Patents by Inventor Joseph R. Renteria

Joseph R. Renteria 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: 11634211
    Abstract: A linear thruster aircraft includes: an airframe, including an elongated mounting nacelle and a main body; an aircraft control unit with a processor, a non-transitory memory, and an input/output component; and at least one linear thruster arrangement with at least four thrusters mounted along at least one elongated axis of the elongated mounting nacelle, such that the thrusters are configured to provide lift, pitch, roll, and yaw movement. Optionally, the linear thruster arrangement can include alternating lateral and vertical offsets of the thrusters from the elongated axis, and pairs of thrusters can be vertically overlapping.
    Type: Grant
    Filed: December 28, 2020
    Date of Patent: April 25, 2023
    Inventor: Joseph R. Renteria
  • Publication number: 20210114724
    Abstract: A linear thruster aircraft includes: an airframe, including an elongated mounting nacelle and a main body; an aircraft control unit with a processor, a non-transitory memory, and an input/output component; and at least one linear thruster arrangement with at least four thrusters mounted along at least one elongated axis of the elongated mounting nacelle, such that the thrusters are configured to provide lift, pitch, roll, and yaw movement. Optionally, the linear thruster arrangement can include alternating lateral and vertical offsets of the thrusters from the elongated axis, and pairs of thrusters can be vertically overlapping.
    Type: Application
    Filed: December 28, 2020
    Publication date: April 22, 2021
    Inventor: Joseph R. Renteria
  • Publication number: 20180354609
    Abstract: A linear thruster aircraft includes, an aircraft body; an air craft control unit with a processor, a non-transitory memory, and an input/output component; and at least one linear thruster arrangement with at least four thrusters mounted along at least one elongated axis of the aircraft body, such that the thrusters are configured to provide lift, pitch, roll, and yaw movement. Optionally, the linear thruster arrangement can include an alternating lateral offset of the thrusters from the elongated axis.
    Type: Application
    Filed: January 3, 2018
    Publication date: December 13, 2018
    Inventor: Joseph R. Renteria