Garrett, GB
Andrew J. Garrett, Abbots Langley GB
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20080209444 | METHOD, SYSTEM AND PROGRAM PRODUCT FOR DEFINING IMPORTS INTO AND EXPORTS OUT FROM A DATABASE SYSTEM USING SPREAD SHEETS BY USE OF A CONTROL LANGUAGE - The present invention provides a vehicle for the exchange of data between a database and an independent spreadsheet. Specifically, the present invention may be used to import data from a database to a spreadsheet and/or to export data to a spreadsheet. To facilitate this exchange, one or more controls are entered into cells in the spreadsheet. The controls specify the manner in which the data is exchanged between the database and the spreadsheet. For example, a control may specify a data type, a formatting parameter, a source field, a destination field, and/or a formula for a designated cell in the spreadsheet. The controls are executed by a linker that links the data in the database and the data in the spreadsheet to effect the exchange of data between the two. | 08-28-2008 |
Andrew J. Garrett, Kings Langley GB
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20130132354 | MULTIPLE SOURCE DATA MANAGEMENT USING A CONFLICT RULE - A solution for managing data received from multiple sources is provided. In particular, when conflicting data values are received from multiple sources for a data element, a conflict rule is used to determine the main data value for the data element, which is subsequently stored for use. The conflict rule can define any automatic, semi-automatic, or manual procedure for resolving the conflict. The conflict rule, or an identifier thereof, can be stored with each data value and the main data value for the data element. | 05-23-2013 |
Andrew James Garrett, London GB
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20160037231 | DATA COMMUNICATIONS - Embodiments herein provide systems and methods for sending broadband data to end-users over a DTTV broadcast transmission. Systems and methods for receiving such data are also described. A wireless overlay system is set up by an Internet Service Provider/Communications Provider (ISP/CP) 11 by means of receiving from end-user equipment 27 data requests over a DSL uplink together with identification of at least one DTTV transmitter 21 23. The ISP/CP 11 provides an overlay controller 26 which causes routing of the requested data over a selected DTTV transmitter 21. At the end-user equipment, the requested data can be received from the DTTV broadcast and extracted for output. | 02-04-2016 |
Andrew Ronald Garrett, Hertfordshire GB
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20130333326 | TRANSPORTATION BASE LOAD UNITIZER - A transportation base load unitizer ( | 12-19-2013 |
Brian Garrett, Newton Abbott GB
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20110091204 | METHOD AND SYSTEM FOR DEPLOYING AN OPTICAL DEMODULATOR ARRANGEMENT IN A COMMUNICATIONS NETWORK - The present application describes methods and systems for use in a communications network. More specifically, a method of deploying an optical demodulator arrangement having at least one interferometer in a network that transmits an optical signal is provided. The optical signal may include one or more on-off-keyed signals and one or more DMPSK signals. In some embodiments, the DMPSK signal is a DQPSK signal. The network may include one or more of fiber spans carrying the signals. The interferometer may have a first optical path and a second optical path and a time delay is formed between the first and second optical paths. The method may involve determining a cross-talk penalty that results from cross-phase modulation between the channels, and determining a time delay value for the interferometer. The time delay value may be determined based at least in part on determined the cross-talk penalty. | 04-21-2011 |
Graham Samuel Garrett, County Down GB
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20090069494 | Polymer material - A process is described for providing a polymer material by blending as a first component one or more hydrophilic polymers, and as a second component one or more neutralising chemicals, in the complete or substantial absence of water. In the absence of water, the components will not be aqueous solutions. Thus the components can be used in blending processes, and the present invention is able to form many other shapes and forms of material other than laminates on substrates. | 03-12-2009 |
Lisa Marie Garrett, Swindon GB
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20140271722 | ALLERGEN DOSAGE FORM - The invention provides allergen containing pharmaceutical products and in particular fast-dispersing solid allergen dosage forms. In particular, fast-dispersing, non-compressed solid dosage forms suitable for oromucosal administration comprising a matrix and at least one allergen are provided. Suitable matrices are gelatine, starch and mannitol. Methods for the dosage forms are also provided. | 09-18-2014 |
Michael Garrett, Woking GB
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20080262370 | Gas sensor - A method of determining the respiratory function of a subject is disclosed, the method comprising measuring the concentration of water vapour in the gas stream exhaled by the subject, and from the measured water vapour concentration determining the respiratory function of the subject. Mathematical techniques for analyzing the data obtained from the measurement of concentrations of gaseous components in an exhaled gas stream are also disclosed and their use in determining the lung function of a subject. | 10-23-2008 |
20150377821 | Gas Sensor - A sensor for sensing a target substance in a target substance is provided, the sensor comprising: a sensing element disposed to be exposed to the gas stream, the sensing element comprising: a working electrode; a counter electrode; and a layer of ion exchange material extending between the working electrode and the counter-electrode; whereby contact of the ion exchange layer with the gas stream firms an electrical contact between the working and counter electrodes. | 12-31-2015 |
Michael Garrett, Surry GB
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20100050735 | Gas Sensor - A sensor for sensing a target substance in a gas stream is provided, the sensor comprising: a sensing element disposed to be exposed to the gas stream, the sensing element comprising: a working electrode; a counter electrode; and a layer of ion exchange material extending between the working electrode and the counter electrode; whereby contact of the ion exchange layer with the gas stream forms an electrical contact between the working and counter electrodes. | 03-04-2010 |
Michael Garrett, Wokug GB
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20120165693 | Detection of Respiratory System Lesions - Humidity profiles of exhaled air of individuals obtained using a sensor to detect water vapour content or temperature versus time of exhalation may exhibit an irregularity indicative of a space-occupying respiratory system lesion. Detection of such irregularities provides an inexpensive and rapid means of pre-screening individuals for lung cancer diagnosis, and is applicable even to individuals with other respiratory disorders such as asthma and COPD. | 06-28-2012 |
Michael Ernest Garrett, Woking GB
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20100000064 | Method for manufacturing a product dispensing canister - A method for manufacturing a canister from which product is to be dispensed by a dispensing system comprising a solid/gas arrangement in which the gas is adsorbed on to the solid under pressure and desorbed therefrom when the pressure is released the solid comprises an adsorbent for the gas, the container being sealed and having valve for dispensing the product. The method includes filling the canister with the gas by applying a pressure of gas to the adsorbent via an aperture in the canister and sealing the canister the size of the aperture and the applied pressure being controlled such that sufficient gas is allowed freely to contact the adsorbent and achieve a pre-determined pressure in the sealed canister. | 01-07-2010 |
20110288430 | Gas Sensor - A sensor and method for detecting a target substance, particularly CO | 11-24-2011 |
Michael Ernest Garrett, Wiking GB
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20140048566 | METHOD OF MANUFACTURING A PRODUCT DISPENSING SYSTEM - In a method of manufacturing a dispensing system for dispensing a product from a canister, comprising a solid/gas arrangement in which the gas is adsorbed onto the solid under pressure and desorbed therefrom when the pressure is released and in which the solid comprises activated carbon and the gas comprises at least one of nitrogen, oxygen or mixtures thereof including air, carbon dioxide, nitrous oxide and argon, the canister having valve means to allow the gas adsorbed onto the carbon to be desorbed for generating a pressure in the canister and effect product dispense, the activated carbon is held from the time of its production up to its installation in the canister under a blanketing gas atmosphere which does not prevent the gas to be adsorbed from occupying the adsorption sites of the activated carbon in the canister. | 02-20-2014 |
Michelle Dawn Garrett, Sutton GB
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20090082370 | Pharmaceutical Combinations of PK Inhibitors and Other Active Agents - The invention provides a combination for use as a protein kinase B inhibitor, the combination comprising (or consisting essentially of) an ancillary compound and: (I) a compound of the formula: or salts, solvates, tautomers or N-oxides thereof, wherein R | 03-26-2009 |
20100130464 | PHARMACEUTICAL COMPOUNDS - The invention provides compounds of the formula (I) having ROCK kinase and/or protein kinase p70S6K inhibiting activity: wherein A is a saturated hydrocarbon linker group containing from 1 to 7 carbon atoms, the linker group having a maximum chain length of 5 atoms extending between R1 and NR | 05-27-2010 |
20100166699 | PHARMACEUTICAL COMBINATIONS COMPRISING PYRAZOLE DERIVATIVES AS PROTEIN KINASE MODULATORS - The invention provides a combination comprising an ancillary compound (e.g. one, two or more ancillary compounds) and a compound of the formula (I) having protein kinase B inhibiting activity: wherein A is a saturated hydrocarbon linker group containing from 1 to 7 carbon atoms, the linker group having a maximum chain length of 5 atoms extending between R | 07-01-2010 |
20150126471 | 5-[[4-[[MORPHOLIN-2-YL]METHYLAMINO]-5-(TRIFLUOROMETHYL)-2-PYRIDYL]AMINO]PY- RAZINE-2-CARBONITRILE AND THERAPEUTIC USES THEREOF - The present invention pertains generally to the field of therapeutic compounds. More specifically the present invention pertains to 5-[[4-[[morpholin-2-yl]methylamino]-5-(trifluoromethyl)-2-pyridyl]amino]pyrazine-2-carbonitrile compounds (referred to herein as “TFM compounds”) which, inter alia, inhibit Checkpoint Kinase 1 (CHK1) kinase function. The present invention also pertains to pharmaceutical compositions comprising such compounds, and the use of such compounds and compositions, both in vitro and in vivo, to inhibit CHK1 kinase function, and in the treatment of diseases and conditions that are mediated by CHK1, that are ameliorated by the inhibition of CHK1 kinase function, etc., including proliferative conditions such as cancer, etc., optionally in combination with another agent, for example, (a) a DNA topoisomerase I or II inhibitor; (b) a DNA damaging agent; (c) an antimetabolite or a thymidylate synthase (TS) inhibitor; (d) a microtubule targeted agent; (e) ionising radiation; (f) an inhibitor of a mitosis regulator or a mitotic checkpoint regulator; (g) an inhibitor of a DNA damage signal transducer; or (h) an inhibitor of a DNA damage repair enzyme. | 05-07-2015 |
Owen John Garrett, Cambridge GB
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20100070625 | Supplying Data Files to Requesting Stations - Data files are supplied to a plurality of requesting stations ( | 03-18-2010 |
Owen John Garrett, Wilburton GB
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20130103854 | ROUTING NETWORK TRAFFIC - A traffic manager ( | 04-25-2013 |
Owen John Garrett, Ely GB
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20110040889 | MANAGING CLIENT REQUESTS FOR DATA - Network traffic is distributed between a plurality of networked computers. The traffic comprises requests that are received into the network and replicated to each computer. For each request, each computer makes a decision based on attributes of the request as to whether to process or ignore the request, such that each request is processed by only one computer. Each computer periodically broadcasts a signal to each of the other computers to confirm that it is online. When a first computer is no longer online, the traffic is redistributed amongst the remaining online computers, wherein traffic that is already processed by the remaining computers is not redistributed, traffic that would have been processed by the first computer is split evenly between the remaining computers, and each computer decides independently and identically how to redistribute the traffic without communicating with the other computers. | 02-17-2011 |
Sasha Louise Garrett, Cambridge GB
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20100087428 | Novel Potassium Channel Blockers - The present invention provides a compound of formula (I) | 04-08-2010 |
20140221337 | Potassium Channel Blockers - The present invention provides a compound of formula (I) | 08-07-2014 |
20150259282 | Potassium Channel Blockers - The present invention provides a compound of formula (I) | 09-17-2015 |
Shaun Garrett, Wirral GB
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20150118100 | Film Deposition Using Precursors Containing Amidoimine Ligands - Methods are provided for deposition of films comprising manganese on surfaces using metal coordination complexes comprising an amidoimino-based ligand. Certain methods comprise exposing a substrate surface to a manganese precursor, and exposing the substrate surface to a co-reagent. | 04-30-2015 |
Simon John Garrett, Hertfordshire GB
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20130333326 | TRANSPORTATION BASE LOAD UNITIZER - A transportation base load unitizer ( | 12-19-2013 |
Stephen Garrett, Huddersfield GB
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20090249786 | Turbomachine system and turbine therefor - A turbomachine system comprises a first turbocharger comprising an exhaust gas flow first turbine for location in an exhaust path and a first compressor driven by said first turbine; a turbomachine for location in the exhaust path upstream or downstream of said first turbocharger and comprising an exhaust gas flow second turbine and a second compressor driven by said second turbine. The first turbine has an outlet that is in fluid communication with an inlet of the second turbine. One of said first and second turbines is a radial outflow turbine. The arrangement provides for a relatively compact package. The radial outflow turbine may have a particular structure in which there is provided a deflector member at or near its inlet for directing the gas outwards, a stator for introducing swirl and a downstream turbine rotor. A shroud is fixed to blades of the turbine rotor to prevent leakage and to provide additional structural rigidity. | 10-08-2009 |
20100143099 | TURBOCHARGER - A turbocharger comprises a turbine wheel ( | 06-10-2010 |
20110011085 | VARIABLE GEOMETRY TURBINE WITH WASTEGATE - A variable geometry turbine comprises a turbine wheel ( | 01-20-2011 |
20110027073 | VARIABLE GEOMETRY TURBINE - A variable geometry turbine comprises: a turbine wheel mounted within a housing assembly for rotation about a turbine axis, the housing assembly defining a radial gas flow inlet passage; an annular wall member defining one wall of the inlet passage and which is displaceable in a direction substantially parallel to the turbine axis to control gas flow through the inlet passage; and a linkage mechanism comprising at least one actuating member operably connected to the annular wall member to control displacement of the wall member. The actuating member extends in a direction substantially parallel to the turbine axis through an aperture defined by a retaining member such that a first bearing surface defined by the actuating member extending transverse to the turbine axis is contacted by a surface of the retaining member so as to connect the actuating member to the annular wall member. The aperture is appropriately dimensioned to define a clearance between a wall of the aperture and a portion of the actuating member located within the aperture so as to accommodate displacement of the retaining member, resulting from displacement of the annular wall member, relative to the actuating member. | 02-03-2011 |
20130315718 | TURBOMACHINE - A variable geometry turbine comprising a turbine wheel mounted for rotation about a turbine axis within a housing. The housing defines an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls. The turbine further comprises a cylindrical sleeve that is axially movable across the annular inlet to vary the size of a gas flow path through the inlet. The annular inlet is divided into at least two axially offset inlet passages. The inner diameter of the sleeve is greater than the inner diameter of the inlet passages. | 11-28-2013 |
20140147255 | VARIABLE GEOMETRY TURBINE - A variable geometry turbine comprises: a turbine wheel in a housing assembly defining a radial gas flow inlet passage; an annular wall member which is displaceable to control gas flow through the inlet passage; and a linkage mechanism comprising at least one actuating member operably connected to the annular wall member to control displacement of the wall member. The actuating member has a terminal portion defining a radially extending flange and extends in a direction substantially parallel to the turbine axis through an aperture defined by a retaining member to locate the radially extending flange in between said retaining member and annular wall member. The terminal portion is contacted by the retaining member to connect the actuating member to the annular wall member. The aperture defines a clearance to accommodate displacement of the retaining member relative to the actuating member. | 05-29-2014 |
Stephen Garrett, Highburton GB
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20120114464 | VARIABLE GEOMETRY TURBINE AND ASSEMBLY THEREOF - A variable geometry turbine has a housing for receipt of the turbine wheel. A gas flow control mechanism in the housing upstream of said turbine wheel is operable to control gas flow through a gas flow inlet passage. The control mechanism has a movable nozzle ring or shroud for varying the size of the gas flow inlet passage. A transmission mechanism for connection between an actuator and the control mechanism converts movement applied by the actuator into movement shroud or nozzle ring. The transmission mechanism comprises a yoke having a shaft that is rotatably supported by a wall of the housing. The yoke defines arms that extend outwardly of the shaft and which engage with the shroud or nozzle ring. There is provided at least one recess defined in an inside surface of the housing, the recess extending from shaft rotation axis and configured to allow passage of an end of the yoke shaft along it during insertion of the yoke into the housing. | 05-10-2012 |
Stephen Edward Garrett, Huddersfield GB
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20110100000 | VARIABLE GEOMETRY TURBINE - A variable geometry turbine comprises a turbine wheel supported in a housing for rotation about a turbine axis. The housing defines an annular inlet passage around an inducer portion of the turbine wheel and an outlet passage including a tubular wall disposed around an exducer portion of the turbine wheel; the inlet passage is defined between first and second radial inlet surfaces, one of the inlet surfaces being defined by a moveable wall member and the other of the inlet surfaces being defined by a facing wall of said housing. The moveable wall member is moveable relative to the facing wall of the housing along the turbine axis to vary the size of the inlet passageway. The moveable wall member is displaceably mounted within an annular cavity defined between the tubular wall and a surrounding wall of the housing. | 05-05-2011 |
20110116911 | VARIABLE GEOMETRY TURBINE - A variable geometry turbine comprises a turbine wheel supported in a housing for rotation about a turbine axis. An exhaust gas inlet passageway is defined between a shroud and a wall of a nozzle ring. The shroud is moveable in the axial direction to vary the size of the inlet passageway. The nozzle ring has an array of vanes that extends across the inlet passageway. An array of openings is provided in the shroud for receipt of the array of vanes. The shroud is part of a substantially annular axially moveable sleeve that is slidably disposed on an annular supporting wall. At least one biasing member is disposed between the moveable sleeve and the support and is designed to apply a circumferentially distributed force in the radial direction so as to maintain concentric alignment of the supporting wall and the sleeve. | 05-19-2011 |
20110146271 | GAS EXPANDER SYSTEM - According to an aspect of the present invention, there is provided a gas expander system suitable for use in a turbomachine, the gas expander system comprising: a gas expander provided with a moveable part; a magnetic gear arrangement; and a shaft; the moveable part of the gas expander being connectable to a load via the magnetic gear arrangement and the shaft, and movement of the moveable part of the gas expander being arranged to cause movement of the shaft. | 06-23-2011 |
20110194929 | TURBOMACHINE - According to a first aspect of the present invention there is provided a variable geometry turbine comprising: a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions; a cylindrical sleeve axially movable across the annular inlet to vary the size of a gas flow path through the inlet; and a guide for guiding the movement of the cylindrical sleeve, the guide being at least partially located within the inlet at a radially extent of the inlet portions, and extending in an axial direction parallel to the turbine axis. | 08-11-2011 |
20120128471 | VARIABLE GEOMETRY TURBINE - A variable geometry turbine comprises a turbine wheel mounted within a housing for rotation about a turbine axis; and a gas flow control passage upstream of said turbine wheel, the gas flow control passage being defined at least in part between a radial first surface of a movable wall member and a facing wall of the housing, the movable wall member also comprising second and third surfaces which oppose the first surface. The movable wall member is movable in an axial direction so as to vary the size of the gas flow control passage. There is a first gas region of the turbine, a portion of which is upstream of the gas flow control passage, the first gas region including at least a portion of the gas flow control passage; a second gas region of the turbine downstream of the gas flow control passage which contains the turbine wheel; and a third gas region of the turbine downstream of the turbine wheel. The first gas region comprises the first and second surfaces, and the second gas region or third gas region comprises the third surface. | 05-24-2012 |
20130239569 | GAS EXPANDER SYSTEM - A gas expander system suitable for use in a turbomachine, the gas expander system comprising: a gas expander provided with a moveable part; a magnetic gear arrangement; and a shaft; the moveable part of the gas expander being connectable to a load via the magnetic gear arrangement and the shaft, and movement of the moveable part of the gas expander being arranged to cause movement of the shaft, wherein the magnetic gear arrangement is used in a closed loop heat recovery system, with the inner and outer rotors of the magnetic gear separated by a wall that contains the stator. | 09-19-2013 |
20140105730 | TURBOMACHINE - According to a first aspect of the present invention there is provided a variable geometry turbine comprising: a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions; a cylindrical sleeve axially movable across the annular inlet to vary the size of a gas flow path through the inlet; and a guide for guiding the movement of the cylindrical sleeve, the guide being at least partially located within the inlet at a radially extent of the inlet portions, and extending in an axial direction parallel to the turbine axis. | 04-17-2014 |
Stephen Edward Garrett, West Yorkshire GB
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20150345433 | ENGINE SYSTEMS AND METHODS FOR OPERATING AN ENGINE - A unique engine system has an engine with a dedicated exhaust gas recirculation cylinder, an EGR system that receives exhaust gas from the dedicated cylinder, and a turbocharger having turbine inlet ports in fluid communication with other engine cylinders via a plurality of exhaust passages. At least two of the exhaust passages are substantially isolated from each other. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for engines and engine systems. | 12-03-2015 |
Steve Garrett, Kidwelly GB
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20110283968 | OIL SUPPLY SYSTEM FOR AN ENGINE - An oil supply system for a reciprocating piston internal combustion engine is disclosed in which the supply of oil to piston cooling jets is controlled by pressure operated valves designed to open at a pre-defined valve opening pressure. The pressure of oil supplied by a pump is controlled to be below this pre-defined valve opening pressure during operation of the engine in which piston cooling is not required, and the pressure of oil is controlled to above the pre-defined valve opening pressure when piston cooling is required. The control of the pump is by an electronic control unit based upon a combination of engine speed and engine load. | 11-24-2011 |
Steve Garrett, Darlington GB
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20130179049 | METHOD AND DEVICE FOR OPERATING A LUBRICATING SYSTEM OF A COMBUSTION ENGINE - The application relates to a method for operating a lubricating system of a combustion engine in a motor vehicle, the engine having a variably controllable oil pump and a plurality of piston cooling jets. The oil pressure may be adjusted based on operating conditions to activate and de-activate the piston cooling jets when needed. | 07-11-2013 |
Steven Edward Garrett, Huddersfield GB
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20100037605 | VARIABLE GEOMETRY TURBINE - A variable geometry turbine has a gas inlet chamber and a gas flow inlet passage downstream of the inlet chamber and upstream of said turbine wheel. The inlet passage is defined between a moveable first wall and a second wall and an actuator is operable to control displacement of the first wall in order to vary the size of the gas flow inlet passage. A piston member defining the first wall or being connected to it is received in a piston chamber and serves to move the first wall as a result of displacement of the piston member in the piston chamber. A bypass passage defined in the housing and extends between the piston chamber and a location in the turbine upstream of the inlet passage for delivering gas to the piston chamber. The bypass passage is disposed such that gas introduced through the bypass passage pressurises the chamber and applies a force to displace the piston member in a direction that causes the first wall to move towards the second wall. The gas, which may be the exhaust gas from an engine, thus serves to assist the operation of the actuator. | 02-18-2010 |