Patents by Inventor Emil V. Ardelean

Emil V. Ardelean 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: 20230261433
    Abstract: A system includes one or more diodes, a power source, a tank, and a cooling plate. The power source is coupled to the one or more diodes and the tank is operable to store a fluid under pressure. The cooling plate includes one or more channels configured to receive at least some of the fluid stored in the tank and is operable to transfer heat from the one or more diodes to the fluid through the one or more channels.
    Type: Application
    Filed: February 16, 2022
    Publication date: August 17, 2023
    Inventors: Robert E. Richard, Jonathan D. Kemp, Emil V. Ardelean
  • Patent number: 10358851
    Abstract: A compliant hinge for deployable membrane-like structures and other applications is provided. The compliant hinge generally includes a flexible intermediate portion having one or more enclosed contours connected by inner longitudinal segments along a longitudinal axis of symmetry. The enclosed contours are resiliently deformable in response to an in-plane load, including tension and shear forces. The compliant hinge allows for rotation, bending, and extension, and can interconnect rigid panels in tensioned precision structures and other applications.
    Type: Grant
    Filed: May 9, 2018
    Date of Patent: July 23, 2019
    Assignee: The United States of America as Represented by the Secretary of the Air Force
    Inventors: Emil V. Ardelean, Sungeun K. Jeon, Jeremy A. Banik
  • Patent number: 9970222
    Abstract: A compliant hinge for deployable membrane-like structures and other applications is provided. The compliant hinge generally includes a flexible intermediate portion having one or more enclosed contours connected by inner longitudinal segments along a longitudinal axis of symmetry. The enclosed contours are resiliently deformable in response to an in-plane load, including tension and shear forces. The compliant hinge allows for rotation, bending, and extension, and can interconnect rigid panels in tensioned precision structures and other applications.
    Type: Grant
    Filed: December 17, 2014
    Date of Patent: May 15, 2018
    Assignee: The United States of America as Represented by the Secretary of the Air Force
    Inventors: Emil V. Ardelean, Sungeun K. Jeon, Jeremy A. Banik
  • Patent number: 8544340
    Abstract: An improved test fixture to evaluate thin composite laminates commonly used in deployable space structures. The fixture is designed to impart a pure moment into the coupon, a necessary improvement to prior test methods where results are obtained by fitting material properties in a nonlinear structural analysis of the test. Fixture mechanics allow for direct calculation of the coupon flexural modulus and allowable flexural strain based on two key measurements, fixture displacement and applied load.
    Type: Grant
    Filed: September 26, 2011
    Date of Patent: October 1, 2013
    Assignee: The United States of America as Represented by the Secretary of the Air Force
    Inventors: Emil V. Ardelean, Thomas W. Murphey, Gregory E. Sanford
  • Patent number: 8286498
    Abstract: A standard tensile test device is improved to accurately measure the mechanical properties of stranded cables, ropes, and other composite structures wherein a witness is attached to the top and bottom mounting blocks holding the cable under test. The witness is comprised of two parts: a top and a bottom rod of similar diameter with the bottom rod having a smaller diameter stem on its upper end and the top rod having a hollow opening in its lower end into which the stem fits forming a witness joint. A small gap is present between the top rod and the larger diameter portion of the bottom rod. A standard extensometer is attached to the top and bottom rods of the witness spanning this small witness gap. When a force is applied to separate the mounting blocks, the gap in the witness expands the same length that the entire test specimen is stretched.
    Type: Grant
    Filed: August 9, 2010
    Date of Patent: October 16, 2012
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Lawrence M. Robertson, Emil V. Ardelean, James C. Goodding, Vit Babuska