An apparatus for deploying a wing of a guided missile comprises a fixed wing fixedly coupled to a body of a guided missile, a rotary wing rotatably coupled to the fixed wing, and a deploying portion for rotating the rotary wing into an unfolded state from a folded state by providing a torsion force to the rotary wing. In the apparatus, a folded degree of the rotary wing can be maximized.

 
Web www.patentalert.com

< Delayed tail fin deployment mechanism and method

> Variable speed transmission for a rotary wing aircraft

> Yaw control device for a nozzle having a rectangular outlet section

~ 00564