Patents by Inventor Brian Varney
Brian Varney has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 10371600Abstract: An on-board diagnostic for a particle filter of a vehicle exhaust system records repeating data about flow and pressure around the particle filter. Data is recorded in virtual data bins having successive thresholds or filters within a numerical scale. Each data point is typically recorded in several bins to permit a rapid calculation of averaged data for use in the diagnostic. Sensitivity of less frequently recorded data is preserved, while giving quickly delivery of a result from the diagnostic.Type: GrantFiled: December 6, 2013Date of Patent: August 6, 2019Assignee: JAGUAR LAND ROVER LIMITEDInventor: Brian Varney
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Patent number: 9416735Abstract: A diagnostic routine momentarily forces an engine to an alternative operating condition, and at the same time adjust fuelling of the engine so as to be appropriate to the alternative operating condition (31). In one embodiment substantially unchanged exhaust constituents (32) indicate correct adoption of the alternative operating condition. In another embodiment a substantial change in a calculated measure is indicative of correct adoption of the alternative condition. The invention allows better control of undesired exhaust emissions during operation of the diagnostic.Type: GrantFiled: June 21, 2012Date of Patent: August 16, 2016Assignee: Jaguar Land Rover LimitedInventor: Brian Varney
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Patent number: 9228523Abstract: A diagnostic for identifying cylinder to cylinder air/fuel ratio faults of an engine having closed loop fuel control. Air mass flow is accumulated for a plurality of load bands on the engine load/speed map, and for each load band a rich/lean air fuel ratio is determined at a mass threshold. This threshold data is processed and compared with fixed data to determine whether any cylinder of an engine is experiencing an air/fuel ratio fault which is substantially different to the remainder.Type: GrantFiled: April 25, 2012Date of Patent: January 5, 2016Assignee: Jaguar Land Rover LimitedInventor: Brian Varney
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Publication number: 20150369700Abstract: An on-board diagnostic for a particle filter of a vehicle exhaust system records repeating data about flow and pressure around the particle filter. Data is recorded in virtual data bins having successive thresholds or filters within a numerical scale. Each data point is typically recorded in several bins to permit a rapid calculation of averaged data for use in the diagnostic. Sensitivity of less frequently recorded data is preserved, whilst giving quickly delivery of a result from the diagnostic.Type: ApplicationFiled: December 6, 2013Publication date: December 24, 2015Inventor: Brian VARNEY
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Patent number: 9188075Abstract: A momentary diagnostic for determining correct operation of a cam profile switching system of an internal combustion engine by calculation of changes in cylinder bank to bank air mass flow ratios: operating said engine in one condition of the cam profile switching system; providing for a first cylinder subset the inlet fuel flow and the corresponding oxygen content of the exhaust flow, and calculating the mass of air passing through the first cylinder subset in a defined time period; providing for a second cylinder subset the inlet fuel flow and the corresponding oxygen content of the exhaust flow; calculating the mass of air passing through the second cylinder subset in said defined time period; comparing the mass air flow the oxygen content for the first and second cylinder subsets to give a standard ratio; momentarily forcing the cam profile switching system of one of said cylinder subsets to an alternative condition; re-calculating providing the corresponding mass of air oxygen content passing through theType: GrantFiled: April 30, 2012Date of Patent: November 17, 2015Assignee: JAGUAR LAND ROVER LIMITEDInventor: Brian Varney
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Publication number: 20140343822Abstract: A diagnostic method comprising the steps of: first sampling exhaust gas; implementing a forced change of engine operating condition; second sampling exhaust gas associated with said change at a delay after initiating said change, said second sampling being at a location corresponding to said delay; and comparing said first sampling and second sampling to detect a change in exhaust constituents.Type: ApplicationFiled: May 3, 2012Publication date: November 20, 2014Inventor: Brian Varney
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Publication number: 20140202425Abstract: A diagnostic routine momentarily forces an engine to an alternative operating condition, and at the same time adjust fuelling of the engine so as to be appropriate to the alternative operating condition (31). In one embodiment substantially unchanged exhaust constituents (32) indicate correct adoption of the alternative operating condition. In another embodiment a substantial change in a calculated measure is indicative of correct adoption of the alternative condition. The invention allows better control of undesired exhaust emissions during operation of the diagnostic.Type: ApplicationFiled: June 21, 2012Publication date: July 24, 2014Applicant: Jaguar Land Rover LimitedInventor: Brian Varney
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Publication number: 20140123940Abstract: A momentary diagnostic for determining correct operation of a cam profile switching system of an internal combustion engine by calculation of changes in cylinder bank to bank air mass flow ratios: operating said engine in one condition of the cam profile switching system; providing for a first cylinder subset the inlet fuel flow and the corresponding oxygen content of the exhaust flow, and calculating the mass of air passing through the first cylinder subset in a defined time period; providing for a second cylinder subset the inlet fuel flow and the corresponding oxygen content of the exhaust flow; calculating the mass of air passing through the second cylinder subset in said defined time period; comparing the mass air flow the oxygen content for the first and second cylinder subsets to give a standard ratio; momentarily forcing the cam profile switching system of one of said cylinder subsets to an alternative condition; re-calculating providing the corresponding mass of air oxygen content passing through theType: ApplicationFiled: April 30, 2012Publication date: May 8, 2014Applicant: JAGUAR LAND ROVER LIMITEDInventor: Brian Varney
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Publication number: 20140123943Abstract: A diagnostic for identifying cylinder to cylinder air/fuel ratio faults of an engine having closed loop fuel control. Air mass flow is accumulated for a plurality of load bands on the engine load/speed map, and for each load band a rich/lean air fuel ratio is determined at a mass threshold. This threshold data is processed and compared with fixed data to determine whether any cylinder of an engine is experiencing an air/fuel ratio fault which is substantially different to the remainder.Type: ApplicationFiled: April 25, 2012Publication date: May 8, 2014Applicant: JAGUAR LAND ROVER LIMITEDInventor: Brian Varney
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Publication number: 20070113566Abstract: An electronic HEMD determines the optimum balance between gas cooling and heat exchanger pressure loss, for any given operating condition, and adjusts the gas flow rate through the exchanger accordingly, to yield the maximum net power savings (and thereby energy savings) afforded by the exchanger. Maintaining the optimum balance between cooling and exchanger pressure loss reduces the amount of energy required to transport a given volume of gas through a pipeline and thereby increases the transmission efficiency of the gas pipeline system. A method of operating a heat exchanger on a natural gas transmission pipeline using a control algorithm that in turn controls the position of a heat exchanger bypass valve.Type: ApplicationFiled: January 23, 2007Publication date: May 24, 2007Inventor: Brian Varney
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Publication number: 20070100847Abstract: Methods and structures within a SAS expander for initiating communication with one or more SAS initiators in a SAS domain to inform the initiators of sensed changes in the domain without the need for a full SAS Discovery process. In one aspect hereof, the expander may transmit a vendor unique BROADCAST primitive to inform SAS initiators that they should initiate a vendor unique SMP or SSP exchange with the expander to determine changes to the SAS domain. In another aspect hereof, the SAS initiator may respond as an SMP or SSP target device in response to initiation of vendor unique SMP or SSP exchanges by the expander. The expander may report to initiators regarding sensed changes in the domain and/or statistics regarding operation of the expander or other elements of the domain.Type: ApplicationFiled: October 31, 2005Publication date: May 3, 2007Inventors: Mark Slutz, David Uddenberg, Brian Varney
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Publication number: 20070093124Abstract: Methods and structures within a SAS expander for monitoring bandwidth utilization of a SAS wide port associated with the expander and for effecting reconfiguration of the wide port to improve SAS domain performance. In one aspect, a SAS expander may monitor utilization of a wide port of the expander. If the wide port is over-utilized, the expander may inform a SAS initiator of the need for one or more additional links to be configured in the wide port. If the wide port is under-utilized, the expander may reconfigure the wide port by disabling a link to reduce power consumption associated with that link. If the wide port is later over-utilized, a previously disabled link may be re-enabled by the expander to restore available bandwidth. Disabled links of a wide port may also be reported to a SAS initiator to be reconfigured by the initiator for use in another communication path.Type: ApplicationFiled: October 20, 2005Publication date: April 26, 2007Inventors: Brian Varney, David Uddenberg, Mark Slutz
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Publication number: 20070070885Abstract: Methods and structures within a SAS expander for detecting link level errors in PHYs of a SAS expander to reduce overhead bandwidth utilization of SAS links between SAS initiators and SAS expanders. In one aspect hereof, a SAS expander self monitors the error status registers of its own PHYs over an internal path that does not use bandwidth of the attached SAS links. When a link level error is so detected the SAS expander may initiate actions and/or report the error to a SAS initiator to thereby reduce he potential for lost data integrity. Where multiple SAS expanders are configured in a SAS domain fabric, each expander may monitor its PHYs or one expander may be designated a master and monitor PHYs of all expanders in the fabric.Type: ApplicationFiled: September 13, 2005Publication date: March 29, 2007Inventors: David Uddenberg, Mark Slutz, Brian Varney
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Publication number: 20070061632Abstract: Methods and structures within a SAS expander for testing SAS devices and other SAS expanders in the SAS domain. Testing devices and expanders in the domain by operations performed within a SAS expander in the domain relieves the burden of such processing in attached host systems and adds flexibility for scheduling processing for test operation of devices and expanders in the domain. In one aspect hereof, the testing may be performed by a master SAS expander configured in the domain. The SAS expander may initiate testing of devices following completion of the SAS discovery process. Testing may also be initiated in response to events in the SAS domain not typically detected by attached host systems.Type: ApplicationFiled: September 13, 2005Publication date: March 15, 2007Inventors: David Uddenberg, Mark Slutz, Brian Varney
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Publication number: 20050034467Abstract: An electronic HEMD determines the optimum balance between gas cooling and heat exchanger pressure loss, for any given operating condition, and adjusts the gas flow rate through the exchanger accordingly, to yield the maximum net power savings (and thereby energy savings) afforded by the exchanger. Maintaining the optimum balance between cooling and exchanger pressure loss reduces the amount of energy required to transport a given volume of gas through a pipeline and thereby increases the transmission efficiency of the gas pipeline system. A method of operating a heat exchanger on a natural gas transmission pipeline using a control algorithm that in turn controls the position of a heat exchanger bypass valve.Type: ApplicationFiled: September 10, 2003Publication date: February 17, 2005Inventor: Brian Varney
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Patent number: 6513334Abstract: A three stage lean burn combustion chamber (28) comprises a primary combustion zone (36), a secondary combustion zone (40) and a tertiary combustion zone (44). Each of the combustion zones (36, 40, 44) is supplied with premixed fuel and air by respective fuel and air mixing ducts (76, 78, 80, 92). Secondary fuel injectors (106) and two secondary fuel manifolds (105A, 105B) supply fuel into different circumferential sectors, halves, of the secondary fuel and air mixing duct (80). The secondary fuel manifolds (105A, 105B) have secondary fuel valves (107A, 107B) which supply a greater proportion of fuel to the secondary fuel manifold (105A) than the secondary fuel manifold (105B) so that there is circumferential biasing of fuel in the secondary combustion zone (40). This circumferential biasing of fuel in the secondary combustion zone (40) reduces the generation of harmful pressure oscillations in the combustion chamber (28).Type: GrantFiled: July 25, 2001Date of Patent: February 4, 2003Assignee: Rolls-Royce plcInventor: Brian A. Varney
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Publication number: 20020020173Abstract: A three stage lean burn combustion chamber (28) comprises a primary combustion zone (36), a secondary combustion zone (40) and a tertiary combustion zone (44). Each of the combustion zones (36,40,44) is supplied with premixed fuel and air by respective fuel and air mixing ducts (76,78,80,92). Secondary fuel injectors (106) and two secondary fuel manifolds (105A, 105B) supply fuel into different circumferential sectors, halves, of the secondary fuel and air mixing duct (80). The secondary fuel manifolds (105A, 105B) have secondary fuel valves (107A,107B) which supply a greater proportion of fuel to the secondary fuel manifold (105A) than the secondary fuel manifold (105B) so that there is circumferential biasing of fuel in the secondary combustion zone (40). This circumferential biasing of fuel in the secondary combustion zone (40) reduces the generation of harmful pressure oscillations in the combustion chamber (28).Type: ApplicationFiled: July 25, 2001Publication date: February 21, 2002Inventor: Brian A. Varney
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Patent number: 6190090Abstract: An apparatus for use in a pipeline is disclosed. The apparatus has a housing through which pipeline fluids may enter from the rear of the housing, pass through the housing and subsequently exit from the housing. A first bonnet, having several openings, is mounted at the front of the housing on a shaft which is oriented parallel to the longitudinal axis of the housing. A second bonnet is mounted on the housing and fits over the first bonnet. The second bonnet has openings which, when aligned with the openings in the first bonnet, permit the flow of pipeline fluid out of the housing in various directions. The first bonnet is movable in relation to the second bonnet so as to vary the degree of alignment of the openings in the bonnets. By varying the degree of alignment of the openings in the bonnets, the flow of fluids through the housing is regulated so as to control the speed of the apparatus.Type: GrantFiled: October 6, 1998Date of Patent: February 20, 2001Assignee: Tuboscope Pipeline Services Canada, Inc.Inventors: Douglas Clinton Campbell, Brian Varney
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Patent number: 5094006Abstract: A swag (10) for decorative use in curtaining is made using a template (11) which may be of rigid sheet material and formed by two side edges (14), each bearing deep cut-outs (15, 16 . . . ) and projections (17). The side edges taper outwardly from top to bottom and their separation, but not their inclination, can be adjusted using an adjustable slide (22) having a scale (24).Type: GrantFiled: January 19, 1990Date of Patent: March 10, 1992Assignee: Parkhill Blinds and Curtains LimitedInventor: Brian A. Varney