Patents by Inventor Alexander S. Babazadeh

Alexander S. Babazadeh 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).

  • Flight control system and method of use
    Patent number: 10759520
    Abstract: A flight control system for a flight control surface includes a first actuator control electronics (ACE), a second ACE, a third ACE, a first remote electronics unit (REU), and a second REU. The first ACE is configured to generate a first control signal for the flight control surface. The second ACE is configured to generate a second control signal for the flight control surface. The third ACE is configured to generate a third control signal for the flight control surface. The first REU is coupled to the first ACE and the second ACE, and configured to operate, based on the first control signal and the second control signal, an actuator coupled to the flight control surface. The second REU is coupled to the second ACE and the third ACE, and configured to operate, based on the second control signal and the third control signal, the actuator.
    Type: Grant
    Filed: September 29, 2017
    Date of Patent: September 1, 2020
    Assignee: THE BOEING COMPANY
    Inventor: Alexander S. Babazadeh
  • FLIGHT CONTROL SYSTEM AND METHOD OF USE
    Publication number: 20190100299
    Abstract: A flight control system for a flight control surface includes a first actuator control electronics (ACE), a second ACE, a third ACE, a first remote electronics unit (REU), and a second REU. The first ACE is configured to generate a first control signal for the flight control surface. The second ACE is configured to generate a second control signal for the flight control surface. The third ACE is configured to generate a third control signal for the flight control surface. The first REU is coupled to the first ACE and the second ACE, and configured to operate, based on the first control signal and the second control signal, an actuator coupled to the flight control surface. The second REU is coupled to the second ACE and the third ACE, and configured to operate, based on the second control signal and the third control signal, the actuator.
    Type: Application
    Filed: September 29, 2017
    Publication date: April 4, 2019
    Inventor: Alexander S. Babazadeh