KR20020074889A - Apparatus for loading anti-tank missile - Google Patents

Abstract

PURPOSE: A device for carrying an antitank missile is provided to improve a safety by protecting a missile from an impact by pivotally moving a three-stage horizontal pivot member and a two-stage vertical pivot member. CONSTITUTION: A one-stage load supporting member(3), a two-stage vertical pivoting member(4) and a three-stage horizontal pivoting member(5) are installed at a front of a carrying device(1). A plurality of vertical members(6) is installed at the carrying device(1). Each vertical member(6) is spaced apart in the width direction thereof and in parallel each other. A rear side portion of the carrying device(1) is symmetric with respect to the front side of the carrying device(1). The vertical members(6) forms a corner of the carrying device(1). The vertical members(6) are connected to the rear side portion of the carrying device(1) by means of a cross-embossment member(7). An elliptical installation plate(8) is installed at an upper side of the one-stage load supporting member(3). The two-stage vertical pivoting member(4) is positioned and spaced apart from the one-stage load supporting member(3).

Description

Apparatus for loading anti-tank missile

The present invention relates to an anti-tank missile loading apparatus, and more particularly, to a missile loading apparatus that can securely fix an anti-tank missile carried by a vehicle, and can be quickly mounted and removed.

Antitank missiles, which are essential in modern warfare, are launched from fighters or helicopters, or from targets installed on vehicles. When a missile is launched into a target from a vehicle, the missile-loading vehicle, which is operated to support combat, loads a number of missiles and supplies them as they travel through the battle zone. Missiles loaded on such combat vehicles are always at risk of explosion, so the crew should be careful to handle them, and the missile loading device should be designed to protect the missile. In addition, the loading, removal, mounting and firing of missiles should be as quick and accurate as possible to suit the special circumstances of combat.

1 shows a conventional missile loading device, wherein the missile loading device 1 includes a first stage load supporting member 11, a second stage horizontal pivoting member 12, and a vertical member 13 to be approximately square. It is formed in a box shape, and a plurality of fixing devices 4 are respectively provided on the first stage load supporting member 11 and the second stage horizontal pivot member 12 so that the missile is tightly fixed.

The second stage horizontal pivot member 12 is horizontally pivotable and provided with a rest 15 on its top surface. The fixing device 14 is composed of a stand 15, strips 16 and 16a and a clamp 17, and the stand 15 is approximately elliptical in shape and a missile, not shown, is settled and the strips 16 and 16a. Are respectively fixed to the settable 15. In addition, the strips 16 and 16a are provided with a clamp 17 and a hole, not shown, and the missile is fixed by the hook 17a of the clamp being inserted into the hole and locked.

With the above configuration, when the missile is loaded at the first end of the loading apparatus, the missile is secured while being placed in the rest provided on the first stage load supporting member and wrapped with clamps and strips. In addition, when the missile is loaded in the second stage, after the second stage horizontal pivot member pivots horizontally to face the first stage load bearing member, the missile is loaded by the same procedure as the missile is loaded in the first stage. In the reverse order, the missile is removed.

However, the missile loading device as described above is fixed to each missile with a clamping device consisting of a clamp and a strip, there is a disadvantage that a lot of time is required to lock and release the respective fixing device when the missile is loaded or removed.

Accordingly, an object of the present invention to provide a missile loading device having a structure that is easy to release the fixing device.

1 is a front view of a conventional missile loading device.

Figure 2 is a perspective view showing the configuration of a missile loading apparatus according to the present invention.

Figure 3a is a perspective view showing the operation sequence of the missile loading apparatus according to the present invention.

Figure 3b is a perspective view showing the operation sequence of the missile loading apparatus according to the present invention.

(Explanation of symbols for the main parts of the drawing)

1: loading device 2: missile

3: first stage load supporting member 4: second stage vertical pivot member

5: 3rd stage horizontal turning member 6: vertical member

7: Lateral rigidity member 8: Set rest

9: elastic plate

The object as described above is provided with a bottom support member provided with a substantially semi-circular pedestal for supporting the lower outer surface of the missile, and an elastic plate elastically in close contact with the upper surface of the missile facing the pedestal and being pivoted in the vertical direction. It is achieved by a missile stacking device comprising a vertical swing member spaced apart from the first-stage load supporting member by a distance, and a substantially semi-circular pedestal supporting the upper outer surface of the missile, facing the pedestal of the vertical swing member and composed of a horizontal swing member. Can be.

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.

2 shows one end of the missile loading device 1.

The stacking device 1 is provided in a substantially rectangular box shape, and each corner is composed of a frame member, and is formed to be symmetric in the longitudinal direction and the width direction.

In the front part of the stacking apparatus 1, the 1st stage load supporting member 3, the 2nd stage vertical pivot member 4, and the 3rd stage horizontal pivot member 5 are many vertical members 6 in an up-down direction. ) Are provided at a distance apart from each other in parallel to each other in the width direction of the loading apparatus. In addition, the rear part of the loading device 1, which is not shown, is provided symmetrically with the front part, and the vertical members 6 forming the corners of the loading device 1 have end portions corresponding to the corresponding ends of the rear part and the transverse rigid member 7. ) Is connected.

The upper surface of the first stage load bearing member 3 is provided with a large number of substantially elliptical set rests 8. The second stage up and down pivot member 4 is positioned above the first stage load bearing member 3 by a predetermined distance, and is fixed to the vertical member 6 so that one end thereof can pivot in the up and down direction, and the other end is a vertical member. (6) is locked.

Further, a plurality of elastic plates 9 are provided on the lower surface of the second stage up and down pivot member 4 facing the settling base 8 of the first stage load supporting member 3. The elastic plate 9 is bent in a substantially semicircular shape and both ends thereof are fixed to the vertical swing member 4, and the second vertical swing member 4 is pivoted and fixed to the vertical member 6. Is fixed in close contact with the upper surface of the missile (2).

In addition, the upper surface of the second stage up and down pivot member 4 is secured to the same platform as the platform 8 attached to the first stage load supporting member 3. A fixing device consisting of a settling platform and strips and clamps not shown is provided in the second stage up and down pivot member 4. Strips, not shown, are secured to both ends of the rest, each strip being provided with a clamp and a hole, and the missile is fixed by the clamp's hooks being inserted into the hole and locked.

The upper surface of the third stage horizontal pivot member 5 is provided with a plurality of the same platform as the platform 8 provided on the upper surface of the first load supporting member 3, the missile is placed on the second stage vertical pivot member 4 It is fixed in the same way as it is fixed. In addition, since the missile loading device 1 is symmetrical with each other in the width direction, it is natural to mount more missiles by increasing the width and height by the above configuration.

3A and 3B illustrate the release order of the missile loading apparatus according to the present invention, wherein the third stage pivot member 5 is pivoted in a horizontal direction and the second stage pivot member 4 is pivoted upwards. Remove (2).

According to the present invention by the above configuration, the missile is removed by pivoting the third stage horizontal pivot member 5 in the horizontal direction and the second stage vertical pivot member upward so that the missile can be quickly mounted on the missile launcher. Can be. In addition, since the missile fixed to the first end by the elastic plate is protected from impact, there is an effect of improving safety.

Claims (1)

In a substantially rectangular box-shaped loading device for fixing anti-tank missiles carried by vehicles, A first stage load bearing member provided with several semi-circular restraints; A plurality of vertical members provided at a distance apart from each other in the width direction and having one end fixed to the first end load supporting member; A semi-circular restraint provided on the upper surface of the first end load supporting member, which is spaced apart from the predetermined distance and fixed to the middle of the vertical member in a rotatable manner, and provided with a locking device, elastically absorbs the shock, and A second stage up and down pivot member provided on an under surface of an elastic plate to fix the missile; And a third stage horizontal pivot member provided facing the second stage vertical pivot member at a predetermined distance and provided with a stabilization member and the strip of the second stage vertical pivot member and fixed to pivot horizontally to the vertical member. Missile loading device, characterized in that.