Patents by Inventor Joseph Carmody

Joseph Carmody 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: 11879410
    Abstract: A rocket motor for a gun-fired projectile is configured stiffen the burnable propellant in the rocket motor during burning and/or protect the rocket motor from the pressure that occurs during firing of the projectile from the gun. The rocket motor may include a rigid structure that is integrated into the burnable propellant grain to stabilize the burnable propellant grain during burning of the burnable propellant grain. The rigid structure has a matrix or truss-like shape that extends into the depth of the burnable propellant grain. The rocket motor may include a baffled end cap that covers a nozzle of the rocket motor. The end cap defines a baffled path through the end cap to dampen gas flow into the nozzle and prevent particles of the gun propellant from entering the rocket motor. A rocket motor may implement the rigid structure or the baffled end cap, or both structures.
    Type: Grant
    Filed: February 24, 2021
    Date of Patent: January 23, 2024
    Assignee: Raytheon Company
    Inventors: Joseph A. Carmody, Benjamin C. Hulbert, Ryan J. Paffenroth, Andrew J. Harris
  • Publication number: 20220025835
    Abstract: A rocket motor for a gun-fired projectile is configured stiffen the burnable propellant in the rocket motor during burning and/or protect the rocket motor from the pressure that occurs during firing of the projectile from the gun. The rocket motor may include a rigid structure that is integrated into the burnable propellant grain to stabilize the burnable propellant grain during burning of the burnable propellant grain. The rigid structure has a matrix or truss-like shape that extends into the depth of the burnable propellant grain. The rocket motor may include a baffled end cap that covers a nozzle of the rocket motor. The end cap defines a baffled path through the end cap to dampen gas flow into the nozzle and prevent particles of the gun propellant from entering the rocket motor. A rocket motor may implement the rigid structure or the baffled end cap, or both structures.
    Type: Application
    Filed: February 24, 2021
    Publication date: January 27, 2022
    Inventors: Joseph A. Carmody, Benjamin C. Hulbert, Ryan J. Paffenroth, Andrew J. Harris
  • Publication number: 20070155423
    Abstract: Methods, devices and systems for integrating multiple communication systems including multiple wireless communication protocols into a single system are discussed. In an illustrative example, a communication system includes a device adapted to communicate via first and second wireless communication protocols. The system may further include local area network or other wired sub-network, with the device adapted for first and second protocols also being adapted to operate using the local area network or other wired sub-network.
    Type: Application
    Filed: December 30, 2005
    Publication date: July 5, 2007
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Joseph Carmody, Yu-Gene Chen, Patrick Gonia, Paul McLaughlin