| 摘要 |
The purpose of the present invention is to achieve an aeroplane crushing device for swiftly demolishing an aeroplane so as to effectively reclaim resources therein for use. The present invention is provided with: a gate-shaped outer hull part formed so as to cover an upper outer periphery and both sides of an aeroplane-airframe torso part having had horizontal and vertical wings cut and removed therefrom; a wedge-shaped pressing piece which is provided to an upper part of the outer hull part, and which is used to apply a pressing force, towards the centre of the torso part, to at least one place on an outer periphery of at least one of a plurality of annular frame members of the torso part, said annular frame members being arranged in the length direction; a pair of side wall pressing pieces which are provided to both sides of the outer hull part, and which, after the pressing force has been applied by the wedge-shaped pressing piece, simultaneously apply a pressing force to the torso part from two directions which intersect, at a torso-part centre position, the direction in which the pressing force is applied by the wedge-shaped pressing piece; and a movement means which causes relative movement of the airframe torso part and the outer hull part. |
