Patents by Inventor Douglas B Kirkland

Douglas B Kirkland 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: 10988237
    Abstract: A method and apparatus for controlling movement of a component in a system by a plurality of actuators. An operation actuation command to move the component is received. For each of the plurality of actuators, the operation actuation command is used to generate a feed-forward equalization command for the actuator, the feed-forward equalization command for the actuator is combined with the operation actuation command to provide an equalized actuation command for the actuator, and the actuator is controlled to move the component using the equalized actuation command for the actuator.
    Type: Grant
    Filed: December 17, 2019
    Date of Patent: April 27, 2021
    Assignee: The Boeing Company
    Inventors: Douglas B. Kirkland, Eyhab A. Saeed
  • Patent number: 8855943
    Abstract: A system and methods for actuator fatigue monitoring is disclosed. At least two measured actuator forces are received from at least two actuators respectively, and a hybrid force is calculated. The hybrid force is calculated based on a force fight of the at least two actuators calculated based on the at least two measured actuator forces, and a monitored actuator force among the at least two measured actuator forces. An air load of the at least two actuators is estimated based on the at least two measured actuator forces, and a fatigue anomaly is determined based on the hybrid force and the air load.
    Type: Grant
    Filed: October 31, 2011
    Date of Patent: October 7, 2014
    Assignee: The Boeing Company
    Inventors: Gen Matsui, Douglas B. Kirkland
  • Patent number: 8474752
    Abstract: An actuation system including a plurality of actuators; a plurality of position sensors coupled to the actuators, the plurality of position sensors providing rate feedback signals proportional to an actuator rate; a plurality of force sensors coupled to the actuators, the plurality of force sensors providing delta pressure signals; and a feedback control loop configured to receive the rate feedback signals and delta pressure signals and compute a difference in actual actuator rates and sum the difference with a computed difference in actuator forces to generate actuator positioning commands that equalize the actuator forces on a control surface.
    Type: Grant
    Filed: August 20, 2012
    Date of Patent: July 2, 2013
    Assignee: The Boeing Company
    Inventor: Douglas B. Kirkland
  • Publication number: 20130026298
    Abstract: An actuation system including a plurality of actuators; a plurality of position sensors coupled to the actuators, the plurality of position sensors providing rate feedback signals proportional to an actuator rate; a plurality of force sensors coupled to the actuators, the plurality of force sensors providing delta pressure signals; and a feedback control loop configured to receive the rate feedback signals and delta pressure signals and compute a difference in actual actuator rates and sum the difference with a computed difference in actuator forces to generate actuator positioning commands that equalize the actuator forces on a control surface.
    Type: Application
    Filed: August 20, 2012
    Publication date: January 31, 2013
    Applicant: The Boeing Company
    Inventor: Douglas B. Kirkland
  • Patent number: 8245967
    Abstract: An actuation system including a plurality of actuators; a plurality of position sensors coupled to the actuators, the plurality of position sensors providing rate feedback signals proportional to an actuator rate; a plurality of force sensors coupled to the actuators, the plurality of force sensors providing delta pressure signals; and a feedback control loop configured to receive the rate feedback signals and delta pressure signals and compute a difference in actual actuator rates and sum the difference with a computed difference in actuator forces to generate actuator positioning commands that equalize the actuator forces on a control surface.
    Type: Grant
    Filed: November 25, 2008
    Date of Patent: August 21, 2012
    Assignee: The Boeing Company
    Inventor: Douglas B. Kirkland
  • Publication number: 20100127132
    Abstract: An actuation system including a plurality of actuators; a plurality of position sensors coupled to the actuators, the plurality of position sensors providing rate feedback signals proportional to an actuator rate; a plurality of force sensors coupled to the actuators, the plurality of force sensors providing delta pressure signals; and a feedback control loop configured to receive the rate feedback signals and delta pressure signals and compute a difference in actual actuator rates and sum the difference with a computed difference in actuator forces to generate actuator positioning commands that equalize the actuator forces on a control surface.
    Type: Application
    Filed: November 25, 2008
    Publication date: May 27, 2010
    Inventor: Douglas B. Kirkland
  • Patent number: 7640281
    Abstract: A method is provided to reduce delay in signal processing of a digital control system. The method includes receiving outputs from a digital controller at a first frequency. A pre-load data value is then loaded into an accumulator register and output to a digital to analog converter (DAC). In one preferred embodiment, the pre-load data value is the value of the current digital controller output. In another preferred embodiment, the pre-load data value is the value of a previous digital controller output. The method additionally includes computing a step increment value that includes the difference between the most recent value output from the digital controller and the value output by the digital controller just prior to the most recent value. The step increment value is added to the pre-load data value in the accumulator register to create an augmented value, which is then output to the DAC.
    Type: Grant
    Filed: May 18, 2004
    Date of Patent: December 29, 2009
    Assignee: The Boeing Company
    Inventor: Douglas B Kirkland