Patents by Inventor Mark W. Volner

Mark W. Volner 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: 11358733
    Abstract: A system and method for computing and displaying a fuel optimal idle deceleration start point which minimizes the overall auto throttle movement keeping the throttle at idle detent throughout the maneuver thus minimizing the fuel burn and stress on engine. The need for speed brakes deployment is also reduced because the deceleration distance length is accordingly adjusted based on current parameters. The accurate solution takes into account the current condition such as aircraft weight, altitude and speed and environmental parameters such as wind and temperature. The computed deceleration start point is displayed on map/navigation and vertical display for enhanced flight crew awareness.
    Type: Grant
    Filed: March 12, 2020
    Date of Patent: June 14, 2022
    Assignee: Rockwell Collins, Inc.
    Inventors: Bradley R. Mickelson, Mark W. Volner, Dinesh Kumar Kushwaha
  • Patent number: 11320842
    Abstract: A system includes a processing circuit onboard an aircraft and configured to determine an optimum cruise profile for the aircraft based on a flight plan, a characteristic of the aircraft, and an environmental characteristic. The processing circuit is also configured to determine an optimized cruise vertical path based on the optimum cruise profile and air traffic information of at least one other aircraft, and control an autopilot system of the aircraft to cause the aircraft to follow the optimized cruise vertical path.
    Type: Grant
    Filed: September 24, 2019
    Date of Patent: May 3, 2022
    Assignee: Rockwell Collins, Inc.
    Inventors: Dinesh K. Kushwaha, Mark W. Volner, Bradley R. Mickelson
  • Publication number: 20210221529
    Abstract: A system and method for computing and displaying a fuel optimal idle deceleration start point which minimizes the overall auto throttle movement keeping the throttle at idle detent throughout the maneuver thus minimizing the fuel burn and stress on engine. The need for speed brakes deployment is also reduced because the deceleration distance length is accordingly adjusted based on current parameters. The accurate solution takes into account the current condition such as aircraft weight, altitude and speed and environmental parameters such as wind and temperature. The computed deceleration start point is displayed on map/navigation and vertical display for enhanced flight crew awareness.
    Type: Application
    Filed: March 12, 2020
    Publication date: July 22, 2021
    Inventors: Bradley R. Mickelson, Mark W. Volner, Dinesh Kumar Kushwaha
  • Publication number: 20200103924
    Abstract: A system includes a processing circuit onboard an aircraft and configured to determine an optimum cruise profile for the aircraft based on a flight plan, a characteristic of the aircraft, and an environmental characteristic. The processing circuit is also configured to determine an optimized cruise vertical path based on the optimum cruise profile and air traffic information of at least one other aircraft, and control an autopilot system of the aircraft to cause the aircraft to follow the optimized cruise vertical path.
    Type: Application
    Filed: September 24, 2019
    Publication date: April 2, 2020
    Applicant: Rockwell Collins, Inc.
    Inventors: Dinesh K. Kushwaha, Mark W. Volner, Bradley R. Mickelson
  • Patent number: 9583010
    Abstract: Present novel and non-trivial system, device, and method for generating a vertical path profile are disclosed. The vertical path profile generating system is comprised of a source of navigation data, a source of performance factors data, a vertical path generator (“VPG”) and a presentation system. The VPG may be configured to receive the navigation data representative of takeoff runway information; receive the performance data may be representative of aircraft performance factors; determine a first vertical path and/or second vertical path as a function of criteria employing the navigation data and the performance data; generate presentation data responsive to the determination; and provide the presentation data to one or more presentation devices comprised of, in part, a visual display unit configured to display a first takeoff path profile and/or a second takeoff path profile.
    Type: Grant
    Filed: September 25, 2014
    Date of Patent: February 28, 2017
    Assignee: Rockwell Collins, Inc.
    Inventors: Kirk A. Kolek, Norm W. Arons, Mark W. Volner
  • Patent number: 9020665
    Abstract: A present novel and non-trivial system, device, and method for presenting winds aloft symbology on an aircraft display unit are disclosed. Symbology image data representative of a plurality of sets of winds aloft symbologies may be generated as a function of flight plan data and weather data; flight plan data representative flight plan comprised of a plurality of waypoints may be received along with weather data representative of winds aloft data corresponding to each waypoint. Each set of winds aloft symbologies may be comprised of winds aloft symbology corresponding to each waypoint of the flight plan at a single altitude and symbolize winds aloft at that altitude. When provided to a display unit, each set of winds aloft symbologies represented in the symbology image data may be presented in a series of increasing or decreasing altitudes, where the series is presented sequentially or simultaneously.
    Type: Grant
    Filed: June 26, 2013
    Date of Patent: April 28, 2015
    Assignee: Rockwell Collins, Inc.
    Inventors: Michael G. Espenes, Mark W. Volner