A variable lift, variable drag airfoil assembly including a leading edge and a trailing edge connected together in spaced apart relation and an elastic skin connected to and extending between the leading and trailing edges to define an airfoil profile. A resilient spring member positioned within said airfoil profile exerts biased outward pressure against a central portion of the lifting surface of the elastic skin to automatically create a varying thickness of said airfoil profile responsive to increased air speed over the airfoil profile wherein lift and drag of the airfoil assembly are proportionately reduced as airspeed increases. In a preferred embodiment, the airfoil assembly is inverted in the form of a rear spoiler of a land vehicle oriented transversely across a rear portion of the vehicle to produce an increasing downward road gripping force on the rear wheels of the vehicle with increasing vehicle speed while reducing the drag produced by the airfoil assembly.
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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