Patents by Inventor Nicholas B. Muha

Nicholas B. Muha 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: 11754136
    Abstract: An elastomeric compression spring for isolating vibrations between a first part and a second part. The first part is movable in a direction relative to the second part. The elastomeric compression spring comprises a tube elongated along a central axis of the tube. The central axis of the tube is perpendicular to the direction. The tube is configured to compress in the direction. The tube comprises an outer surface comprising an initial contact line configured to initially receive contact from the first part. The tube further comprises at least one load tuning feature in the outer surface, parallel to the central axis, and circumferentially spaced apart from the initial contact line. The at least one load tuning feature creates a localized change in a thickness of the tube and a stiffness of the elastomeric compression spring at the at least one load tuning feature.
    Type: Grant
    Filed: February 5, 2021
    Date of Patent: September 12, 2023
    Assignee: The Boeing Company
    Inventors: Nicholas B. Muha, Jeremie J. Albert, Douglas R. Ludin
  • Patent number: 11027859
    Abstract: A penetration device including a casing, a propellant positioned in the casing, and a flyer plate. The flyer plate is coupled to the casing and adjacent to the propellant. The flyer plate includes a center portion having a substantially constant first thickness and includes a peripheral portion around the center portion and defining an edge. The peripheral portion includes one or more recesses in a first surface of the peripheral portion.
    Type: Grant
    Filed: October 16, 2017
    Date of Patent: June 8, 2021
    Assignee: THE BOEING COMPANY
    Inventors: Nicholas B. Muha, Jeremie Joel Albert, Robert W. Thomas
  • Publication number: 20210156443
    Abstract: An elastomeric compression spring for isolating vibrations between a first part and a second part. The first part is movable in a direction relative to the second part. The elastomeric compression spring comprises a tube elongated along a central axis of the tube. The central axis of the tube is perpendicular to the direction. The tube is configured to compress in the direction. The tube comprises an outer surface comprising an initial contact line configured to initially receive contact from the first part. The tube further comprises at least one load tuning feature in the outer surface, parallel to the central axis, and circumferentially spaced apart from the initial contact line. The at least one load tuning feature creates a localized change in a thickness of the tube and a stiffness of the elastomeric compression spring at the at least one load tuning feature.
    Type: Application
    Filed: February 5, 2021
    Publication date: May 27, 2021
    Inventors: Nicholas B. Muha, Jeremie J. Albert, Douglas R. Ludin
  • Patent number: 10962073
    Abstract: An elastomeric compression spring for isolating vibrations between a first part and a second part. The first part is movable in a direction relative to the second part. The elastomeric compression spring comprises a tube elongated along a central axis of the tube. The central axis of the tube is perpendicular to the direction. The tube is configured to compress in the direction. The tube comprises an outer surface comprising an initial contact line configured to initially receive contact from the first part. The tube further comprises at least one load tuning feature in the outer surface, parallel to the central axis, and circumferentially spaced apart from the initial contact line. The at least one load tuning feature creates a localized change in a thickness of the tube and a stiffness of the elastomeric compression spring at the at least one load tuning feature.
    Type: Grant
    Filed: July 5, 2018
    Date of Patent: March 30, 2021
    Assignee: The Boeing Company
    Inventors: Nicholas B. Muha, Jeremie J. Albert, Douglas R. Ludin
  • Publication number: 20200011393
    Abstract: An elastomeric compression spring for isolating vibrations between a first part and a second part. The first part is movable in a direction relative to the second part. The elastomeric compression spring comprises a tube elongated along a central axis of the tube. The central axis of the tube is perpendicular to the direction. The tube is configured to compress in the direction. The tube comprises an outer surface comprising an initial contact line configured to initially receive contact from the first part. The tube further comprises at least one load tuning feature in the outer surface, parallel to the central axis, and circumferentially spaced apart from the initial contact line. The at least one load tuning feature creates a localized change in a thickness of the tube and a stiffness of the elastomeric compression spring at the at least one load tuning feature.
    Type: Application
    Filed: July 5, 2018
    Publication date: January 9, 2020
    Inventors: Nicholas B. Muha, Jeremie J. Albert, Douglas R. Ludin
  • Publication number: 20190112077
    Abstract: A penetration device including a casing, a propellant positioned in the casing, and a flyer plate. The flyer plate is coupled to the casing and adjacent to the propellant. The flyer plate includes a center portion having a substantially constant first thickness and includes a peripheral portion around the center portion and defining an edge. The peripheral portion includes one or more recesses in a first surface of the peripheral portion.
    Type: Application
    Filed: October 16, 2017
    Publication date: April 18, 2019
    Inventors: Nicholas B. Muha, Jeremie Joel Albert, Robert W. Thomas
  • Publication number: 20190112076
    Abstract: A penetration device including a casing, a propellant positioned in the casing, and a flyer plate. The flyer plate is coupled to the casing and adjacent to the propellant. The flyer plate includes a center portion having a substantially constant first thickness and includes a peripheral portion around the center portion and defining an edge. The peripheral portion tapers from the first thickness to a second thickness at the edge, where the second thickness is less than the first thickness.
    Type: Application
    Filed: October 16, 2017
    Publication date: April 18, 2019
    Inventors: Jeremie Joel Albert, Nicholas B. Muha, Robert W. Thomas