Patents by Inventor Corey C. Jordan

Corey C. Jordan 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).

  • Patent number: 10518903
    Abstract: An aerial vehicle launcher including a rail having a first end and a longitudinal axis and a piston movable in a passageway formed in the rail, the piston connected to a carriage by at least two elongate flexible members. The carriage having a support device for releasably engaging the aerial vehicle. Upon the carriage and the aerial vehicle approaching one end of the rail, the support device controllably disengaging the aerial vehicle, permitting the aerial vehicle to be launched. A device is connected to a pressurized gas source, the device controllably providing pressurized gas from the pressurized gas source to the passageway for drivingly moving the piston, the carriage, and aerial vehicle along the rail for launching the aerial vehicle. The device includes a reservoir for holding pressurized gas, the reservoir being a conduit, the pressurized gas in the reservoir providing the driving force for launching the aerial vehicle.
    Type: Grant
    Filed: May 1, 2017
    Date of Patent: December 31, 2019
    Assignee: CIRCOR AEROSPACE, INC.
    Inventors: Russell S. Sirvis, Christopher R. Lovasco, Juan Vasquez, David W. Gass, Corey C. Jordan, Liron Dror, John Nellikunnel, Jeffrey Horning, Christopher Olsen
  • Publication number: 20170313442
    Abstract: An aerial vehicle launcher including a rail having a first end and a longitudinal axis and a piston movable in a passageway formed in the rail, the piston connected to a carriage by at least two elongate flexible members. The carriage having a support device for releasably engaging the aerial vehicle. Upon the carriage and the aerial vehicle approaching one end of the rail, the support device controllably disengaging the aerial vehicle, permitting the aerial vehicle to be launched. A device is connected to a pressurized gas source, the device controllably providing pressurized gas from the pressurized gas source to the passageway for drivingly moving the piston, the carriage, and aerial vehicle along the rail for launching the aerial vehicle. The device includes a reservoir for holding pressurized gas, the reservoir being a conduit, the pressurized gas in the reservoir providing the driving force for launching the aerial vehicle.
    Type: Application
    Filed: May 1, 2017
    Publication date: November 2, 2017
    Inventors: Russell S. SIRVIS, Christopher R. LOVASCO, Juan VASQUEZ, David W. GASS, Corey C. JORDAN, Liron DROR, John NELLIKUNNEL, Jeffrey HORNING, Christopher OLSEN
  • Patent number: 9378909
    Abstract: A spring contact, an inertia switch, and a method of manufacturing an inertia switch are provided. The spring contact includes a conductive body portion having an outer edge and an inner edge partially surrounding an open area, a split in the conductive body portion, the split extending between the outer edge and the inner edge, and a conductive contact finger extending from the inner edge into the open area. The inertia switch includes a shell; a mass movably positioned within the shell; the spring contact positioned within the mass; a biasing member positioned between the spring contact and the header; and a conductive member extending through the header. The biasing member provides a bias between the spring contact within the mass and the conductive member. The method includes at least partially closing the split in the spring contact during insertion of the spring contact within the mass.
    Type: Grant
    Filed: August 18, 2014
    Date of Patent: June 28, 2016
    Assignee: Circor Aerospace, Inc.
    Inventors: David Gass, Brent Salamone, Corey C. Jordan
  • Publication number: 20160049270
    Abstract: A spring contact, an inertia switch, and a method of manufacturing an inertia switch are provided. The spring contact includes a conductive body portion having an outer edge and an inner edge partially surrounding an open area, a split in the conductive body portion, the split extending between the outer edge and the inner edge, and a conductive contact finger extending from the inner edge into the open area. The inertia switch includes a shell; a mass movably positioned within the shell; the spring contact positioned within the mass; a biasing member positioned between the spring contact and the header; and a conductive member extending through the header. The biasing member provides a bias between the spring contact within the mass and the conductive member. The method includes at least partially closing the split in the spring contact during insertion of the spring contact within the mass.
    Type: Application
    Filed: August 18, 2014
    Publication date: February 18, 2016
    Inventors: David GASS, Brent SALAMONE, Corey C. JORDAN
  • Patent number: 5134255
    Abstract: This miniature normally open circuited acceleration switch has a hollow cylindrical casing closed at one end. Its other end is closed by a header having an insulated axial lead wire extending inwardly of the casing, and an electrically conductive ring secured peripherally to the casing. Inside the casing is an internally conical guide sleeve in which is a freely rollable massive ball. A lightweight cup-shaped piston in the guide sleeve carries a contact member spaced by an expanded coil spring from the lead wire. The ball impinges on the piston when a sufficient axially directed force of acceleration is applied to the casing, even if a simultaneous laterally directed force of acceleration is applied thereto. The piston moves axially against the spring bias such that the contact member contacts the lead wire to close the normally open circuited switch.
    Type: Grant
    Filed: March 18, 1991
    Date of Patent: July 28, 1992
    Assignee: Aerodyne Controls Corporation
    Inventors: Leonard P. Tetrault, Corey C. Jordan