Patents by Inventor Robert S. Piascik

Robert S. Piascik 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).

  • Patent number: 9499882
    Abstract: A composite material includes a structural material and a shape-memory alloy embedded in the structural material. The shape-memory alloy changes crystallographic phase from austenite to martensite in response to a predefined critical macroscopic average strain of the composite material. In a second embodiment, the composite material includes a plurality of particles of a ferromagnetic shape-memory alloy embedded in the structural material. The ferromagnetic shape-memory alloy changes crystallographic phase from austenite to martensite and changes magnetic phase in response to the predefined critical macroscopic average strain of the composite material.
    Type: Grant
    Filed: January 11, 2010
    Date of Patent: November 22, 2016
    Assignee: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
    Inventors: Terryl A. Wallace, Stephen W. Smith, Robert S. Piascik, Michael R. Horne, Peter L. Messick, Joel A. Alexa, Edward H. Glaessgen, Benjamin T. Hailer
  • Patent number: 8679642
    Abstract: A first material with a known maximum temperature of operation is coated with a second material on at least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.
    Type: Grant
    Filed: September 26, 2013
    Date of Patent: March 25, 2014
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stephen W. Smith, John A. Newman, Robert S. Piascik, Edward H. Glaessgen
  • Publication number: 20140030543
    Abstract: A first material with a known maximum temperature of operation is coated with a second material on at least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.
    Type: Application
    Filed: September 26, 2013
    Publication date: January 30, 2014
    Inventors: Stephen W. Smith, John A. Newman, Robert S. Piascik, Edward H. Glaessgen
  • Patent number: 8347479
    Abstract: A first material with a known maximum temperature of operation is coated with a second material on at least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.
    Type: Grant
    Filed: August 4, 2010
    Date of Patent: January 8, 2013
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Stephen W. Smith, John A. Newman, Robert S. Piascik, Edward H. Glaessgen
  • Publication number: 20110033728
    Abstract: A first material with a known maximum temperature of operation is coated with a second material on at least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.
    Type: Application
    Filed: August 4, 2010
    Publication date: February 10, 2011
    Applicants: Space Administration
    Inventors: Stephen W. Smith, John A. Newman, Robert S. Piascik, Edward H. Glaesgen
  • Publication number: 20100190026
    Abstract: A composite material includes a structural material and a shape-memory alloy embedded in the structural material. The shape-memory alloy changes crystallographic phase from austenite to martensite in response to a predefined critical macroscopic average strain of the composite material. In a second embodiment, the composite material includes a plurality of particles of a ferromagnetic shape-memory alloy embedded in the structural material. The ferromagnetic shape-memory alloy changes crystallographic phase from austenite to martensite and changes magnetic phase in response to the predefined critical macroscopic average strain of the composite material.
    Type: Application
    Filed: January 11, 2010
    Publication date: July 29, 2010
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Terryl A. Wallace, Stephen W. Smith, Robert S. Piascik, Michael R. Horne, Peter L. Messick, Joel A. Alexa, Edward H. Glaessgen, Benjamin T. Hailer