Patents by Inventor Mitchell Zachary Kotlik

Mitchell Zachary Kotlik 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).

  • Composite sandwich panels with over-crushed edge regions
    Patent number: 11926077
    Abstract: A composite sandwich panel comprises a first composite skin, a second composite skin, a hollow cell core between the first composite skin and the second composite skin, and a first over-crush edge region with a first edge. The first edge has a first thickness at least 40% less than a nominal thickness of the composite sandwich panel. The first over-crush edge region has a length of at least 0.25 inches over which a thickness of the composite sandwich panel decreases.
    Type: Grant
    Filed: August 3, 2022
    Date of Patent: March 12, 2024
    Assignee: The Boeing Company
    Inventors: Jason Turner, Mitchell Zachary Kotlik, Christopher Robert Schwartz, Michael B. Black
  • Composite Sandwich Panels with Over-Crushed Edge Regions
    Publication number: 20220371234
    Abstract: A composite sandwich panel comprises a first composite skin, a second composite skin, a hollow cell core between the first composite skin and the second composite skin, and a first over-crush edge region with a first edge. The first edge has a first thickness at least 40% less than a nominal thickness of the composite sandwich panel. The first over-crush edge region has a length of at least 0.25 inches over which a thickness of the composite sandwich panel decreases.
    Type: Application
    Filed: August 3, 2022
    Publication date: November 24, 2022
    Inventors: Jason Turner, Mitchell Zachary Kotlik, Christopher Robert Schwartz, Michael B. Black
  • Composite sandwich panels with over-crushed edge regions
    Patent number: 11440283
    Abstract: A composite sandwich panel comprises a first composite skin, a second composite skin, a hollow cell core between the first composite skin and the second composite skin, and a first over-crush edge region with a first edge. The first edge has a first thickness at least 40% less than a nominal thickness of the composite sandwich panel. The first over-crush edge region has a length of at least 0.25 inches over which a thickness of the composite sandwich panel decreases.
    Type: Grant
    Filed: February 2, 2018
    Date of Patent: September 13, 2022
    Assignee: The Boeing Company
    Inventors: Jason Turner, Mitchell Zachary Kotlik, Christopher Robert Schwartz, Michael B. Black
  • Composite Sandwich Panels with Over-Crushed Edge Regions
    Publication number: 20190240949
    Abstract: A composite sandwich panel comprises a first composite skin, a second composite skin, a hollow cell core between the first composite skin and the second composite skin, and a first over-crush edge region with a first edge. The first edge has a first thickness at least 40% less than a nominal thickness of the composite sandwich panel. The first over-crush edge region has a length of at least 0.25 inches over which a thickness of the composite sandwich panel decreases.
    Type: Application
    Filed: February 2, 2018
    Publication date: August 8, 2019
    Inventors: Jason Turner, Mitchell Zachary Kotlik, Christopher Robert Schwartz, Michael B. Black