Aeroplane crushing device, and aeroplane demolition method
An aircraft collapsing device that collapses an aircraft fuselage inward includes: a gate-shaped shell which covers a circumference of both sides and an upper portion of a fuselage of an aircraft body from which horizontal wings and a vertical wing have been decoupled, a wedge-shaped pressing member that is mounted to an upper portion of the shell to press at least one portion of a circumference of at least one of annular frames juxtaposed in a longitudinal direction of the fuselage toward a center of the fuselage, a pair of sidewall pressing members that is mounted to both sides of the shell to press the fuselage simultaneously from two directions crossing a pressing direction of the wedge-shaped pressing member at the center of the fuselage after pressing by the wedge-shaped pressing member, and a moving unit that moves the fuselage of the aircraft and the shell relative to one another.
1. An aircraft collapsing device that collapses a fuselage of an aircraft inward, the system comprising:
a gate-shaped shell formed to cover a circumference of both sides and an upper portion of a fuselage of an aircraft body from which horizontal wings and a vertical wing have been decoupled;
a wedge-shaped pressing member that is mounted to an upper portion of the shell to press at least one portion of a circumference of at least one of annular frames juxtaposed in a longitudinal direction of the fuselage toward a center of the fuselage;
a pair of sidewall pressing members that is mounted to both sides of the shell to press the fuselage simultaneously from two directions crossing a pressing direction of the wedge-shaped pressing member at the center of the fuselage after pressing by the wedge-shaped pressing member; and
a moving unit that moves the fuselage of the aircraft and the shell relative to one another.
2. The aircraft collapsing device according to claim 1 , wherein the moving unit moves a circumferential surface of the fuselage from one longitudinal end on a tail side to an other end on a cockpit side.
3. The aircraft collapsing device according to claim 1 , wherein when the wedge-shaped pressing member abuts each of the juxtaposed annular frames of the fuselage, the wedge-shaped pressing member presses each annular frame substantially equally.
4. The aircraft collapsing device according to claim 1 , wherein the wedge-shaped pressing member presses the at least one of annular frames of the fuselage obliquely to a circumferential direction of the at least one of annular frames.
5. The aircraft collapsing device according to claim 1 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
6. The aircraft collapsing device according to claim 2 , wherein when the wedge-shaped pressing member abuts each of the juxtaposed annular frames of the fuselage, the wedge-shaped pressing member substantially presses each annular frame equally.
7. The aircraft collapsing device according to claim 2 , wherein the wedge-shaped pressing member presses the at least one of annular frames of the fuselage obliquely to a circumferential direction of the at least one of annular frames.
8. The aircraft collapsing device according to claim 3 , wherein the wedge-shaped pressing member presses the annular frames of the fuselage obliquely to a circumferential direction of the annular frames.
9. The aircraft collapsing device according to claim 6 , wherein the wedge-shaped pressing member presses the annular frames of the fuselage obliquely to a circumferential direction of the annular frames.
10. The aircraft collapsing device according to claim 2 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
11. The aircraft collapsing device according to claim 3 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
12. The aircraft collapsing device according to claim 4 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
13. The aircraft collapsing device according to claim 6 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
14. The aircraft collapsing device according to claim 7 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
15. The aircraft collapsing device according to claim 8 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.
16. The aircraft collapsing device according to claim 9 , wherein auxiliary pressing members that are capable of preventing a buildup of the fuselage when the wedge-shaped pressing member presses the fuselage are provided to both sides of the wedge-shaped pressing member.