Patents by Inventor David Blanding

David Blanding 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: 11486477
    Abstract: A method for monitoring remaining useful life (RUL) of an actuation system in a vehicle that includes receiving position data of the actuation system from a position sensor, maintaining a total distance traveled for the actuation system, and calculating the RUL of the actuation system. The calculating includes estimating force data using an output variable estimator, determining motor torque, weighing the estimated force data using a confidence level, predicting a total life of the actuation system based on the weighted force data, and comparing the predicted total life with the total distance traveled to determine the remaining useful life.
    Type: Grant
    Filed: September 10, 2019
    Date of Patent: November 1, 2022
    Assignee: THE BOEING COMPANY
    Inventors: Neal Huynh, David Blanding, Jimmy Quiambao, Jeffrey Coffman
  • Publication number: 20210071742
    Abstract: A method for monitoring remaining useful life (RUL) of an actuation system in a vehicle that includes receiving position data of the actuation system from a position sensor, maintaining a total distance traveled for the actuation system, and calculating the RUL of the actuation system. The calculating includes estimating force data using an output variable estimator, determining motor torque, weighing the estimated force data using a confidence level, predicting a total life of the actuation system based on the weighted force data, and comparing the predicted total life with the total distance traveled to determine the remaining useful life.
    Type: Application
    Filed: September 10, 2019
    Publication date: March 11, 2021
    Inventors: Neal Huynh, David Blanding, Jimmy Quiambao, Jeffrey Coffman
  • Patent number: 10759519
    Abstract: Systems for compensating for force fighting in multi-actuator systems are provided. A drive controller unit comprises a first feedforward controller in communication with a first actuator and configured to receive a drive command signal. A first feedback regulator is configured to output a first feedback input into the first feedforward controller, and to receive as input a first actuator position and a first actuator force. The drive controller unit further comprises a second feedforward controller in communication with a second actuator and configured to receive the drive command signal. A second feedback regulator is configured to output a second feedback input into the second feedforward controller, and to receive as input a second actuator position and a second actuator force. The drive controller unit utilizes both feedforward controllers and both feedback regulators to minimize force fighting while driving a common aileron.
    Type: Grant
    Filed: October 31, 2017
    Date of Patent: September 1, 2020
    Assignee: The Boeing Company
    Inventors: David Blanding, Jeffrey Coffman, Jimmy Quiambao, Neal Van Huynh
  • Publication number: 20190127049
    Abstract: Systems for compensating for force fighting in multi-actuator systems are provided. A drive controller unit comprises a first feedforward controller in communication with a first actuator and configured to receive a drive command signal. A first feedback regulator is configured to output a first feedback input into the first feedforward controller, and to receive as input a first actuator position and a first actuator force. The drive controller unit further comprises a second feedforward controller in communication with a second actuator and configured to receive the drive command signal. A second feedback regulator is configured to output a second feedback input into the second feedforward controller, and to receive as input a second actuator position and a second actuator force. The drive controller unit utilizes both feedforward controllers and both feedback regulators to minimize force fighting while driving a common aileron.
    Type: Application
    Filed: October 31, 2017
    Publication date: May 2, 2019
    Applicant: The Boeing Company
    Inventors: David Blanding, Jeffrey Coffman, Jimmy Quiambao, Neal Van Huynh
  • Patent number: 9016633
    Abstract: A de-icing system and method. An electromechanical actuator heat sink is operable to receive heat from an electromechanical actuator, and a heat distribution element is operable to distribute heat to a surface. A heat transportation device is operable to transport heat from the electromechanical actuator heat sink to the heat distribution element.
    Type: Grant
    Filed: June 13, 2011
    Date of Patent: April 28, 2015
    Assignee: The Boeing Company
    Inventors: Julie Fatemeh Asfia, David Blanding, Jeffrey Coffman
  • Publication number: 20120312925
    Abstract: A de-icing system and method is disclosed. An electromechanical actuator heat sink is operable to receive heat from an electromechanical actuator, and a heat distribution element is operable to distribute heat to a surface. A heat transportation device is operable to transport heat from the electromechanical actuator heat sink to the heat distribution element.
    Type: Application
    Filed: June 13, 2011
    Publication date: December 13, 2012
    Inventors: Julie Fatemeh Asfia, David Blanding, Jeffrey Coffman
  • Publication number: 20060113933
    Abstract: An electromechanical actuator (EMA) is provided. The EMA includes a threaded output ram connectable to a mechanical component and at least one motor module engageable with the output ram for controllably translating the output ram along a linear axis of the output ram. The actuator further includes a torque sensing adaptive control (TSAC) system for monitoring torque within the motor module. The TSAC generates a disengagement command signal when the TSAC system determines torque within the motor module is outside an allowable motor module torque range. The disengagement command signal initiates disengagement of the motor module from the output ram.
    Type: Application
    Filed: December 1, 2005
    Publication date: June 1, 2006
    Inventors: David Blanding, James Peck
  • Publication number: 20050269887
    Abstract: An electrical actuator comprises two or more electrical motors to drive a threaded screw ram. Each motor has an armature that drives a threaded roller screw that is engaged to the threaded screw ram. Each armature of each motor is independently engageable and/or dis-engageable with the ram. The motor armatures are engageable and disengageable by way of threaded roller screws, the ends of which are tapered to enable them to be lifted away from or lowered into engagement with the threaded ram.
    Type: Application
    Filed: June 4, 2004
    Publication date: December 8, 2005
    Applicant: The Boeing Company
    Inventors: David Blanding, Atsuo Watanabe