Patents by Inventor Jeremie J. Albert

Jeremie J. Albert 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
  • 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
  • Patent number: 9352845
    Abstract: A storage container, which may be a fuel bladder, includes a container wall configured to retain a fluid within the container and an opening through the container wall. The container includes a rim of the container wall surrounding the opening and a non-planar flex region of the container wall adjacent to the rim. The flex region includes at least one resilient crease in the container wall and the rim is between the flex region and the opening. A portion of the container wall surrounds the flex region. The flex region exhibits the property of allowing movement of the rim with respect to the portion of the container wall.
    Type: Grant
    Filed: February 9, 2012
    Date of Patent: May 31, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Jeremie J. Albert, Martin G. Andrews, Jason L. Firko
  • Patent number: 9334061
    Abstract: A tank system may include a tank having a tank volume and mounted in a vehicle having a system CG and a system CG offset limit. The tank system may further include at least one outer baffle having an outer baffle port and dividing the tank volume into an inner compartment and at least one outer compartment. The outer baffle may be positioned such that when the outer baffle port is open and the combined volume of liquid in the inner and outer compartment is less than a total inner compartment volume, the system CG may exceed the system CG offset limit during a shift of a liquid CG, and when the outer baffle port is closed and the outer compartment is substantially empty of liquid, the system CG remains within the system CG offset limit during a shift of the liquid CG for at least one fill level of the inner compartment.
    Type: Grant
    Filed: January 24, 2014
    Date of Patent: May 10, 2016
    Assignee: The Boeing Company
    Inventors: Jeremie J. Albert, Jeffrey M. Thomas
  • Publication number: 20150259081
    Abstract: Apparatus and methods described herein provide for a structural armor configured to provide load-bearing capabilities to a structure, as well as to provide protection from hypervelocity impacts. According to one aspect of the disclosure provided herein, the structural armor may include two armor facesheets, with an angular member core disposed between. The angular member core may include a number of nodes abutting the armor facesheets, with angular members intersecting at the nodes at acute node angles from the armor facesheets and extending between the armor facesheets. The acute node angles correspond with estimated spread angles of a debris field resulting from an impact of an object with an armor facesheet while moving at hypervelocity speed.
    Type: Application
    Filed: March 13, 2014
    Publication date: September 17, 2015
    Applicant: The Boeing Company
    Inventors: Jeremie J. Albert, Richard R Laverty, Jonathan W. Gabrys, Russell F. Graves
  • Publication number: 20150210162
    Abstract: A tank system may include a tank having a tank volume and mounted in a vehicle having a system CG and a system CG offset limit. The tank system may further include at least one outer baffle having an outer baffle port and dividing the tank volume into an inner compartment and at least one outer compartment. The outer baffle may be positioned such that when the outer baffle port is open and the combined volume of liquid in the inner and outer compartment is less than a total inner compartment volume, the system CG may exceed the system CG offset limit during a shift of a liquid CG, and when the outer baffle port is closed and the outer compartment is substantially empty of liquid, the system CG remains within the system CG offset limit during a shift of the liquid CG for at least one fill level of the inner compartment.
    Type: Application
    Filed: January 24, 2014
    Publication date: July 30, 2015
    Applicant: THE BOEING COMPANY
    Inventors: Jeremie J. Albert, Jeffrey M. Thomas