Patents by Inventor Douglas Pedersen

Douglas Pedersen 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).

  • Automatic analysis of organization process/operations data
    Patent number: 11151505
    Abstract: A device may receive data associated with one or more healthcare organizations. The data may relate to a performance of one or more processes or operations of the one or more healthcare organizations. The device may process the data using one or more techniques to permit mapping of the data to a healthcare operating model. The device may map the data to the healthcare operating model. The healthcare operating model may be used to perform one or more analyses of the one or more processes or operations of the one or more healthcare organizations. The device may perform one or more analyses of the data to identify one or more deficiencies related to the one or more processes or operations. The device may perform one or more actions to positively impact the performance of the one or more processes or operations of the one or more healthcare organizations.
    Type: Grant
    Filed: October 20, 2017
    Date of Patent: October 19, 2021
    Assignee: Accenture Global Solutions Limited
    Inventors: RaeAnn J. Hancock, Scott Alister, Marjorie P. Bogaert, Denise M. Brock, Amber Brockington, Doreen Colburn, Aakash R. Desai, John M. Froehlich, Betty J. Gillespie, Ninad Gokhale, Amit Jindal, Daniel Huedig, Brian P. Kalis, Franklin C. Lee, Thomas N. Mangan, Gerald J. Meklaus, Aaron Morrow, Jennifer Nichol, Milind Pawar, Douglas Pedersen, Frank Pino, Ann Turner, Cristi Velastegui, Joseph Wee
  • Rotary wing aircraft vibration control system with resonant inertial actuators
    Patent number: 10543911
    Abstract: A control system for resonant inertial actuators estimates operating parameters of the resonant inertial actuators based on voltage and current feedback and dynamically limits selected parameters to maintain the safe, efficient, and cost effective operation of the resonant inertial actuators. Resistance within the electrical drives for the resonant inertial actuators is estimated from the voltage and current feedback and in conjunction with the modeling of the resonant inertial actuators other operating parameters are calculated or otherwise estimated. Having regard for the responsiveness of the resonant inertial actuators to changes in command signals, the command signals are adjusted to dynamically limit the estimated parameters.
    Type: Grant
    Filed: January 16, 2018
    Date of Patent: January 28, 2020
    Assignee: LORD Corporation
    Inventors: Paul Black, Douglas Swanson, Askari Badre-Alam, David Edeal, Douglas Pedersen
  • Rotary wing aircraft vibration control system with resonant inertial actuators
    Patent number: 10308354
    Abstract: A control system for resonant inertial actuators estimates operating parameters of the resonant inertial actuators based on voltage and current feedback and dynamically limits selected parameters to maintain the safe, efficient, and cost effective operation of the resonant inertial actuators. Resistance within the electrical drives for the resonant inertial actuators is estimated from the voltage and current feedback and in conjunction with the modeling of the resonant inertial actuators other operating parameters are calculated or otherwise estimated. Having regard for the responsiveness of the resonant inertial actuators to changes in command signals, the command signals are adjusted to dynamically limit the estimated parameters.
    Type: Grant
    Filed: February 3, 2012
    Date of Patent: June 4, 2019
    Assignee: LORD Corporation
    Inventors: Paul Black, Doug Swanson, Askari Badre-Alam, David Edeal, Douglas Pedersen
  • ROTARY WING AIRCRAFT VIBRATION CONTROL SYSTEM WITH RESONANT INERTIAL ACTUATORS
    Publication number: 20180346106
    Abstract: A control system for resonant inertial actuators estimates operating parameters of the resonant inertial actuators based on voltage and current feedback and dynamically limits selected parameters to maintain the safe, efficient, and cost effective operation of the resonant inertial actuators. Resistance within the electrical drives for the resonant inertial actuators is estimated from the voltage and current feedback and in conjunction with the modeling of the resonant inertial actuators other operating parameters are calculated or otherwise estimated. Having regard for the responsiveness of the resonant inertial actuators to changes in command signals, the command signals are adjusted to dynamically limit the estimated parameters.
    Type: Application
    Filed: January 16, 2018
    Publication date: December 6, 2018
    Inventors: Paul BLACK, Douglas SWANSON, Askari BADRE-ALAM, David EDEAL, Douglas PEDERSEN
  • ROTARY WING AIRCRAFT VIBRATION CONTROL SYSTEM WITH RESONANT INERTIAL ACTUATORS
    Publication number: 20130311012
    Abstract: A control system for resonant inertial actuators estimates operating parameters of the resonant inertial actuators based on voltage and current feedback and dynamically limits selected parameters to maintain the safe, efficient, and cost effective operation of the resonant inertial actuators. Resistance within the electrical drives for the resonant inertial actuators is estimated from the voltage and current feedback and in conjunction with the modeling of the resonant inertial actuators other operating parameters are calculated or otherwise estimated. Having regard for the responsiveness of the resonant inertial actuators to changes in command signals, the command signals are adjusted to dynamically limit the estimated parameters.
    Type: Application
    Filed: February 3, 2012
    Publication date: November 21, 2013
    Applicant: LORD Corporation
    Inventors: Paul Black, Doug Swanson, Askari Badre-Alam, David Edeal, Douglas Pedersen