Patents by Inventor David R. Nielson

David R. Nielson 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: 20240131403
    Abstract: Disclosed herein is a golf club head comprising at least one crown opening and at least one crown insert attached to the body and covering the at least one crown opening. The golf club head further comprises at least one sole opening and at least one sole insert attached to the body and covering the at least one sole opening. The golf club head additionally includes at least one weight member configured to clamp first and second ledges at selected locations along a sliding weight track. The golf club head also comprise a coefficient of restitution (COR) feature located on the sole of the golf club head. The at least one crown insert is formed from a composite material having a density between 1 g/cc and 2 g/cc. The at least one sole insert is formed from a composite material having a density between 1 g/cc and 2 g/cc.
    Type: Application
    Filed: July 18, 2023
    Publication date: April 25, 2024
    Inventors: Matthew Johnson, David Bennett, Joseph Hoffman, Joseph R. Nielson, Nathan T. Sargent, Christopher J. Harbert, Jared Guttmann, Christian R. Wester, Jake Feuerstein, Mattieu Bovee
  • Patent number: 4104637
    Abstract: A VOR monitoring system responds to the phase difference between two signals to determine the bearing of an aircraft with reference to a transmitting station. Even harmonic distortion interference in the monitored signals produces a bearing error and when the bearing error exceeds a preset limit the monitor of the present invention energizes an alarm. The two monitored signals are identified as a 30 Hz reference and 30 Hz variable signal, each of which is doubled in frequency to 60 Hz and divided by three to produce two 20 Hz signals. One of the 20 Hz signals is identified as a positive error signal and the second as a negative error signal. The negative error signal is phase delayed through a programmable delay by an amount related to the bearing of an aircraft with respect to a transmitting field station. The two error signals are then phase compared and the difference tested against a preset bearing error limit.
    Type: Grant
    Filed: October 27, 1976
    Date of Patent: August 1, 1978
    Assignee: E-Systems, Inc.
    Inventor: David R. Nielson