A control device for use with an aerodynamic wing including a bar having a safety system that restrains one of the flying lines by routing an attachment through an aperture on the bar. Preferably, the system includes a stopper housing that engages an increased diameter element of the flying line. During normal operation, the increased diameter element is secured by the stopper housing, preventing the flying line from being pulled beyond the stopper housing. When the safety system is deployed, the increased diameter element is pulled from the stopper housing and slack is developed along the remaining flying lines to depower the kite.
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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