Patents by Inventor Matthew M. Whitmer

Matthew M. Whitmer 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: 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
  • 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