Patents by Inventor Thomas M. Rusak

Thomas M. Rusak 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: 9405312
    Abstract: An active control column transitionable to a fully passive state for an aircraft and methods of use are provided. The control column includes a passive feedback arrangement, a stick and a ground lock mechanism is provided. The passive feedback arrangement is moveable relative to a mechanical ground to adjust a feedback profile provided to the stick. The stick is movable relative to the mechanical ground and the passive feedback arrangement. The ground lock mechanism has a locked state in which the passive feedback arrangement is maintained in a fixed position relative to the mechanical ground. This places the control column in a fully passive state. The ground lock mechanism also has a normal state in which the passive feedback arrangement is permitted to move relative to the mechanical ground such that active feedback can be provided to the stick.
    Type: Grant
    Filed: July 28, 2010
    Date of Patent: August 2, 2016
    Assignee: Woodward MPC, Inc.
    Inventors: Darryl S. Stachniak, Thomas M. Rusak
  • Patent number: 9051045
    Abstract: An indirect drive active control column for an aircraft control system is provided. The indirect drive active control column provides both active and passive feedback to the control stick. The passive feedback relates to adjustments of the control stick relative to a feedback neutral position. The active feedback actively adjusts the position of the feedback neutral position to adjust a feedback profile of the passive feedback.
    Type: Grant
    Filed: July 28, 2010
    Date of Patent: June 9, 2015
    Assignee: Woodward MPC, Inc.
    Inventors: Darryl S. Stachniak, Thomas M. Rusak, Brian P. Dyra
  • Publication number: 20120025030
    Abstract: An indirect drive active control column for an aircraft control system is provided. The indirect drive active control column provides both active and passive feedback to the control stick. The passive feedback relates to adjustments of the control stick relative to a feedback neutral position. The active feedback actively adjusts the position of the feedback neutral position to adjust a feedback profile of the passive feedback.
    Type: Application
    Filed: July 28, 2010
    Publication date: February 2, 2012
    Applicant: WOODWARD MPC, INC.
    Inventors: Darryl S. Stachniak, Thomas M. Rusak, Brian P. Dyra
  • Publication number: 20120025031
    Abstract: An active control column transitionable to a fully passive state for an aircraft and methods of use are provided. The control column includes a passive feedback arrangement, a stick and a ground lock mechanism is provided. The passive feedback arrangement is moveable relative to a mechanical ground to adjust a feedback profile provided to the stick. The stick is movable relative to the mechanical ground and the passive feedback arrangement. The ground lock mechanism has a locked state in which the passive feedback arrangement is maintained in a fixed position relative to the mechanical ground. This places the control column in a fully passive state. The ground lock mechanism also has a normal state in which the passive feedback arrangement is permitted to move relative to the mechanical ground such that active feedback can be provided to the stick.
    Type: Application
    Filed: July 28, 2010
    Publication date: February 2, 2012
    Applicant: WOODWARD MPC, INC.
    Inventors: Darryl S. Stachniak, Thomas M. Rusak