Patents by Inventor Tejbir Arora

Tejbir Arora 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).

  • Yaw drive tidal turbine system and method
    Patent number: 8777555
    Abstract: A tidal turbine system includes yaw drive for rotating the turbine between a first position associated with tidal flow and a second position associated with tidal ebbs. The yaw drive is capable of moving the tidal turbine to a position where the tidal turbine is pointed substantially directly into the tidal flow in the first position and substantially into the tidal ebb in a second position. A method for harvesting tidal energy includes rotating the tidal turbine between one of the first position and the second position.
    Type: Grant
    Filed: February 21, 2013
    Date of Patent: July 15, 2014
    Assignee: Lockheed Martin Corporation
    Inventors: Benjamin Balbir, Richard J. Handwerg, Tejbir Arora, Richard P. Clark
  • System and method for shock isolation in a launch system
    Patent number: 8534177
    Abstract: A system and method for providing a munitions launching system with dynamic shock isolation in which a spring plate skirt having an integral spring arrangement is provided between a munitions frame and a munitions extension, the spring plate skirt defining an opening that provides for the uninterrupted flow of expelled rocket gases, as well as underside access to the munitions frame.
    Type: Grant
    Filed: March 1, 2010
    Date of Patent: September 17, 2013
    Assignee: Lockheed Martin Corporation
    Inventors: William Kalms, Tejbir Arora, John Snediker
  • SYSTEM AND METHOD FOR SHOCK ISOLATION IN A LAUNCH SYSTEM
    Publication number: 20120104219
    Abstract: A system and method for providing a munitions launching system with dynamic shock isolation in which a spring plate skirt having an integral spring arrangement is provided between a munitions frame and a munitions extension, the spring plate skirt defining an opening that provides for the uninterrupted flow of expelled rocket gases, as well as underside access to the munitions frame.
    Type: Application
    Filed: March 1, 2010
    Publication date: May 3, 2012
    Applicant: Lockheed Martin Corpration
    Inventors: William Kalms, Tejbir Arora, John Snediker