioned radially outboard of the first resilient seal and secured to the first resilient seal, wherein the first backup ring is substantially harder than the first resilient seal. | 01-21-2010 |