Patent ID: 9689650
Date: 2017-06-27
CPC Classifications: F42B

Claim:
1. A mechanism for deploying a pair of wings from an airborne body, wherein deployment of the wings in motion, each wing around an axis, defines the wings' deployment plane relative to the airborne body, and wherein the mechanism comprises— an assembly that can be propelled that is mounted in said airborne body and is suited to a rotational motion around an axis that is substantially orthogonal to said wings' deployment plane, and a pair of arms that are linked, each one, on one side of each arm to said assembly that can be propelled and at distance from the rotation axis of said assembly, and on each arm's opposite side to an end of one of said wings and at a distance from said axis around which said rotational motion of the wing in the wings' deployment plane is enabled, and wherein said link of each one of the arms is performed in a manner that enables angular motion of each of the arms relative to the assembly and to said end of the wing unto which each one of the arms is linked, and wherein propelling said assembly to rotational motion and actuating a momentum for turning the wing as a result by said arm that is connected to the wing bring about concurrent rotational motion of the pair of wings in opposing directions and to deployment of the pair of wings on the wings' deployment plane.