Patents by Inventor Scott Kenneth Newlin

Scott Kenneth Newlin 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: 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
  • 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
  • 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
  • Patent number: 9153400
    Abstract: An integrated switch to indicate pressure changes in an environment includes a housing with a cavity between a first retainer portion and a second retainer portion, a first diaphragm held in the cavity of the housing to indicate fault conditions, and a second diaphragm held in the cavity of the housing to indicate alarm conditions.
    Type: Grant
    Filed: March 15, 2013
    Date of Patent: October 6, 2015
    Assignee: Kidde Technologies, Inc.
    Inventors: David Frasure, Steven Wallace, Harlan Hagge, Scott Kenneth Newlin
  • Publication number: 20140262723
    Abstract: An integrated switch to indicate pressure changes in an environment includes a housing with a cavity between a first retainer portion and a second retainer portion, a first diaphragm held in the cavity of the housing to indicate fault conditions, and a second diaphragm held in the cavity of the housing to indicate alarm conditions.
    Type: Application
    Filed: March 15, 2013
    Publication date: September 18, 2014
    Applicant: KIDDE TECHNOLOGIES, INC.
    Inventors: David Frasure, Steven Wallace, Harlan Hagge, Scott Kenneth Newlin