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).

  • Publication number: 20240099086
    Abstract: 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: Application
    Filed: November 17, 2023
    Publication date: March 21, 2024
    Inventors: 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
  • Patent number: 11521590
    Abstract: 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: Grant
    Filed: June 24, 2019
    Date of Patent: December 6, 2022
    Assignee: The Boeing Company
    Inventors: John Z. Lin, Wayne Cooper, Kane M. Mordaunt
  • Patent number: 11255825
    Abstract: 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: Grant
    Filed: October 31, 2016
    Date of Patent: February 22, 2022
    Assignee: The Boeing Company
    Inventors: 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
  • Patent number: 10946593
    Abstract: 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: Grant
    Filed: November 26, 2019
    Date of Patent: March 16, 2021
    Assignee: The Boeing Company
    Inventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
  • Publication number: 20200402495
    Abstract: 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: Application
    Filed: June 24, 2019
    Publication date: December 24, 2020
    Inventors: John Z. Lin, Wayne Cooper, Kane M. Mordaunt
  • Patent number: 10809236
    Abstract: 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: Grant
    Filed: November 18, 2019
    Date of Patent: October 20, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
  • Publication number: 20200094494
    Abstract: 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: Application
    Filed: November 26, 2019
    Publication date: March 26, 2020
    Applicant: The Boeing Company
    Inventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
  • Publication number: 20200088692
    Abstract: 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: Application
    Filed: November 18, 2019
    Publication date: March 19, 2020
    Inventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
  • Patent number: 10525638
    Abstract: 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: Grant
    Filed: August 29, 2017
    Date of Patent: January 7, 2020
    Assignee: The Boeing Company
    Inventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
  • Patent number: 10502719
    Abstract: 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: Grant
    Filed: August 21, 2015
    Date of Patent: December 10, 2019
    Assignee: The Boeing Company
    Inventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
  • Publication number: 20190061282
    Abstract: 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: Application
    Filed: August 29, 2017
    Publication date: February 28, 2019
    Applicant: The Boeing Company
    Inventors: Brice A. Johnson, Samuel F. Pedigo, Sayata Ghose, John Z. Lin
  • Publication number: 20180120268
    Abstract: 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: Application
    Filed: October 31, 2016
    Publication date: May 3, 2018
    Applicant: The Boeing Company
    Inventors: 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
  • Publication number: 20170052152
    Abstract: 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: Application
    Filed: August 21, 2015
    Publication date: February 23, 2017
    Inventors: Hong Hue Tat, Kelly M. Greene, John Z. Lin, Carlyn R. Brewer, Russell Lee Keller
  • Patent number: 9539690
    Abstract: 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: Grant
    Filed: September 19, 2013
    Date of Patent: January 10, 2017
    Assignee: The Boeing Company
    Inventors: Lauren K. Lundquist, McKay A. Kunz, James E. Pillers, James B. Castle, John Z. Lin, Sebastian Nervi
  • Patent number: 9274089
    Abstract: 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: Grant
    Filed: October 31, 2012
    Date of Patent: March 1, 2016
    Assignee: The Boeing Company
    Inventors: John Z Lin, Richard H Bossi
  • Publication number: 20150075240
    Abstract: 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: Application
    Filed: September 19, 2013
    Publication date: March 19, 2015
    Applicant: The Boeing Company
    Inventors: Lauren K. LUNDQUIST, McKay A. KUNZ, James E. PILLERS, James B. CASTLE, John Z. LIN, Sebastian NERVI
  • Patent number: 8965100
    Abstract: 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: Grant
    Filed: January 20, 2012
    Date of Patent: February 24, 2015
    Assignee: The Boeing Company
    Inventors: John Z. Lin, Hong Tat, Richard H. Bossi
  • Publication number: 20130188858
    Abstract: 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: Application
    Filed: January 20, 2012
    Publication date: July 25, 2013
    Inventors: John Z. Lin, Hong Tat, Richard H. Bossi