Patents by Inventor Grzegorz Glinka

Grzegorz Glinka 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).

  • METHOD FOR THE PREDICTION OF FATIGUE LIFE FOR WELDED STRUCTURES
    Publication number: 20120259593
    Abstract: A method of determining the fatigue life of a welded structure, including the steps of: creating a 3D coarse mesh model of the welded structure to be analyzed; analyzing the coarse mesh model using an FEA model to generate FEA data; identifying a critical stress location on the coarse mesh model having a through thickness stress distribution, based on the FEA data; post processing the FEA data in the middle portion of the through thickness stress distribution while excluding the through thickness stress distribution near the edges of the identified critical stress location to determine a peak stress; and determining a fatigue life of the welded structure at the identified critical stress location, dependent on the determined peak stress.
    Type: Application
    Filed: April 7, 2011
    Publication date: October 11, 2012
    Inventors: Mohamad S. El-Zein, Rakesh K. Goyal, Grzegorz Glinka
  • System and method for predicting material fatigue and damage
    Patent number: 7889840
    Abstract: A method and system for determining damage prediction of a component. The component may be critical component used in an aircraft or other vehicle experiencing cyclic loading. The method and system determines the ?K, Kmax and Kinternal values for the component and utilizes these values in order to predict damage and/or failure of the component.
    Type: Grant
    Filed: January 10, 2008
    Date of Patent: February 15, 2011
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Asuri K. Vasudevan, Kuntimaddi Sadananda, Grzegorz Glinka, Daniel Kujawski
  • System and Method for predicting Material Fatigue and Damage
    Publication number: 20080177516
    Abstract: A method and system for determining damage prediction of a component. The component may be critical component used in an aircraft or other vehicle experiencing cyclic loading. The method and system determines the ?K, Kmax and Kinternal values for the component and utilizes these values in order to predict damage and/or failure of the component.
    Type: Application
    Filed: January 10, 2008
    Publication date: July 24, 2008
    Inventors: Asuri K. Vasudevan, Kuntimaddi Sadananda, Grzegorz Glinka, Daniel Kujawski