Patents by Inventor Norman Arnold Turnquist
Norman Arnold Turnquist 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: 8327752Abstract: Disclosed is an actuator that includes a cylinder having an input port, a piston disposed at least partially inside of the cylinder, and one or more piston rings disposed in a circumferential piston ring groove or grooves. The actuator also includes at least one spring, inserted into the circumferential piston ring groove adjacent to the one or more piston rings and a high pressure side of said piston ring. The spring preloads the one or more piston rings to seal between a low pressure face of the one or more piston rings and a low pressure face of the circumferential piston ring groove. The invention also includes a method for moving an adjustable seal in a radial direction using the piston-ring sealed actuator. The method includes moving the adjustable seal in an axial direction, breaking a primary axial contact between the adjustable seal and a primary sealing face.Type: GrantFiled: October 27, 2006Date of Patent: December 11, 2012Assignee: General Electric CompanyInventors: Kripa Kiran Varanasi, Shorya Awtar, Frederick George Baily, Mark Edward Burnett, Farshad Ghasripoor, Imdad Imam, Norman Arnold Turnquist
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Publication number: 20120251290Abstract: An aspirating face seal includes a primary seal, a secondary seal, and a biasing device. The primary seal includes a first seal component and a second seal component. The first seal component is configured to be coupled to a rotor and rotatable with the rotor. The secondary seal includes a plurality of flexible elements and configured to be disposed between the second seal component and a stator housing. A biasing device is coupled to the second seal component such that the second seal component is biased along an axial direction away from the first seal component during a non-operating condition.Type: ApplicationFiled: March 31, 2011Publication date: October 4, 2012Applicant: GENERAL ELECTRIC COMPANYInventors: Norman Arnold Turnquist, Rodrigo Rodriguez Erdmenger, Xiaoqing Zheng, Robbert Christiaan Pannekeet, Keith Michael Parker
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Patent number: 8262349Abstract: A steam turbine comprises a steam turbine casing, a rotor, and at least one compliant plate seal assembly situated between the casing and the rotor. The compliant plate seal assembly comprises a supporting member being stationary with respect to the casing, a plurality of plate members movably mounted to the supporting member and extending towards the rotor, each plate member being inclined with respect to a rotation direction of the rotor, and an actuator for selectively exerting a pressure to retract the plate members in a direction away from the rotor.Type: GrantFiled: December 22, 2008Date of Patent: September 11, 2012Assignee: General Electric CompanyInventors: Norman Arnold Turnquist, Bernard Arthur Courture, Jr., Mark William Kowalczyk, Frederick George Baily, Mark Edward Burnett
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Patent number: 8250756Abstract: A compliant plate seal arrangement manufacturing method is provided. A compliant plate seal manufacturing method includes assembling a plurality of t-shims and a plurality of spacer shims into a straight weld fixture, thereby forming a shim pack having a front and rear end and sides, welding the sides of the shim pack to a top plate, removing a portion of the weld fixture, removing the plurality of spacer shims, shaping the shim pack into a target diameter, and applying a radial flow plate to the leaf pack.Type: GrantFiled: February 20, 2009Date of Patent: August 28, 2012Assignee: General Electric CompanyInventors: William Edward Adis, Bernard Arthur Couture, Jr., Hrishikesh Vishvas Deo, Sean Douglas Feeny, Michael Dennis Mack, Daniel Frederick Purdy, Norman Arnold Turnquist
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Patent number: 8240913Abstract: A device includes a stationary, rotary component, and a fiber optic sensing system. The fiber optic sensing system includes a cable having one or more fiber optic sensors disposed on the stationary component, the rotary component, or combinations thereof. The fiber optic sensing system is configured to detect one or more first parameters including temperature, strain, pressure, vibration, torque; or combinations thereof related to the stationary component, the rotary component, or combinations thereof. The one or more first parameters is used to determine one or more second parameters including thermal expansion, clearance, fluid flow rate variation, condensation, fluid leakage, thermal loss, life, thermal stress, or combinations thereof related to the stationary component, the rotary component, or combinations thereof.Type: GrantFiled: September 24, 2008Date of Patent: August 14, 2012Assignee: General Electric CompanyInventors: Danian Zheng, Norman Arnold Turnquist, Peter John Eisenzopf, Kevin Thomas McCarthy, Hua Xia, Roy Paul Swintek
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Publication number: 20120201489Abstract: A method includes transmitting light through at least one transmission optical fiber towards a target, receiving light reflected from the target through at least one signal optical fiber, filtering the received light at least two different wavelengths, and using the filtered light to detect a clearance variation. An optical fiber probe includes a plurality of optical fibers, a moisture-resistant enclosure enclosing the optical fibers, a hydrophobic layer situated over an end of the optical fiber probe for preventing moisture from reaching the optical fibers, and a broadband transmission layer between ends of the optical fibers and the hydrophobic layer.Type: ApplicationFiled: August 2, 2011Publication date: August 9, 2012Applicant: GENERAL ELECTRIC COMPANYInventors: Danian Zheng, Peter John Eisenzopf, Kevin Thomas McCarthy, Roy Paul Swintek, Norman Arnold Turnquist, Hua Xia
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Publication number: 20120195741Abstract: A brush seal assembly for turbomachinery having a rotor can include a stationary seal component, a floating seal component coupled to the stationary seal component and circumferentially angled bristles arranged in a bristle pack, disposed in the floating seal component and extended axially with respect to the rotor.Type: ApplicationFiled: January 31, 2011Publication date: August 2, 2012Applicant: GENERAL ELECTRIC COMPANYInventors: Neelesh Nandkumar Sarawate, Norman Arnold Turnquist, William Edward Adis, Robert Gerard Baran, Rodrigo Rodriguez Erdmenger, Robbert Christiaan Pannekeet, Keith Michael Parker, Xiaoqing Zheng
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Patent number: 8162324Abstract: A method of assembling a turbomachine that includes a rotor and a stationary component is provided. The method includes coupling a housing to the stationary component using at least one biasing member, wherein the housing extending circumferentially about the rotor. The method also includes coupling at least one annular ring to the housing, and coupling a plurality of plate members to the housing such that the at least one annular ring extends from the housing towards the rotor and partially through the plurality of plate members.Type: GrantFiled: February 18, 2008Date of Patent: April 24, 2012Assignee: General Electric CompanyInventors: Hrishikesh Vishvas Deo, Norman Arnold Turnquist, Frederick George Baily, Bernard Arthur Couture, Jr., Sean Douglas Feeny, William Edward Adis, Shorya Awtar
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Publication number: 20120049461Abstract: A seal assembly for a turbomachine includes a plurality of compliant plate members attached to an interior surface of a stationary housing. The compliant plate members define a sealing ring between the stationary housing and a rotor. Each of the compliant plate members comprises at least one slot therein. The seal assembly further includes at least one arcuate static ring attached to the interior surface of the stationary housing and extending radially into the at least one slot in the compliant plate members. Each of the at least one static ring extends circumferentially through and between a plurality of the compliant plate members. Finally, the seal assembly includes a vibration damper disposed adjacent to or provided on the plurality of compliant plate members. The vibration damper is configured to dampen vibration of the plurality of compliant plate members.Type: ApplicationFiled: August 31, 2010Publication date: March 1, 2012Applicant: General Electric CompanyInventors: Hrishikesh Vishvas Deo, Norman Arnold Turnquist, Farshad Ghasripoor, William Edward Adis
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Patent number: 8113771Abstract: A spring assembly for a retractable turbine rotor seal supported in an arcuate segment may include in one embodiment a first radially inner restraining plate having a lower surface adapted to engage a surface of a turbine stator, and a flat upper surface provide with an upstanding hub; a second radially outer restraining plate having a flat lower surface and an upper surface adapted to engage a surface of the arcuate segment, the radially outer restraining plate formed with an opening receiving the upstanding hub; and at least one spring telescoped over the upstanding hub and exerting a radially outward biasing force on the second radially outer restraining plate, and adapted to exert a radially outward retracting force on the arcuate segment.Type: GrantFiled: March 20, 2009Date of Patent: February 14, 2012Assignee: General Electric CompanyInventors: Norman Arnold Turnquist, Shorya nmn Awtar, Mustafa Gursoy, Kartik Mangudi Varadarajan
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Patent number: 8052375Abstract: Disclosed is a seal for turbomachinery including a seal face locatable between a first turbomachinery component and a second turbomachinery component. At least one fluid channel extends through the seal. The at least one fluid channel is capable of injecting fluid flow between the first turbomachinery component and the second turbomachinery component at the seal face thereby disrupting a leakage flow between the first turbomachinery component and the second turbomachinery component. Further disclosed is a turbomachine utilizing the seal.Type: GrantFiled: June 2, 2008Date of Patent: November 8, 2011Assignee: General Electric CompanyInventors: Norman Arnold Turnquist, Kevin L. Bruce, Ciro Cerretelli, John Ernest Tourigny
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Patent number: 8042412Abstract: A fiberoptic multi-parameter sensing system for monitoring turbomachinery system shaft static and dynamic torques, vibration modes and associated operation status includes a multi-furcated fiber bundle based optical splitter configured to transmit light to a surface of at least one turbomachinery system shaft through a plurality of optical fiber bundles disposed at a plurality of locations in proximity to the surface of the at least one shaft, in which the plurality of locations together are arranged in a substantially axial direction between the ends of the at least one shaft.Type: GrantFiled: June 25, 2008Date of Patent: October 25, 2011Assignee: General Electric CompanyInventors: Hua Xia, Norman Arnold Turnquist, David So Keung Chan, Danian Zheng, Kevin Thomas McCarthy, Richard Joseph Gawrelski, Matthew Damian Pietrzykowski, Alexander Seth Ross, Yun Li, Juntao Wu
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Patent number: 8009939Abstract: A fiberoptic system for clearance detection between rotating and stationary turbomachinery components is presented. The system comprises an optical fiber probe comprising a plurality of optical fibers, at least one of the optical fibers comprising a transmission fiber and at least one of the optical fibers comprising a signal fiber; a light source for providing light through the transmission fiber towards a target; filters for receiving light from the signal fibers, at least two of the filters for filtering different wavelengths; and at least one photodetector for receiving filtered light from the filters.Type: GrantFiled: September 30, 2008Date of Patent: August 30, 2011Assignee: General Electric CompanyInventors: Danian Zheng, Peter John Eisenzopf, Kevin Thomas McCarthy, Roy Paul Swintek, Norman Arnold Turnquist, Hua Xia
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Publication number: 20110135445Abstract: A pressure balance seal includes a sealing surface facing an inward radial direction, and a stator interface comprising at least one surface interfacing with a stator. The pressure balance seal further includes a friction reducing feature. The friction reducing feature includes a cavity on the sealing surface. The cavity is configured to receive a fluid such that a normal force acting on the pressure balance seal is counterbalanced by a force generated by a pressure of the fluid.Type: ApplicationFiled: December 4, 2009Publication date: June 9, 2011Applicant: GENERAL ELECTRIC COMPANYInventors: Norman Arnold Turnquist, Keith Michael Parker, Xiaoqing Zheng, Rodrigo Rodriguez Erdmenger, Robbert Christiaan Pannekeet, Alexander Kimberley Simpson, Biao Fang
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Publication number: 20100239415Abstract: A spring assembly for a retractable turbine rotor seal supported in an arcuate segment may include in one embodiment a first radially inner restraining plate having a lower surface adapted to engage a surface of a turbine stator, and a flat upper surface provide with an upstanding hub; a second radially outer restraining plate having a flat lower surface and an upper surface adapted to engage a surface of the arcuate segment, the radially outer restraining plate formed with an opening receiving the upstanding hub; and at least one spring telescoped over the upstanding hub and exerting a radially outward biasing force on the second radially outer restraining plate, and adapted to exert a radially outward retracting force on the arcuate segment.Type: ApplicationFiled: March 20, 2009Publication date: September 23, 2010Applicant: General Electric CompanyInventors: Norman Arnold TURNQUIST, Shorya nmn AWTAR, Mustafa GURSOY, Karatik Mangudi VARADARAJAN
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Publication number: 20100213675Abstract: A compliant plate seal arrangement manufacturing method is provided. A compliant plate seal manufacturing method includes assembling a plurality of t-shims and a plurality of spacer shims into a straight weld fixture, thereby forming a shim pack having a front and rear end and sides, welding the sides of the shim pack to a top plate, removing a portion of the weld fixture, removing the plurality of spacer shims, shaping the shim pack into a target diameter, and applying a radial flow plate to the leaf pack.Type: ApplicationFiled: February 20, 2009Publication date: August 26, 2010Applicant: GENERAL ELECTRIC COMPANYInventors: William Edward Adis, Bernard Arthur Couture, JR., Hrishikesh Vishvas Deo, Sean Douglas Feeny, Michael Dennis Mack, Daniel Frederick Purdy, Norman Arnold Turnquist
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Publication number: 20100176556Abstract: A compliant plate seal manufacturing method is provided. The method includes assembling a plurality of compliant plates and a plurality of spacer shims into a weld fixture, thereby forming a leaf pack having a front and rear end and sides and a curvature, welding the sides of the leaf pack to hook plates on the weld fixture, removing a portion of the weld fixture, removing a portion of the hook plates and applying a radial flow plate to the leaf pack.Type: ApplicationFiled: January 12, 2009Publication date: July 15, 2010Applicant: General Electric CompanyInventors: Michael Dennis Mack, William Edward Adis, Hrishikesh Vishvas Deo, Daniel Frederick Purdy, Norman Arnold Turnquist
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Publication number: 20100158674Abstract: A steam turbine comprises a steam turbine casing, a rotor, and at least one compliant plate seal assembly situated between the casing and the rotor. The compliant plate seal assembly comprises a supporting member being stationary with respect to the casing, a plurality of plate members movably mounted to the supporting member and extending towards the rotor, each plate member being inclined with respect to a rotation direction of the rotor, and an actuator for selectively exerting a pressure to retract the plate members in a direction away from the rotor.Type: ApplicationFiled: December 22, 2008Publication date: June 24, 2010Applicant: GENERAL ELECTRIC COMPANYInventors: Norman Arnold Turnquist, Bernard Arthur Couture, JR., Mark William Kowalczyk, Frederick George Baily, Mark Edward Burnett
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Publication number: 20100143102Abstract: A self-correcting seal assembly comprises a plurality of compliant plates coupled circumferentially to a stationary component, at least one slot in the compliant plates extending from the stationary component towards a rotor; and a resistance member coupled to a stationary component. The resistance member comprising at least one annular ring extending from the stationary component towards a rotor and through the slot. The seal assembly is configured to create passive feedback on hydrostatic forces in response to a tip-clearance between the rotor and tips of the compliant plates.Type: ApplicationFiled: February 15, 2010Publication date: June 10, 2010Applicant: GENERAL ELECTRIC COMPANYInventors: Hrishikesh Vishvas Deo, Norman Arnold Turnquist, Barbaros Yildirim
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Patent number: 7703774Abstract: A shaft seal reduces leakage between a rotating shaft such as a rotor and a stator. The shaft seal or shingle seal includes a plurality of compliant-plate members attached to the stator in facing relation. The compliant-plate members define a sealing ring between the stator and the rotating shaft. Each of the compliant-plate members includes a plurality of shingles, where adjacent compliant-plate members are disposed relative to each other such that the shingles are at least partially staggered in a direction of axial leakage.Type: GrantFiled: September 12, 2006Date of Patent: April 27, 2010Assignee: General Electric CompanyInventors: Shorya Awtar, William Edward Adis, Mark William Kowalczyk, Norman Arnold Turnquist