Patents by Inventor Matt Boyd

Matt Boyd 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: 20170089464
    Abstract: Gaskets, including aircraft gaskets, are disclosed, the gaskets having an elastomeric gel body and substantially incompressible skeletons. The bodies may be pliable and deformable and, in one example, may be comprised of a two-part chemically cured polyurethane that sets up as a gel after mixing with the web so that it is fully integral with the web and so that there is substantially no air bubbles or air pockets left in the web. The web may be a regular shaped web and made of nylon.
    Type: Application
    Filed: November 10, 2015
    Publication date: March 30, 2017
    Inventors: Matt Boyd, Jeff Busby, Kent Boomer, Michael Dry
  • Publication number: 20160208919
    Abstract: An assembly for use on an aircraft wing having an aircraft skin and a fuel tank, the assembly comprising a metal access door for accessing the fuel tank, a metal retainer ring for engaging the wing and the access door. Fasteners removably couple the access door to the retainer ring. A lip, which may be on the wing surface, is configured to receive a perimeter of the access door when the access door is coupled to the retainer ring. A polyurethane elastomeric gel gasket having a metallic skeleton is configured to lay between the access door and a lip of the metal wing surface. Under compression, the polyurethane will deform and squeeze out the edges and flatten so as to provide metal-to-metal contact between the access door and the lip.
    Type: Application
    Filed: March 30, 2016
    Publication date: July 21, 2016
    Inventors: MICHAEL DRY, MATT BOYD, KENT BOOMER, JEFF BUSBY
  • Publication number: 20160131259
    Abstract: Gaskets, including aircraft gaskets, are disclosed, the gaskets having an elastomeric gel body and substantially incompressible skeletons. The bodies may be pliable and deformable and, in one example, may be comprised of a two-part chemically cured polyurethane that sets up as a gel after mixing with the web so that it is fully integral with the web and so that there is substantially no air bubbles or air pockets left in the web. The web may be a regular shaped web and made of nylon.
    Type: Application
    Filed: November 10, 2015
    Publication date: May 12, 2016
    Inventors: Matt Boyd, Jeff Busby, Kent Boomer, Michael Dry
  • Patent number: 9303447
    Abstract: An assembly for use on an aircraft wing having an aircraft skin and a fuel tank, the assembly comprising a metal access door for accessing the fuel tank, a metal retainer ring for engaging the wing and the access door. Fasteners removably couple the access door to the retainer ring. A lip, which may be on the wing surface, is configured to receive a perimeter of the access door when the access door is coupled to the retainer ring. A polyurethane elastomeric gel gasket having a metallic skeleton is configured to lay between the access door and a lip of the metal wing surface. Under compression, the polyurethane will deform and squeeze out the edges and flatten so as to provide metal-to-metal contact between the access door and the lip.
    Type: Grant
    Filed: March 7, 2013
    Date of Patent: April 5, 2016
    Assignee: Aviation Devices & Electronic Components LLC
    Inventors: Michael Dry, Matt Boyd, Kent Boomer, Jeff Busby
  • Publication number: 20160033043
    Abstract: A gasket or tape material for sealing between two members. The gasket or tape material, in one embodiment, includes a skeletal member and/or metallic and/or non-metallic particles. Enclosing the skeletal member and/or particles is a flexible, compressible resilient polyurea body member having a tacky outer surface, the tacky outer surface for engagement between the two members. The resilient body may be comprised of polyurea. The skeletal member may be comprised of a metallic or a non-metallic material, woven or non-woven metallic or non-metallic.
    Type: Application
    Filed: July 31, 2015
    Publication date: February 4, 2016
    Inventors: JEFF BUSBY, MIKE DRY, KENT BOOMER, MATT BOYD
  • Publication number: 20160018000
    Abstract: A sealant is provided for use on an aircraft or other vehicle. The sealant may be used with a gasket. The sealant is a perimeter seal that comprises a polyurea member. The polyurea member is a self-curing, two-component mix. It may cure to a hardness in the range of about 40 to 100 (Shore A). It may maintain an adequate peel strength to withstand multiple thermal and pressure cycling, and may have a working life, wherein it may be shaped, of less than about eleven minutes.
    Type: Application
    Filed: July 14, 2015
    Publication date: January 21, 2016
    Inventors: Jeff Busby, Chad Knight, Kent Boomer, Mike Dry, Matt Boyd
  • Publication number: 20160017999
    Abstract: A gasket for compressible placement between a first surface and a second surface is disclosed. In one embodiment, the gasket has a cellular metal skeleton embedded in a viscoelastic, pliable, deformable tacky polymer body. The skeleton has multiple strands, which connect to form multiple interconnected cells or pores. The skeleton, prior to being encapsulated in the tacky polymer body, is typically about 75% or more void space. The void space is substantially filled in the manufacture of the gasket, with the tacky uncured polymer. The uncured polymer will set up or cure, and then the gasket may be used.
    Type: Application
    Filed: July 17, 2015
    Publication date: January 21, 2016
    Inventors: MATT BOYD, JEFF BUSBY, KENT BOOMER, MIKE DRY, EMILY SAMUELSON
  • Publication number: 20150322988
    Abstract: A thin, cured gel gasket is disclosed, including methods of making the thin gel gasket and the use of the thin gel gasket in an aircraft joint. In one embodiment, the thin gel gasket has no skeleton or other structure and is comprised of only a cured polyurethane gel and has a thickness of less than about 12 mill. It is manufactured using a release film that is adapted in a number of ways to make release from the gel prior to use easier. In one method of making and using the thin gel gasket. it is applied to a joint which is subject to compression, in one embodiment, a lap joint of an aircraft fuselage.
    Type: Application
    Filed: May 5, 2015
    Publication date: November 12, 2015
    Inventors: Jeff Busby, David Schmidt, Kent Boomer, Matt Boyd
  • Publication number: 20150252903
    Abstract: A spacer and gasket assembly is shown for receipt between a static structure having a surface and fastener holes therethrough and a removable structure having a surface and fastener holes. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing surfaces. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a sticky, deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness.
    Type: Application
    Filed: April 28, 2015
    Publication date: September 10, 2015
    Inventors: Matt BOYD, David SCHMIDT, Jeff BUSBY
  • Patent number: 9016697
    Abstract: A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes therethrough and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness.
    Type: Grant
    Filed: March 11, 2013
    Date of Patent: April 28, 2015
    Assignee: Aviation Devices & Electronic Components, LLC
    Inventors: Matt Boyd, Michael Dry, Kent Boomer, Jeff Busby
  • Publication number: 20150069722
    Abstract: Gaskets, including aircraft gaskets, are disclosed, the gaskets having an elastomeric gel body and substantially incompressible skeletons. The bodies may be pliable and deformable and, in one example, may be comprised of a two-part chemically cured polyurethane that sets up as a gel after mixing with the web so that it is fully integral with the web and so that there is substantially no air bubbles or air pockets left in the web. The web may be a regular shaped web and made of nylon.
    Type: Application
    Filed: September 12, 2014
    Publication date: March 12, 2015
    Inventors: Matt Boyd, Jeff Busby, Kent Boomer, Michael Dry
  • Publication number: 20140326830
    Abstract: A single piece gasket is disclosed having a skeletal member, typically metallic, and a pliable body. The pliable body includes a first portion having a first firmness and a second perimeter portion have a firmer consistency. When such a composite body is placed under compression, the perimeter will tend to limit the flow of the softer inner material past the firmer perimeter region or portion of the gasket. In this manner, creep or overrun of the less firm portion material will be reduced.
    Type: Application
    Filed: June 27, 2014
    Publication date: November 6, 2014
    Inventors: Jeff Busby, Kent Boomer, Matt Boyd, Michael Dry
  • Publication number: 20140312574
    Abstract: A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes therethrough and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness.
    Type: Application
    Filed: April 29, 2014
    Publication date: October 23, 2014
    Applicant: Aviation Devices & Electronic Components, L.L.C.
    Inventors: Jeff Busby, Matt Boyd
  • Publication number: 20140167367
    Abstract: A single piece gasket is disclosed having a skeletal member, typically metallic, and a pliable body. The pliable body includes a first portion having a first firmness and a second perimeter portion have a firmer consistency. When such a composite body is placed under compression, the perimeter will tend to limit the flow of the softer inner material past the firmer perimeter region or portion of the gasket. In this manner, creep or overrun of the less firm portion material will be reduced.
    Type: Application
    Filed: May 11, 2012
    Publication date: June 19, 2014
    Applicant: AVIATION DEVICES & ELECTRONIC COMPONENTS, L.L.C.
    Inventors: Jeff Busby, Kent Boomer, Matt Boyd, Michael Dry, Doug Smith
  • Publication number: 20140015204
    Abstract: A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes therethrough and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness.
    Type: Application
    Filed: March 11, 2013
    Publication date: January 16, 2014
    Applicant: Aviation Devices & Electronic Components, L.L.C.
    Inventors: Matt Boyd, Michael Dry, Kent Boomer, Jeff Busby