Patents by Inventor Steven E. Pearson

Steven E. Pearson 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: 11794873
    Abstract: An auxiliary power unit enclosure of an aircraft includes a space frame configured to carry a load and defining an auxiliary power unit compartment. The space frame includes a plurality of frame elements coupled together at a plurality of nodes. The auxiliary power unit enclosure also includes a fairing coupled to and surrounding the space frame.
    Type: Grant
    Filed: March 8, 2019
    Date of Patent: October 24, 2023
    Assignee: The Boeing Company
    Inventors: Steven E. Pearson, Rosario Vingiani, Rajagopalan Margessery, Bernhard Dopker, Richard R. Rosman
  • Publication number: 20200283117
    Abstract: An auxiliary power unit enclosure of an aircraft includes a space frame configured to carry a load and defining an auxiliary power unit compartment. The space frame includes a plurality of frame elements coupled together at a plurality of nodes. The auxiliary power unit enclosure also includes a fairing coupled to and surrounding the space frame.
    Type: Application
    Filed: March 8, 2019
    Publication date: September 10, 2020
    Applicant: The Boeing Company
    Inventors: Steven E. Pearson, Rosario Vingiani, Rajagopalan Margessery, Bernhard Dopker, Richard R. Rosman
  • 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
  • Patent number: 6619733
    Abstract: A passenger headrest is platform deployable and stowable from a passenger seat. The platform operates as a rear headrest and is pivoted to a forward position to serve as a forward leaning face-headrest. The headrest includes a headrest platform that is attached to an adjustable post made of tubular construction and having a plurality of holes. The adjustable post is concentrically dimensioned to be slidably received by a tubular bar. The tubular bar has a set of holes and is pivotably attached to the passenger seat. A first connector secures the adjustable post and tubular bar to each other. The headrest is pivotable through a range of motion adjusted by a passenger, wherein the passenger selects an inclination angle. The inclination angle used by the passenger is established via a second connector that secures the tubular bar to the seat.
    Type: Grant
    Filed: November 19, 2001
    Date of Patent: September 16, 2003
    Assignee: The Boeing Company
    Inventor: Steven E. Pearson
  • Publication number: 20030094843
    Abstract: A passenger headrest is platform deployable and stowable from a passenger seat. The platform operates as a rear headrest and is pivoted to a forward position to serve as a forward leaning face-headrest. The headrest includes a headrest platform that is attached to an adjustable post made of tubular construction and having a plurality of holes. The adjustable post is concentrically dimensioned to be slidably received by a tubular bar. The tubular bar has a set of holes and is pivotably attached to the passenger seat. A first connector secures the adjustable post and tubular bar to each other. The headrest is pivotable through a range of motion adjusted by a passenger, wherein the passenger selects an inclination angle. The inclination angle used by the passenger is established via a second connector that secures the tubular bar to the seat.
    Type: Application
    Filed: November 19, 2001
    Publication date: May 22, 2003
    Inventors: Thomas M. Jensen, Steven E. Pearson