Patents by Inventor Larry D. Peterson

Larry D. Peterson 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: 20240124867
    Abstract: The disclosure provides methods and related kits, reagents, and systems for selectively deaminating unmethylated cytosine residues in nucleic acid molecules. In some embodiments, the methods and related kits, reagents, and systems are applied for methods of detecting and/or mapping methylated cytosine residues in nucleic acids. The nucleic can be RNA or DNA. Some embodiments include contacting the polynucleic acid with a bacterial cytosine deaminase, for example DddA or SsdA, or functional fragments or derivatives thereof. Representative DddA and SsdA have sequences set forth in SEQ ID NOS:1 and 2, respectively. The bacterial cytosine deaminases of the disclosure are sensitive to methylation and, thus, deaminate only unmethylated cytosines to provide a cytosine to uracil conversion. The conversion can be detected as a C•G-to-T•A transitions in subsequent sequencing analysis.
    Type: Application
    Filed: March 30, 2022
    Publication date: April 18, 2024
    Applicant: University of Washington
    Inventors: Joseph D. Mougous, Jay Ashok Shendure, Jean-Benoît Lalanne, Snow Brook Peterson, Larry A. Gallagher
  • Patent number: 6608262
    Abstract: An aircraft load cell shoring for placing a wing with an aircraft engine attached to the wing in an unloaded condition and for use with a load cell mounted on an aircraft jack. The aircraft load cell shoring includes a load cell adapter and a shoring contour assembly. The load cell adapter is able to be disposed above the load cell. The shoring contour assembly is an assembly for supporting an aircraft engine, and has a shoring contour assembly bottom portion, and a fixed receptacle located at the shoring contour assembly bottom portion. The load cell adapter communicates with the fixed receptacle. The fixed receptacle is located such that the aircraft jack is aligned with the center of gravity of the engine and enclosed part of the wing.
    Type: Grant
    Filed: July 17, 2001
    Date of Patent: August 19, 2003
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Robert J. Eiswerth, M. Bruce Keen, Larry D. Peterson, Alan M. Saferstein, Rick P. Strickland