An aircraft fuselage is constructed of a plurality of cylindrical semi-monocoque fuselage sections that are each constructed with mirrored screw threads on either their interior or exterior surfaces. The screw threads of adjacent fuselage sections are secured together end-to-end by a sleeve having complementary screw threads. The sleeve is positioned between adjacent fuselage sections that are held against rotation, but are free to move in translation towards each other. The sleeve is engaged with the screw threads of the adjacent fuselage sections and is rotated, causing the adjacent fuselage sections to move toward each other and into secure engagement in response to the rotating sleeve.
This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.
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