Patents by Inventor Joseph Wilding

Joseph Wilding 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: 10435138
    Abstract: A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed and transported. The folding mechanism includes an extension tube that enables the outboard portion of the wing to be extended away from the inboard section of the wing, rotated about the lateral axis of the aircraft and then pivoted rearward so that the wing is aligned with the longitudinal axis of the aircraft along side the fuselage. The wing-fold mechanism is independent of the structural components of the wing used to convey aerodynamic loads during flight and provides a means for the user to bring the outboard wing section into a near alignment position while the wing-fold mechanism thereafter assists to refine the alignment into its final flight configuration.
    Type: Grant
    Filed: September 6, 2018
    Date of Patent: October 8, 2019
    Assignee: ICON AIRCRAFT, INC.
    Inventors: Matthew Gionta, Jon Karkow, Joseph Wilding, Michael Jagemann
  • Publication number: 20180370612
    Abstract: A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed and transported. The folding mechanism includes an extension tube that enables the outboard portion of the wing to be extended away from the inboard section of the wing, rotated about the lateral axis of the aircraft and then pivoted rearward so that the wing is aligned with the longitudinal axis of the aircraft along side the fuselage. The wing-fold mechanism is independent of the structural components of the wing used to convey aerodynamic loads during flight and provides a means for the user to bring the outboard wing section into a near alignment position while the wing-fold mechanism thereafter assists to refine the alignment into its final flight configuration.
    Type: Application
    Filed: September 6, 2018
    Publication date: December 27, 2018
    Applicant: ICON Aircraft, Inc.
    Inventors: Matthew Gionta, Jon Karkow, Joseph Wilding, Michael Jagemann
  • Patent number: 10099770
    Abstract: A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed and transported. The folding mechanism includes an extension tube that enables the outboard portion of the wing to be extended away from the inboard section of the wing, rotated about the lateral axis of the aircraft and then pivoted rearward so that the wing is aligned with the longitudinal axis of the aircraft along side the fuselage. The wing-fold mechanism is independent of the structural components of the wing used to convey aerodynamic loads during flight and provides a means for the user to bring the outboard wing section into a near alignment position while the wing-fold mechanism thereafter assists to refine the alignment into its final flight configuration.
    Type: Grant
    Filed: July 18, 2014
    Date of Patent: October 16, 2018
    Assignee: ICON Aircraft, Inc.
    Inventors: Matthew Gionta, Jon Karkow, Joseph Wilding, Michael Jagemann
  • Publication number: 20160185444
    Abstract: A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed and transported. The folding mechanism includes an extension tube that enables the outboard portion of the wing to be extended away from the inboard section of the wing, rotated about the lateral axis of the aircraft and then pivoted rearward so that the wing is aligned with the longitudinal axis of the aircraft along side the fuselage. The wing-fold mechanism is independent of the structural components of the wing used to convey aerodynamic loads during flight and provides a means for the user to bring the outboard wing section into a near alignment position while the wing-fold mechanism thereafter assists to refine the alignment into its final flight configuration.
    Type: Application
    Filed: July 18, 2014
    Publication date: June 30, 2016
    Applicant: ICON AIRCRAFT, INC.
    Inventors: Matthew Gionta, Jon Karkow, Joseph Wilding, Michael Jagemann
  • Publication number: 20060169400
    Abstract: The invention relates to systems and methods for manufacturing composite parts for aircraft. In one innovative aspect, a system and method for adjusting a location of a center of gravity of an aircraft relative to a center of lift of a wing of the aircraft is disclosed, wherein a modular spar tunnel mold is provided and configured to be detachably fixed at a plurality of selected locations within a main mold for a fuselage portion of the aircraft. In another innovative aspect, a movable detail or mold is used for manufacturing complex composite parts for an aircraft. In yet another innovative aspect, a movable detail is used to fabricate a common feature for a plurality of different parts for one or more aircraft or a family of aircraft of similar design.
    Type: Application
    Filed: October 14, 2005
    Publication date: August 3, 2006
    Applicant: Adam Aircraft Industries, Inc.
    Inventors: Joseph Wilding, Dennis Olcott