A Survey and Evaluation of Mesh Reduction Techniques
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The invention is a spring return type aircraft ignition switch characterized by retainer plate (10) that includes a tab (12) that extends between a portion of the coil spring (20) and the wall (65) of the rotor body (60) to prevent the windings from the coil (20) from wedging from between the retainer plate (10) and the rotor body (60).
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