Patents by Inventor Jeremy Nathaniel Montgomery

Jeremy Nathaniel Montgomery 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).

  • Electronic rudder bias system
    Patent number: 10745141
    Abstract: A rudder bias system for an aircraft with a right engine and a left engine includes a component determining a left and right primary and secondary thrust estimates. The system includes a left engine thrust estimate selector determining a left selected estimate based on the left thrust estimates and a right engine thrust estimate selector determining a right selected estimate based on the right thrust estimates. The system includes an enable and mode component determining one or more corresponding validities for the thrust estimates. The system includes a control component generating an engage command based on a thrust differential between the right engine and the left engine, calculated from the left selected estimate and the right selected estimate and a torque command based on an equivalent pedal force assistance calculated as a difference between the thrust differential and an activation threshold.
    Type: Grant
    Filed: December 1, 2016
    Date of Patent: August 18, 2020
    Assignee: HONDA PATENTS & TECHNOLOGIES NORTH AMERICA, LLC
    Inventors: Jukka Matti Hirvonen, Nilesh Arun Sahani, Jeremy Nathaniel Montgomery
  • ELECTRONIC RUDDER BIAS SYSTEM
    Publication number: 20190009922
    Abstract: A rudder bias system for an aircraft with a right engine and a left engine includes a component determining a left and right primary and secondary thrust estimates. The system includes a left engine thrust estimate selector determining a left selected estimate based on the left thrust estimates and a right engine thrust estimate selector determining a right selected estimate based on the right thrust estimates. The system includes an enable and mode component determining one or more corresponding validities for the thrust estimates. The system includes a control component generating an engage command based on a thrust differential between the right engine and the left engine, calculated from the left selected estimate and the right selected estimate and a torque command based on an equivalent pedal force assistance calculated as a difference between the thrust differential and an activation threshold.
    Type: Application
    Filed: December 1, 2016
    Publication date: January 10, 2019
    Inventors: Jukka Matti Hirvonen, Nilesh Arun Sahani, Jeremy Nathaniel Montgomery