Patents by Inventor Artem Igorevich Grigoryev

Artem Igorevich Grigoryev 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).

  • Man-portable, multi-mode unmanned aerial system launcher
    Patent number: 8894006
    Abstract: A man-portable unmanned aerial system launcher (UAS) launcher includes a rail assembly having an internal track and a carriage assembly having a base configured to translate within the internal track. The carriage assembly also includes a cradle configured to support a UAS and a bracket configured to support the cradle above the base. The UAS launcher includes a launch control system configured to secure the carriage assembly in the launch-ready position until the launch control system receives a launch signal. The UAS launcher also includes one or more elastic members configured to engage the carriage assembly and the rail assembly. Once the carriage assembly is translated to the launch-ready position, strain is applied to the carriage assembly by the one or more elastic members. Release of the carriage assembly enables force generated by strain of the elastic members to propel the carriage assembly toward a launch position.
    Type: Grant
    Filed: April 19, 2012
    Date of Patent: November 25, 2014
    Assignee: Wintec Arrowmaker, Inc.
    Inventors: John Charles Jones, Artem Igorevich Grigoryev, Luis Carlos Espinosa
  • MAN-PORTABLE, MULTI-MODE UNMANNED AERIAL SYSTEM LAUNCHER
    Publication number: 20130277497
    Abstract: A man-portable unmanned aerial system launcher (UAS) launcher includes a rail assembly having an internal track and a carriage assembly having a base configured to translate within the internal track. The carriage assembly also includes a cradle configured to support a UAS and a bracket configured to support the cradle above the base. The UAS launcher includes a launch control system configured to secure the carriage assembly in the launch-ready position until the launch control system receives a launch signal. The UAS launcher also includes one or more elastic members configured to engage the carriage assembly and the rail assembly. Once the carriage assembly is translated to the launch-ready position, strain is applied to the carriage assembly by the one or more elastic members. Release of the carriage assembly enables force generated by strain of the elastic members to propel the carriage assembly toward a launch position.
    Type: Application
    Filed: April 19, 2012
    Publication date: October 24, 2013
    Applicant: WINTEC ARROWMAKER, INC.
    Inventors: John Charles Jones, Artem Igorevich Grigoryev, Luis Carlos Espinosa