Patents by Inventor Jeff ELDREDGE

Jeff ELDREDGE 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: 20200222649
    Abstract: An aspect of the disclosure is related to a medical device for providing an air passageway through a neck of a patient. In one embodiment, the medical device may include: a neckband configured to extend around the neck of the patient, the neckband including a connector positioned along a length of the neckband for positioning along an anterior part of the neck of the patient, the connector including a connector through hole; a cannula having an elongated tube extending from a connecting head, the elongated tube being configured to extend into a trachea of the patient and including an inner passageway, the connecting head having a through hole that is continuous with the inner passageway of the elongated tube thereby allowing air to pass through the cannula into the trachea, the connecting head having an outer diameter that is sized to have a friction fit with the connector through hole.
    Type: Application
    Filed: August 23, 2018
    Publication date: July 16, 2020
    Inventors: Byron Wilson, Harrison Yen, Ethan Young, Jeff Eldredge, Tim Colonius
  • Publication number: 20170131726
    Abstract: An aircraft system includes three or more aircraft and a flight control system. The flight control system controls flight of the aircraft so as to maintain the three aircraft in an inverted-V flight formation. Specifically, two leading aircraft fly along parallel flight paths and maintain substantially identical longitudinal positions along the parallel flight paths. A trailing aircraft flies along a flight path centered between the trailing vortices or flight paths of the leading aircraft and has a longitudinal position that is behind the two leading aircraft. The leading aircraft maintain a lateral separation distance such that the induced drag for the three aircraft formation is minimized for example by setting a lateral separation distance between wingtips of 0.8 to 1.0 wingspan of the trailing aircraft. The longitudinal separation between the leading and trailing aircraft is controlled by the flight control system based on operational objectives of the aircraft system.
    Type: Application
    Filed: November 6, 2015
    Publication date: May 11, 2017
    Inventors: Jason L. SPEYER, Jeff ELDREDGE