Patents by Inventor Kevin Prodromides

Kevin Prodromides 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: 9234672
    Abstract: An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
    Type: Grant
    Filed: January 20, 2014
    Date of Patent: January 12, 2016
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Darrell Horner, Ross F. Meyer, Albert Kang, Kevin Prodromides, Barrett Fuhrmann, Karl Schroeder, Beth Miller, David P. Gentile, Govind Yadav
  • Publication number: 20140134936
    Abstract: An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
    Type: Application
    Filed: January 20, 2014
    Publication date: May 15, 2014
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Darrell Horner, Ross F. Meyer, Albert Kang, Kevin Prodromides, Barrett Fuhrmann, Karl Schroeder, Beth Miller, David P. Gentile, Govind Yadav
  • Patent number: 8632381
    Abstract: An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
    Type: Grant
    Filed: January 4, 2010
    Date of Patent: January 21, 2014
    Assignee: Honeywell International Inc.
    Inventors: Darrell Horner, Ross F. Meyer, Albert Kang, Kevin Prodromides, Barry Fuhrmann, Karl Schroeder, Beth Miller, David P. Gentile, Govind Yadav
  • Publication number: 20110165828
    Abstract: An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
    Type: Application
    Filed: January 4, 2010
    Publication date: July 7, 2011
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Darrell Horner, Ross F. Meyer, Albert Kang, Kevin Prodromides, Barrett Fuhrmann, Karl Schroeder, Beth Miller, David P. Gentile, Govind Yadav
  • Publication number: 20100240291
    Abstract: An aircraft cabin pressure control system outflow valve includes a frame, a valve element, and a position sensor. The frame is configured to be mounted on an aircraft exterior skin. The valve element is rotationally coupled to the frame, and is coupled to receive an actuation drive force. The valve element is responsive to the actuation drive force to rotate to a position between a closed position and a plurality of open positions. The position sensor is coupled to the frame and is configured to directly sense rotation of the valve element and supply a position signal representative of valve element position.
    Type: Application
    Filed: March 23, 2009
    Publication date: September 23, 2010
    Applicant: Honeywell International Inc.
    Inventors: Justin A. Tanner, Darrell Horner, Ross F. Meyer, Ron Friestad, Kevin Prodromides