Patents by Inventor Yoav Efraty

Yoav Efraty 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: 10474167
    Abstract: A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
    Type: Grant
    Filed: August 11, 2017
    Date of Patent: November 12, 2019
    Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
    Inventors: Guy Dekel, Lior Zivan, Yoav Efraty, Amit Wolff, Avner Volovick
  • Publication number: 20180002004
    Abstract: A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
    Type: Application
    Filed: August 11, 2017
    Publication date: January 4, 2018
    Inventors: Guy DEKEL, Lior ZIVAN, Yoav EFRATY, Amit WOLFF, Avner VOLOVICK
  • Patent number: 9731818
    Abstract: A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
    Type: Grant
    Filed: January 10, 2013
    Date of Patent: August 15, 2017
    Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
    Inventors: Guy Dekel, Lior Zivan, Yoav Efraty, Amit Wolff, Avner Volovick
  • Patent number: 9540100
    Abstract: A control system configured to control an acceleration of an air vehicle which comprises a tiltable propulsion unit that is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle, the control system comprising: (a) an input interface for receiving information indicative of a monitored airspeed of the air vehicle; and (b) a control unit, configured to issue controlling commands to a controller of the tiltable propulsion unit for controlling the acceleration of the air vehicle.
    Type: Grant
    Filed: September 12, 2013
    Date of Patent: January 10, 2017
    Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
    Inventors: Guy Dekel, Lior Zivan, Yoav Efraty, Amit Wolff, Avner Volovick
  • Publication number: 20150197335
    Abstract: A control system configured to control an acceleration of an air vehicle which comprises a tiltable propulsion unit that is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle, the control system comprising: (a) an input interface for receiving information indicative of a monitored airspeed of the air vehicle; and (b) a control unit, configured to issue controlling commands to a controller of the tiltable propulsion unit for controlling the acceleration of the air vehicle.
    Type: Application
    Filed: September 12, 2013
    Publication date: July 16, 2015
    Inventors: Guy Dekel, Lior Zivan, Yoav Efraty, Amit Wolff, Avner Volovick
  • Publication number: 20140339372
    Abstract: A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
    Type: Application
    Filed: January 10, 2013
    Publication date: November 20, 2014
    Inventors: Guy Dekel, Lior Zivan, Yoav Efraty, Amit Wolff, Avner Volvoick