Patents by Inventor John Z. Lin
John Z. Lin 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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Publication number: 20240099086Abstract: A display may have an array of pixels. Display driver circuitry may supply data and control signals to the pixels. Each pixel may have seven transistors, a capacitor, and a light-emitting diode such as an organic light-emitting diode. The seven transistors may receive control signals using horizontal control lines. Each pixel may have first and second emission enable transistors that are coupled in series with a drive transistor and the light-emitting diode of that pixel. The first and second emission enable transistors may be coupled to a common control line or may be separately controlled so that on-bias stress can be effectively applied to the drive transistor. The display driver circuitry may have gate driver circuits that provide different gate line signals to different rows of pixels within the display. Different rows may also have different gate driver strengths and different supplemental gate line loading structures.Type: ApplicationFiled: November 17, 2023Publication date: March 21, 2024Inventors: Cheng-Ho Yu, Chin-Wei Lin, Shyuan Yang, Ting-Kuo Chang, Tsung-Ting Tsai, Warren S. Rieutort-Louis, Shih-Chang Chang, Yu Cheng Chen, John Z. Zhong
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Patent number: 11521590Abstract: Disclosed herein a method of producing an ultrasound that includes defining a set of criteria for an ultrasound emitter comprising a plate. The set of criteria includes a power output criterion, a frequency criterion and number of nodes for a resonance mode of the plate, a focus criterion, and a durability criterion. The method includes determining an outline and a thickness range for the plate, based on the set of criteria. The method includes using topology optimization to determine internodal zone dimensions for the plate, based on the set of criteria, the outline, and the thickness range. The method includes manufacturing the plate according to the internodal zone dimensions.Type: GrantFiled: June 24, 2019Date of Patent: December 6, 2022Assignee: The Boeing CompanyInventors: John Z. Lin, Wayne Cooper, Kane M. Mordaunt
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Patent number: 11255825Abstract: Methods that provide wrinkle characterization and performance prediction for wrinkled composite structures using automated structural analysis. In accordance with some embodiments, the method combines the use of B-scan ultrasound data, automated optical measurement of wrinkles and geometry of cross-sections, and finite element analysis of wrinkled composite structure to provide the ability to assess the actual significance of a detected wrinkle relative to the intended performance of the structure. The disclosed method uses an ultrasonic inspection system that has been calibrated by correlating ultrasonic B-scan data acquired from reference standards with measurements of optical cross sections (e.g., micrographs) of those reference standards.Type: GrantFiled: October 31, 2016Date of Patent: February 22, 2022Assignee: The Boeing CompanyInventors: Gary E. Georgeson, Jill P. Bingham, Hong Hue Tat, Yuan-Jye Wu, John M. Pryor, Sadie L. Fieni, Mark D. Winters, Kathryn T. Moore, James C. Kennedy, Clayton M. Little, John Z. Lin
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Patent number: 10946593Abstract: Closed-loop systems and methods for controlling the temperature at the compaction point as an automated fiber placement (AFP) machine is placing material over complex surface features at varying speeds. The closed-loop system starts with multiple infrared temperature sensors directed at the layup surface in front of the compaction roller and also at the new layup surface behind the compaction roller. These sensors supply direct temperature readings to a control computer, which also receives speed data and a listing of active tows from the AFP machine and is also programmed with the number of plies in the current layup. In accordance with one embodiment, the heater control system uses a proportional-integral-derivative loop to control the temperature at the compaction point (e.g., at the interface of the compaction roller and a newly laid tow) and regulate the heater power to achieve the desired temperature.Type: GrantFiled: November 26, 2019Date of Patent: March 16, 2021Assignee: The Boeing CompanyInventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
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Publication number: 20200402495Abstract: Disclosed herein a method of producing an ultrasound that includes defining a set of criteria for an ultrasound emitter comprising a plate. The set of criteria includes a power output criterion, a frequency criterion and number of nodes for a resonance mode of the plate, a focus criterion, and a durability criterion. The method includes determining an outline and a thickness range for the plate, based on the set of criteria. The method includes using topology optimization to determine internodal zone dimensions for the plate, based on the set of criteria, the outline, and the thickness range. The method includes manufacturing the plate according to the internodal zone dimensions.Type: ApplicationFiled: June 24, 2019Publication date: December 24, 2020Inventors: John Z. Lin, Wayne Cooper, Kane M. Mordaunt
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Patent number: 10809236Abstract: A method for analyzing a structure includes processing nondestructive inspection (NDI) data for a multi-layer structure to define areas of inconsistency at an internal layer or an interface between adjacent layers. The method includes mapping the areas of inconsistency to finite elements of a finite element model of a nominal of the structure. These finite elements are thereby identified as affected finite elements and include finite elements for the affected internal layer or interface. The method includes producing a reconstructed finite element model of the affected structure from the nominal finite element model, and a modified property or state value assigned to respective element datasets of the affected finite elements. The method includes performing a finite element method (FEM) failure analysis of the reconstructed finite element model under a load, which indicates an extent of residual integrity of the affected structure.Type: GrantFiled: November 18, 2019Date of Patent: October 20, 2020Assignee: THE BOEING COMPANYInventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
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Publication number: 20200094494Abstract: Closed-loop systems and methods for controlling the temperature at the compaction point as an automated fiber placement (AFP) machine is placing material over complex surface features at varying speeds. The closed-loop system starts with multiple infrared temperature sensors directed at the layup surface in front of the compaction roller and also at the new layup surface behind the compaction roller. These sensors supply direct temperature readings to a control computer, which also receives speed data and a listing of active tows from the AFP machine and is also programmed with the number of plies in the current layup. In accordance with one embodiment, the heater control system uses a proportional-integral-derivative loop to control the temperature at the compaction point (e.g., at the interface of the compaction roller and a newly laid tow) and regulate the heater power to achieve the desired temperature.Type: ApplicationFiled: November 26, 2019Publication date: March 26, 2020Applicant: The Boeing CompanyInventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
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Publication number: 20200088692Abstract: A method for analyzing a structure includes processing nondestructive inspection (NDI) data for a multi-layer structure to define areas of inconsistency at an internal layer or an interface between adjacent layers. The method includes mapping the areas of inconsistency to finite elements of a finite element model of a nominal of the structure. These finite elements are thereby identified as affected finite elements and include finite elements for the affected internal layer or interface. The method includes producing a reconstructed finite element model of the affected structure from the nominal finite element model, and a modified property or state value assigned to respective element datasets of the affected finite elements. The method includes performing a finite element method (FEM) failure analysis of the reconstructed finite element model under a load, which indicates an extent of residual integrity of the affected structure.Type: ApplicationFiled: November 18, 2019Publication date: March 19, 2020Inventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
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Patent number: 10525638Abstract: Closed-loop systems and methods for controlling the temperature at the compaction point as an automated fiber placement (AFP) machine is placing material over complex surface features at varying speeds. The closed-loop system starts with multiple infrared temperature sensors directed at the layup surface in front of the compaction roller and also at the new layup surface behind the compaction roller. These sensors supply direct temperature readings to a control computer, which also receives speed data and a listing of active tows from the AFP machine and is also programmed with the number of plies in the current layup. In accordance with one embodiment, the heater control system uses a proportional-integral-derivative loop to control the temperature at the compaction point (e.g., at the interface of the compaction roller and a newly laid tow) and regulate the heater power to achieve the desired temperature.Type: GrantFiled: August 29, 2017Date of Patent: January 7, 2020Assignee: The Boeing CompanyInventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
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Patent number: 10502719Abstract: A method for analyzing a structure includes processing nondestructive inspection (NDI) data for a multi-layer structure to define areas of inconsistency at an internal layer or an interface between adjacent layers. The method includes mapping the areas of inconsistency to finite elements of a finite element model of a nominal of the structure. These finite elements are thereby identified as affected finite elements and include finite elements for the affected internal layer or interface. The method includes producing a reconstructed finite element model of the affected structure from the nominal finite element model, and a modified property or state value assigned to respective element datasets of the affected finite elements. The method includes performing a finite element method (FEM) failure analysis of the reconstructed finite element model under a load, which indicates an extent of residual integrity of the affected structure.Type: GrantFiled: August 21, 2015Date of Patent: December 10, 2019Assignee: The Boeing CompanyInventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
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Publication number: 20190061282Abstract: Closed-loop systems and methods for controlling the temperature at the compaction point as an automated fiber placement (AFP) machine is placing material over complex surface features at varying speeds. The closed-loop system starts with multiple infrared temperature sensors directed at the layup surface in front of the compaction roller and also at the new layup surface behind the compaction roller. These sensors supply direct temperature readings to a control computer, which also receives speed data and a listing of active tows from the AFP machine and is also programmed with the number of plies in the current layup. In accordance with one embodiment, the heater control system uses a proportional-integral-derivative loop to control the temperature at the compaction point (e.g., at the interface of the compaction roller and a newly laid tow) and regulate the heater power to achieve the desired temperature.Type: ApplicationFiled: August 29, 2017Publication date: February 28, 2019Applicant: The Boeing CompanyInventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
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Publication number: 20180120268Abstract: Methods that provide wrinkle characterization and performance prediction for wrinkled composite structures using automated structural analysis. In accordance with some embodiments, the method combines the use of B-scan ultrasound data, automated optical measurement of wrinkles and geometry of cross-sections, and finite element analysis of wrinkled composite structure to provide the ability to assess the actual significance of a detected wrinkle relative to the intended performance of the structure. The disclosed method uses an ultrasonic inspection system that has been calibrated by correlating ultrasonic B-scan data acquired from reference standards with measurements of optical cross sections (e.g., micrographs) of those reference standards.Type: ApplicationFiled: October 31, 2016Publication date: May 3, 2018Applicant: The Boeing CompanyInventors: Gary E. Georgeson, Jill P. Bingham, Hong Hue Tat, Yuan-Jye Wu, John M. Pryor, Sadie L. Fieni, Mark D. Winters, Kathryn T. Moore, James C. Kennedy, Clayton M. Little, John Z. Lin
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Publication number: 20170052152Abstract: A method for analyzing a structure includes processing nondestructive inspection (NDI) data for a multi-layer structure to define areas of inconsistency at an internal layer or an interface between adjacent layers. The method includes mapping the areas of inconsistency to finite elements of a finite element model of a nominal of the structure. These finite elements are thereby identified as affected finite elements and include finite elements for the affected internal layer or interface. The method includes producing a reconstructed finite element model of the affected structure from the nominal finite element model, and a modified property or state value assigned to respective element datasets of the affected finite elements. The method includes performing a finite element method (FEM) failure analysis of the reconstructed finite element model under a load, which indicates an extent of residual integrity of the affected structure.Type: ApplicationFiled: August 21, 2015Publication date: February 23, 2017Inventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
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Patent number: 9539690Abstract: Method and apparatus are provided for processing and changing the physical characteristics of a metal workpiece into a final metal component. Predetermined processing parameters are established for achieving a final metal component. The metal workpiece is positioned securely on a support during the changing of the physical characteristics. Impacts are applied to a surface of the workpiece multiple times for achieving the final metal component while controlling the impacting with the predetermined processing parameters. A sensor is provided for continuously sensing the currently existing physical conditions of the workpiece during impacting. The predetermined processing parameters are changed into adjusted processing parameters and the impacts are changed in reaction to the currently existing physical conditions of the workpiece from the sensing and processing of the workpiece until the final metal component has been achieved.Type: GrantFiled: September 19, 2013Date of Patent: January 10, 2017Assignee: The Boeing CompanyInventors: Lauren K. Lundquist, McKay A. Kunz, James E. Pillers, James B. Castle, John Z. Lin, Sebastian Nervi
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Patent number: 9274089Abstract: An apparatus is provided that includes a wave generator, plurality of transducers and processing device. The wave generator may be configured to simultaneously generate a plurality of acoustic waves that propagate through a laminate along a plurality of in-plane directions. The transducers may be spaced apart from one another and positionable at one or more known distances from the wave generator along respective in-plane directions. The transducers may be configured to detect acoustic waves propagating through the laminate along the respective in-plane directions. The processing device may be coupled to the transducers and configured to simultaneously calculate a plurality of elastic constants of the laminate as a function of velocities of the acoustic waves detected by the transducers. And the processing device may be configured to calculate the velocities as a function of the known distance(s) and arrival times of the acoustic waves at the transducers.Type: GrantFiled: October 31, 2012Date of Patent: March 1, 2016Assignee: The Boeing CompanyInventors: John Z Lin, Richard H Bossi
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Publication number: 20150075240Abstract: Method and apparatus are provided for processing and changing the physical characteristics of a metal workpiece into a final metal component. Predetermined processing parameters are established for achieving a final metal component. The metal workpiece is positioned securely on a support during the changing of the physical characteristics. Impacts are applied to a surface of the workpiece multiple times for achieving the final metal component while controlling the impacting with the predetermined processing parameters. A sensor is provided for continuously sensing the currently existing physical conditions of the workpiece during impacting. The predetermined processing parameters are changed into adjusted processing parameters and the impacts are changed in reaction to the currently existing physical conditions of the workpiece from the sensing and processing of the workpiece until the final metal component has been achieved.Type: ApplicationFiled: September 19, 2013Publication date: March 19, 2015Applicant: The Boeing CompanyInventors: Lauren K. LUNDQUIST, McKay A. KUNZ, James E. PILLERS, James B. CASTLE, John Z. LIN, Sebastian NERVI
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Patent number: 8965100Abstract: A first simulated inspection is conducted to provide a first waveform data set associated with the at least one irregularity parameter. The first simulated inspection is conducted using a first evaluation setting. A first image is produced based on the first waveform set, and it is determined whether a quality of the first image satisfies a predetermined threshold.Type: GrantFiled: January 20, 2012Date of Patent: February 24, 2015Assignee: The Boeing CompanyInventors: John Z. Lin, Hong Tat, Richard H. Bossi
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Publication number: 20130188858Abstract: A first simulated inspection is conducted to provide a first waveform data set associated with the at least one irregularity parameter. The first simulated inspection is conducted using a first evaluation setting. A first image is produced based on the first waveform set, and it is determined whether a quality of the first image satisfies a predetermined threshold.Type: ApplicationFiled: January 20, 2012Publication date: July 25, 2013Inventors: John Z. Lin, Hong Tat, Richard H. Bossi