Patents by Inventor Jeffrey Bernett

Jeffrey Bernett 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: 9555891
    Abstract: An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
    Type: Grant
    Filed: November 26, 2011
    Date of Patent: January 31, 2017
    Assignee: The Boeing Company
    Inventors: James A. Fullerton, Scott E. Coburn, R. Klaus Brauer, Blake Emery, Sebastian Petry, Jeffrey Bernett, Don Chadwick, David Wykes
  • Patent number: 8967743
    Abstract: A furniture component includes a base having a back wall with a first outer vertical face, a first inner vertical face and a first upper edge. A pair of horizontally spaced apart side walls each have a second outer vertical face, a second inner vertical face and a second upper edge. The first and second upper edges are substantially coplanar. An outer top includes a bottom surface spaced above the first and second upper edges and defines a visible gap therebetween. The outer top has a rear edge and a pair of horizontally spaced apart side edges. The rear edge and the first outer vertical face are substantially coplanar, and the side edges and second outer vertical faces are substantially coplanar. A method of assembling and using the furniture component are also provided.
    Type: Grant
    Filed: June 9, 2011
    Date of Patent: March 3, 2015
    Assignee: Herman Miller, Inc.
    Inventors: Jeffrey Bernett, Nicholas Dodziuk, Paul S. Gartland, Scott G. Ball, Jeffrey Allen Book, Eileen M. LaMore, Jeffrey Jay Weirsma, Bruce A. Wilcox
  • Publication number: 20120138744
    Abstract: An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
    Type: Application
    Filed: November 26, 2011
    Publication date: June 7, 2012
    Inventors: James A. Fullerton, Scott E. Coburn, R. Klaus Brauer, Blake Emery, Sebastian Petry, Jeffrey Bernett, Don Chadwick, David Wykes
  • Patent number: 8087613
    Abstract: An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
    Type: Grant
    Filed: December 6, 2010
    Date of Patent: January 3, 2012
    Assignee: The Boeing Company
    Inventors: James A. Fullerton, Scott E. Coburn, R. Klaus Brauer, Blake Emery, Sebastian Petry, Jeffrey Bernett, Don Chadwick, David Wykes
  • Publication number: 20110304251
    Abstract: A furniture component includes a base having a back wall with a first outer vertical face, a first inner vertical face and a first upper edge. A pair of horizontally spaced apart side walls each have a second outer vertical face, a second inner vertical face and a second upper edge. The first and second upper edges are substantially coplanar. An outer top includes a bottom surface spaced above the first and second upper edges and defines a visible gap therebetween. The outer top has a rear edge and a pair of horizontally spaced apart side edges. The rear edge and the first outer vertical face are substantially coplanar, and the side edges and second outer vertical faces are substantially coplanar. A method of assembling and using the furniture component are also provided.
    Type: Application
    Filed: June 9, 2011
    Publication date: December 15, 2011
    Inventors: Jeffrey Bernett, Nicholas Dodziuk, Paul S. Gartland, Scott G. Ball, Jeffrey Allen Book, Eileen M. LaMore, Jeffrey Jay Weirsma, Bruce A. Wilcox
  • Publication number: 20110101165
    Abstract: An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
    Type: Application
    Filed: December 6, 2010
    Publication date: May 5, 2011
    Inventors: James A. Fullerton, Scott E. Coburn, R. Klaus Brauer, Blake Emery, Sebastian Petry, Jeffrey Bernett, Don Chadwick, David Wykes
  • Patent number: 7871039
    Abstract: An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
    Type: Grant
    Filed: August 16, 2007
    Date of Patent: January 18, 2011
    Assignee: The Boeing Company
    Inventors: James A. Fullerton, Scott E. Coburn, R. Klaus-Brauer, Blake Emery, Sebastian Petry, Jeffrey Bernett, Don Chadwick, David Wykes
  • Publication number: 20080290715
    Abstract: An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
    Type: Application
    Filed: August 16, 2007
    Publication date: November 27, 2008
    Inventors: James A. Fullerton, Scott E. Coburn, R. Klaus Brauer, Blake Emery, Sebastian Petry, Jeffrey Bernett, Don Chadwick, David Wykes
  • Patent number: D532984
    Type: Grant
    Filed: February 17, 2006
    Date of Patent: December 5, 2006
    Assignee: Design Within Reach, Inc.
    Inventor: Jeffrey Bernett
  • Patent number: D534734
    Type: Grant
    Filed: May 12, 2006
    Date of Patent: January 9, 2007
    Assignee: Design Within Reach, Inc.
    Inventor: Jeffrey Bernett
  • Patent number: D747892
    Type: Grant
    Filed: September 23, 2014
    Date of Patent: January 26, 2016
    Assignee: TEKNION LIMITED
    Inventors: Jeffrey Bernett, Nicholas Dodziuk