Patents by Inventor Scott E. Graham

Scott E. Graham 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).

  • Seeding system with vertical array of nozzles
    Patent number: 11950526
    Abstract: A product on demand nozzle assembly includes a chamber at least partially defined by an external wall and an array of vertically spaced nozzles. Each nozzle has an air inlet, an air and entrained product outlet extending from the external wall, and an entrainment zone between the air inlet and the air and entrained product outlet to receive a product therein to be distributed.
    Type: Grant
    Filed: October 23, 2019
    Date of Patent: April 9, 2024
    Assignee: Deere & Company
    Inventors: Stanley R. Borkgren, William D. Graham, Terry L. Snipes, Elijah B. Garner, Robert T. Casper, Scott C. McCartney, Michael E. Frasier
  • System and method of determining and displaying procedures for an engine-out takeoff for an aircraft
    Patent number: 11851166
    Abstract: A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
    Type: Grant
    Filed: June 15, 2021
    Date of Patent: December 26, 2023
    Assignee: AeroData, Inc.
    Inventors: Terry L. McDonough, Garrett W. van Ark, Scott E. Graham
  • SYSTEM AND METHOD OF DETERMINING AND DISPLAYING PROCEDURES FOR AN ENGINE-OUT TAKEOFF FOR AN AIRCRAFT
    Publication number: 20210354808
    Abstract: A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
    Type: Application
    Filed: June 15, 2021
    Publication date: November 18, 2021
    Inventors: Terry L. McDonough, Garrett W. van Ark, Scott E. Graham
  • System and method of determining and displaying procedures for an engine-out takeoff for an aircraft
    Patent number: 11066181
    Abstract: A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
    Type: Grant
    Filed: October 2, 2020
    Date of Patent: July 20, 2021
    Assignee: AeroData, Inc.
    Inventors: Terry L. McDonough, Garrett W. van Ark, Scott E. Graham
  • SYSTEM AND METHOD OF DETERMINING AND DISPLAYING PROCEDURES FOR AN ENGINE-OUT TAKEOFF FOR AN AIRCRAFT
    Publication number: 20210101695
    Abstract: A system and method of displaying an Engine Failure Awareness Chart (EFAC) for aircraft with at least one engine out is shown and described herein. The EFAC may display lines and zones indicative of levels of risk of obstacles on the ground. The obstacles may be either man-made or natural structures. The EFAC may update continuously providing the pilot with a real-time awareness of the risks around the aircraft during an engine failure. Using the EFAC the pilot may navigate the aircraft to a landing area or back to the airport for landing.
    Type: Application
    Filed: October 2, 2020
    Publication date: April 8, 2021
    Inventors: Terry L. McDonough, Garrett W. van Ark, Scott E. Graham
  • SYSTEM AND METHOD OF DETERMINING AND DISPLAYING AIRCRAFT TAKEOFF AND LANDING PERFORMANCE
    Publication number: 20210101674
    Abstract: A system and method of planning and displaying takeoff brake release points, landing autobrake points, autobrake settings, and last touchdown points based on aircraft-specific performance is shown and described herein. Aircraft information and environmental information may be obtained from aircraft and airport systems. Takeoff brake release points may be determined based on thrust and economic savings for the aircraft and displayed to the pilot. Further, landing autobrake points, autobrake settings, and last touchdown points may be determined and displayed for the aircraft during landing.
    Type: Application
    Filed: October 2, 2020
    Publication date: April 8, 2021
    Inventors: Terry L. McDonough, Garrett W. van Ark, Scott E. Graham