Patents by Inventor Sam Arjunan

Sam Arjunan 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: 20110036940
    Abstract: A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and an assembly for connecting the upstream portion to the downstream portion. The assembly may comprise dual concentric valve actuators and/or a variety of system load limiting features.
    Type: Application
    Filed: January 8, 2010
    Publication date: February 17, 2011
    Inventors: Peter M. Shultz, Carlos A. Fenny, Todd Walker, Sam Arjunan
  • Patent number: 7890222
    Abstract: A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and an assembly for connecting the upstream portion to the downstream portion. The assembly may comprise dual concentric valve actuators and/or a variety of system load limiting features.
    Type: Grant
    Filed: January 8, 2010
    Date of Patent: February 15, 2011
    Assignee: Textron Innovations Inc.
    Inventors: Peter M. Shultz, Carlos A. Fenny, Todd Walker, Sam Arjunan
  • Patent number: 7668627
    Abstract: A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the upstream portion to the downstream portion. The booster means may comprise dual concentric valve actuators and/or a variety of system load limiting features.
    Type: Grant
    Filed: October 13, 2005
    Date of Patent: February 23, 2010
    Assignee: Bell Helicopter Textron Inc.
    Inventors: Peter M. Shultz, Carlos A. Fenny, Todd Walker, Sam Arjunan
  • Publication number: 20080065278
    Abstract: A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the upstream portion to the downstream portion. The booster means may comprise dual concentric valve actuators and/or a variety of system load limiting features.
    Type: Application
    Filed: October 13, 2005
    Publication date: March 13, 2008
    Inventors: Peter Shultz, Carlos Fenny, Todd Walker, Sam Arjunan