Patents by Inventor Richard Edward Heath

Richard Edward Heath 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: 10913221
    Abstract: A radius filler material positioned at an intersection of a mandrel and a placement surface is heated to form a heated radius filler material. Mechanical pressure is applied to the heated radius filler material to shape the heated radius filler material to a shaped radius filler having a desired shape against a radius of the mandrel. A composite ply is applied over the mandrel and the shaped radius filler.
    Type: Grant
    Filed: August 28, 2018
    Date of Patent: February 9, 2021
    Assignee: The Boeing Company
    Inventors: Richard Alexander Prause, Richard Edward Heath
  • Publication number: 20200070442
    Abstract: A radius filler material positioned at an intersection of a mandrel and a placement surface is heated to form a heated radius filler material. Mechanical pressure is applied to the heated radius filler material to shape the heated radius filler material to a shaped radius filler having a desired shape against a radius of the mandrel. A composite ply is applied over the mandrel and the shaped radius filler.
    Type: Application
    Filed: August 28, 2018
    Publication date: March 5, 2020
    Inventors: Richard Alexander Prause, Richard Edward Heath
  • Patent number: 9993925
    Abstract: Provided are end effectors and methods of using such end effectors for handling various composite structures. An end effector includes a support structure bendable relative the principal axis of the end effector. The support structure is disposed within a cavity partially formed by an engaging portion of the end effector. The engaging portion is formed from a flexible material and includes multiple openings in fluid communication with the cavity. When the engaging portion contacts a composite structure and when the pressure inside the cavity is reduced below the ambient level, the composite structure is forced against the engaging portion due to this pressure differential. The flexibility of the support structure and of the engaging portion allows the end effector to conform to the shape of the composite structure. At the same time, the support structure maintains the shape of the cavity in the directions normal to the principal axis.
    Type: Grant
    Filed: August 25, 2015
    Date of Patent: June 12, 2018
    Assignee: The Boeing Company
    Inventors: Paul D. Shaw, Raviendra S. Suriyaarachchi, Richard Edward Heath
  • Publication number: 20170057100
    Abstract: Provided are end effectors and methods of using such end effectors for handling various composite structures. An end effector includes a support structure bendable relative the principal axis of the end effector. The support structure is disposed within a cavity partially formed by an engaging portion of the end effector. The engaging portion is formed from a flexible material and includes multiple openings in fluid communication with the cavity. When the engaging portion contacts a composite structure and when the pressure inside the cavity is reduced below the ambient level, the composite structure is forced against the engaging portion due to this pressure differential. The flexibility of the support structure and of the engaging portion allows the end effector to conform to the shape of the composite structure. At the same time, the support structure maintains the shape of the cavity in the directions normal to the principal axis.
    Type: Application
    Filed: August 25, 2015
    Publication date: March 2, 2017
    Applicant: The Boeing Company
    Inventors: Paul D. Shaw, Raviendra S. Suriyaarachchi, Richard Edward Heath