Patents by Inventor Chris George Georgoulias

Chris George Georgoulias 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).

  • Aircraft overheat detection using optical fiber technology for system health monitoring by determining a physical characteristic associated with a location
    Patent number: 10585006
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Grant
    Filed: May 19, 2017
    Date of Patent: March 10, 2020
    Assignee: Kidde Technologies, Inc.
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • Optical health monitoring for aircraft overheat and fire detection systems
    Patent number: 10436652
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Grant
    Filed: May 19, 2017
    Date of Patent: October 8, 2019
    Assignee: Kidde Technologies, Inc.
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • Optical health monitoring for aircraft overheat and fire detection systems
    Patent number: 10112726
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Grant
    Filed: May 19, 2017
    Date of Patent: October 30, 2018
    Assignee: Kidde Technologies, Inc.
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • Eutectic based continuous thermal sensing element including fiber wrapped center conductor
    Patent number: 9909933
    Abstract: A eutectic sensing element includes an electrically conductive core extending along a first axis to define a length. The core is coated with a coated with a eutectic material formulated to provide desirable thermal response characteristics. The eutectic sensing element further includes an insulating fiber layer disposed on an external surface of the electrically conductive. The insulating fiber layer includes a strand that extends along the length of the electrically conductive core.
    Type: Grant
    Filed: December 9, 2014
    Date of Patent: March 6, 2018
    Assignee: KIDDE TECHNOLOGIES, INC.
    Inventors: Chris George Georgoulias, Doug John Baxendell
  • OPTICAL HEALTH MONITORING FOR AIRCRAFT OVERHEAT AND FIRE DETECTION SYSTEMS
    Publication number: 20170334574
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Application
    Filed: May 19, 2017
    Publication date: November 23, 2017
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • OPTICAL HEALTH MONITORING FOR AIRCRAFT OVERHEAT AND FIRE DETECTION SYSTEMS
    Publication number: 20170336269
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Application
    Filed: May 19, 2017
    Publication date: November 23, 2017
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • AIRCRAFT OVERHEAT DETECTION USING OPTICAL FIBER TECHNOLOGY FOR SYSTEM HEALTH MONITORING
    Publication number: 20170336268
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Application
    Filed: May 19, 2017
    Publication date: November 23, 2017
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • OPTICAL HEALTH MONITORING FOR AIRCRAFT OVERHEAT AND FIRE DETECTION
    Publication number: 20170334575
    Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
    Type: Application
    Filed: May 19, 2017
    Publication date: November 23, 2017
    Inventors: Christopher Wilson, David William Frasure, Mark Thomas Kern, Mark Sherwood Miller, Scott Kenneth Newlin, Chris George Georgoulias, Stefan Coreth, Ken Bell
  • EUTECTIC BASED CONTINUOUS THERMAL SENSING ELEMENT INCLUDING FIBER WRAPPED CENTER CONDUCTOR
    Publication number: 20160161345
    Abstract: A eutectic sensing element includes an electrically conductive core extending along a first axis to define a length. The core is coated with a coated with a eutectic material formulated to provide desirable thermal response characteristics. The eutectic sensing element further includes an insulating fiber layer disposed on an external surface of the electrically conductive. The insulating fiber layer includes a strand that extends along the length of the electrically conductive core.
    Type: Application
    Filed: December 9, 2014
    Publication date: June 9, 2016
    Inventors: Chris George Georgoulias, Doug John Baxendell