Patents by Inventor Daniel E. McGinty

Daniel E. McGinty 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: 10793251
    Abstract: Hinge pins for foldable aircraft wings are described. An example apparatus includes a hinge pin to rotatably couple a foldable tip of an aircraft wing to a fixed structure of the aircraft wing. The hinge pin includes a first flange, a second flange spaced apart from the first flange along a central axis of the hinge pin, and a through hole oriented along the central axis.
    Type: Grant
    Filed: March 22, 2018
    Date of Patent: October 6, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Eric S. Kamila, Warren H. Steyaert, David D. Boes, Daniel E. McGinty, Ryan A. Fear, Renato Felicio, Eric G. Gruner, Matthew S. Elenbaas, Ian C. Burford, Eric D. Blohm
  • Publication number: 20190291847
    Abstract: Hinge pins for foldable aircraft wings are described. An example apparatus includes a hinge pin to rotatably couple a foldable tip of an aircraft wing to a fixed structure of the aircraft wing. The hinge pin includes a first flange, a second flange spaced apart from the first flange along a central axis of the hinge pin, and a through hole oriented along the central axis.
    Type: Application
    Filed: March 22, 2018
    Publication date: September 26, 2019
    Inventors: Eric S. Kamila, Warren H. Steyaert, David D. Boes, Daniel E. McGinty, Ryan A. Fear, Renato Felicio, Eric G. Gruner, Matthew S. Elenbaas, Ian C. Burford, Eric D. Blohm
  • Patent number: 7387277
    Abstract: Aircraft wing assemblies having both composite and metal panels are disclosed. In one embodiment, a wing assembly includes a support structure, an upper panel assembly formed from a metal material and coupled to the support structure, and a lower panel assembly formed from a composite material and coupled to the support structure. The metal material may be aluminum, titanium, or any other suitable metal, and the composite material may be a carbon fiber reinforced plastic (CFRP) material or other suitable composite material. In another embodiment, the upper panel assembly includes a downwardly depending first web portion, and the lower panel assembly includes an upwardly depending second web portion, the second web portion being proximate the first web portion, and an interface member of an isolating material is disposed between the first and second web portions.
    Type: Grant
    Filed: December 29, 2004
    Date of Patent: June 17, 2008
    Assignee: The Boeing Company
    Inventors: Jan A. Kordel, Richard B. Tanner, Ian C. Burford, Victor A. Munsen, Daniel E. McGinty, Scott N. Rampton, Bruce R. Fox, James M. Kelly, Miles O. Johnson
  • Publication number: 20080023585
    Abstract: Aircraft wing assemblies having both composite and metal panels are disclosed. In one embodiment, a wing assembly includes a support structure, an upper panel assembly formed from a metal material and coupled to the support structure, and a lower panel assembly formed from a composite material and coupled to the support structure. The metal material may be aluminum, titanium, or any other suitable metal, and the composite material may be a carbon fiber reinforced plastic (CFRP) material or other suitable composite material. In another embodiment, the upper panel assembly includes a downwardly depending first web portion, and the lower panel assembly includes an upwardly depending second web portion, the second web portion being proximate the first web portion, and an interface member of an isolating material is disposed between the first and second web portions.
    Type: Application
    Filed: December 29, 2004
    Publication date: January 31, 2008
    Inventors: Jan A. Kordel, Richard B. Tanner, Ian C. Burford, Victor A. Munsen, Daniel E. McGinty, Scott N. Rampton, Bruce R. Fox, James M. Kelly, Miles O. Johnson