Patents by Inventor Martin G. Andrews

Martin G. Andrews 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).

  • Publication number: 20240109031
    Abstract: The present disclosure provides a system for processing ultramafic material. The system may comprise a reactor for accelerating weathering of said ultramafic material. The reactor may comprise one or more chambers comprising one or more microbes, biological medicators, or enzymatic accelerants to facilitate the weathering of the ultramafic material.
    Type: Application
    Filed: April 19, 2023
    Publication date: April 4, 2024
    Inventors: Stephen J. ROMANIELLO, Brian D. LEY, Douglas O. EDWARDS, Margaret G. ANDREWS, Nathan G. WALWORTH, Thomas ISHOEY, Tom C. GREEN, Francesc MONTSERRAT, Martin VAN DEN BERGHE, Kenneth NEALSON, Devon Barnes COLE, Kelly ERHART
  • Patent number: 10055524
    Abstract: An apparatus is provided for finite element modeling and analysis of a structural product. A pre-processing system may produce a finite element model of a structural product including component parts joined by a fastener. The finite element model may represent the product by respective meshes of elements including shell or solid elements for the component parts, and beam and spring elements for the fastener in which at least one spring element has an axial offset from the shell or solid elements with respect to an axis of the fastener. A processing system may perform a finite element method (FEM) failure analysis of the finite element model under an external load that is transferable from the component parts to the fastener. The FEM failure analysis may produce an output that indicates a behavior of the fastener, and the FEM failure analysis may predict a component failure rate of the fastener based on the behavior.
    Type: Grant
    Filed: April 26, 2016
    Date of Patent: August 21, 2018
    Assignee: The Boeing Company
    Inventors: Hangki Lee, Martin G. Andrews, Madhavadas Ramnath, Andrew R. Anderson, Taeksun Nam, Gerald E. Mabson
  • Publication number: 20170308633
    Abstract: An apparatus is provided for finite element modeling and analysis of a structural product. A pre-processing system may produce a finite element model of a structural product including component parts joined by a fastener. The finite element model may represent the product by respective meshes of elements including shell or solid elements for the component parts, and beam and spring elements for the fastener in which at least one spring element has an axial offset from the shell or solid elements with respect to an axis of the fastener. A processing system may perform a finite element method (FEM) failure analysis of the finite element model under an external load that is transferable from the component parts to the fastener. The FEM failure analysis may produce an output that indicates a behavior of the fastener, and the FEM failure analysis may predict a component failure rate of the fastener based on the behavior.
    Type: Application
    Filed: April 26, 2016
    Publication date: October 26, 2017
    Inventors: Hangki Lee, Martin G. Andrews, Madhavadas Ramnath, Andrew R. Anderson, Taeksun Nam, Gerald E. Mabson
  • Patent number: 9387629
    Abstract: There is provided a method of making a composite hat stiffener. The method has the steps of curing a composite hat stiffener in a hat tool to form a pre-cured composite hat stiffener. The pre-cured composite hat stiffener has a composite hat section, a plurality of composite stiffening plies with a body ply, a wrap ply, and a base ply, all coupled to the composite hat section, wherein the body ply is coupled to a first side of the composite hat section, the wrap ply is coupled to the body ply, and the base ply is coupled to the body ply and the wrap ply, a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies, and an outer ply coupled to the composite hat section. The method further includes bonding the pre-cured composite hat stiffener to a structure surface.
    Type: Grant
    Filed: June 23, 2014
    Date of Patent: July 12, 2016
    Assignee: The Boeing Company
    Inventors: Steven E. Pearson, Matthew M. Whitmer, Rebecca M. Dixon, Jason L. Firko, Douglas G. Marciniak, Kenneth D. Cominsky, Martin G. Andrews
  • 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: 9144948
    Abstract: In an embodiment of the disclosure, there is provided a hat stiffener. The hat stiffener has a cap. The hat stiffener further has a first web and a second web extending from opposite ends of the cap. The first web and the second web are non-linear and include at least one canted portion. The hat stiffener further has a first flange extending outwardly from a first web base portion and a second flange extending outwardly from a second web base portion.
    Type: Grant
    Filed: April 4, 2012
    Date of Patent: September 29, 2015
    Assignee: The Boeing Company
    Inventors: Jason Lawrence Firko, Martin G. Andrews
  • Publication number: 20140299257
    Abstract: There is provided a method of making a composite hat stiffener. The method has the steps of curing a composite hat stiffener in a hat tool to form a pre-cured composite hat stiffener. The pre-cured composite hat stiffener has a composite hat section, a plurality of composite stiffening plies with a body ply, a wrap ply, and a base ply, all coupled to the composite hat section, wherein the body ply is coupled to a first side of the composite hat section, the wrap ply is coupled to the body ply, and the base ply is coupled to the body ply and the wrap ply, a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies, and an outer ply coupled to the composite hat section. The method further includes bonding the pre-cured composite hat stiffener to a structure surface.
    Type: Application
    Filed: June 23, 2014
    Publication date: October 9, 2014
    Inventors: Steven E. Pearson, Matthew M. Whitmer, Rebecca M. Dixon, Jason L. Firko, Douglas G. Marciniak, Kenneth D. Cominsky, Martin G. Andrews
  • Patent number: 8758879
    Abstract: There is provided a composite hat stiffener, a composite hat-stiffened pressure web, and a method of making the same. The composite hat stiffener has a composite hat section having a first side and a second side. The composite hat stiffener further has a plurality of composite stiffening plies coupled to the composite hat section. The plurality of composite stiffening plies include a body ply coupled to the first side of the composite hat section, a wrap ply coupled the body ply, and a base ply coupled to the body ply and the wrap ply. The composite hat stiffener further has a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies. The composite hat stiffener further has an outer ply coupled to the second side of the composite hat section.
    Type: Grant
    Filed: June 24, 2012
    Date of Patent: June 24, 2014
    Assignee: The Boeing Company
    Inventors: Steven E. Pearson, Matthew M. Whitmer, Rebecca M. Dixon, Jason L. Firko, Douglas G. Marciniak, Kenneth D. Cominsky, Martin G. Andrews
  • Publication number: 20130344291
    Abstract: There is provided a composite hat stiffener, a composite hat-stiffened pressure web, and a method of making the same. The composite hat stiffener has a composite hat section having a first side and a second side. The composite hat stiffener further has a plurality of composite stiffening plies coupled to the composite hat section. The plurality of composite stiffening plies include a body ply coupled to the first side of the composite hat section, a wrap ply coupled the body ply, and a base ply coupled to the body ply and the wrap ply. The composite hat stiffener further has a pair of radius filler noodles coupled to the composite hat section and disposed between the plurality of composite stiffening plies. The composite hat stiffener further has an outer ply coupled to the second side of the composite hat section.
    Type: Application
    Filed: June 24, 2012
    Publication date: December 26, 2013
    Applicant: The Boeing Company
    Inventors: Steven E. Pearson, Matthew M. Whitmer, Rebecca M. Dixon, Jason L. Firko, Douglas G. Marciniak, Kenneth D. Cominsky, Martin G. Andrews
  • Publication number: 20130264421
    Abstract: In an embodiment of the disclosure, there is provided a hat stiffener. The hat stiffener has a cap. The hat stiffener further has a first web and a second web extending from opposite ends of the cap. The first web and the second web are non-linear and include at least one canted portion. The hat stiffener further has a first flange extending outwardly from a first web base portion and a second flange extending outwardly from a second web base portion.
    Type: Application
    Filed: April 4, 2012
    Publication date: October 10, 2013
    Applicant: The Boeing Company
    Inventors: Jason Lawrence Firko, Martin G. Andrews