An aircraft includes a jet engine with a downward deflectable propelling nozzle; an auxiliary power unit with a downward deflectable propelling nozzle; and a transformable wing. The transformable wing includes a fixed wing, hydraulic sleeve, an air intake duct including an upper wall and a lower wall, a thin wing connected to the hydraulic sleeve, a sliding wing, leading edge flaps, trailing edge flaps, an aileron, and a hinge. The transformable wing is configured, during vertical take-off/landing, to transform such that a leading end to an air intake duct in a vertical direction is formed on the fixed wing, and the air intake duct is formed internally in and along a direction of the wingspan of the fixed wing to cause air taken in by the jet engine to flow, in a common direction, over upper and lower surfaces of the thin wing, thereby generating lift for vertical take-off/landing.
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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