Abstract: The present invention is a safety system for use in conjunction with a control bar for a kite wherein the two front lines are secured by a front line swivel positioned between the bar and the kite. One front line terminates at the swivel and one extension of the other front line, the center line, travels through a central aperture in the swivel. The center line is then routed through an aperture on the control bar and terminated with an end that can be secured to the user either manually or by a leash arrangement. The swivel allows any twists that may form in the front lines to unwind. An increased diameter element located proximally of the swivel is configured to engage the center swivel, but is configured to pass through the aperture on the control bar. When the bar is released, sufficient slack is imparted into the remaining flying lines to effectively depower the kite while retaining attachment to the kite through the restrained front line.

Abstract: 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.

Abstract: 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.