KR102222030B1 - Movable inspection apparatus for rocket - Google Patents

Abstract

The present invention relates to a movable guided missile inspection device and a guided missile test method. The movable guided missile inspection device includes: a trailer unit which includes a guided missile inspection space into which a guided missile to be inspected is inserted, and an explosion-proof body which surrounds the guided missile inspection space to prevent damage to the guided missile; a vehicle body capable of transporting and driving the trailer unit; a jig part for fixing a guided missile which is located in the guided missile inspection space and fixed at the position of a target guided missile; and a guided missile inspection unit which inspects whether the guided missile located in the missile inspection space operates normally. Therefore, without transferring the missile to a missile inspection facility, periodic inspections can be performed around the ammunition depot which stores the missile, thereby greatly reducing the consumption of manpower, time, and costs for inspecting the missile, and stresses such as vibration and shock caused by delivery to the missile. In addition, the movable guided missile inspection device can store the guided missiles stably, prevent malfunctions and performance degradation of guided missiles which can occur during a delivery process, and prevent a gap in the combat readiness posture of an operating unit due to the delivery of guided missiles. The safety of the inspection is ensured through securing the safety of the guided missile inspection before firing.

Description

Mobile guided missile inspection device {MOVABLE INSPECTION APPARATUS FOR ROCKET}

The present invention relates to a mobile guided missile inspection apparatus and a guided missile test method, and more particularly, a mobile guided missile inspection apparatus capable of performing a periodic inspection around an ammunition store in storage without transferring a rocket such as a guided missile to a rocket inspection facility, and The invention relates to a method for testing a missile.

In general, rockets including guided missiles are stored in operating units, that is, in the ammunition storage of infantry battalions, artillery battalions, and ammunition battalions.

In addition, rockets such as guided missiles stored in the ammunition are transferred to the rocket inspection facility according to the inspection period to perform inspection, and are transferred to the ammunition of the operating unit again.

The inspection cycle of rockets such as guided missiles stored in the ammunition is generally between 3 and 5 years and varies depending on the type of ammunition.

However, in the conventional guided missile test method, a rocket such as a guided missile must be periodically transferred to an inspection facility to complete the inspection and then transferred to the ammunition storage of the operating unit again.

In addition, the conventional guided missile test method has a problem of applying stress such as vibration and impact to a rocket such as a guided missile being transferred in a process of reciprocating a rocket such as a guided missile to an inspection facility and an ammunition storage.

In addition, the conventional guided missile test method has a problem that a gap occurs in the combat readiness of the operating unit during the inspection by transporting a rocket such as a guided missile stored in the ammunition storage to an inspection facility, and a gap occurs in the combat readiness posture. There is a problem in that it is necessary to prepare separate spare rockets to prevent the problem.

In addition, the conventional guided missile test method has a problem such as performing a rocket inspection such as a guided missile in a state where safety is not guaranteed in special situations such as shooting training.

0001) Korean Patent Registration No. 1837406'Flight environment simulation test device for guided missiles and its simulation test method' (registered on March 6, 2018)

It is an object of the present invention to provide a mobile guided missile inspection apparatus and a guided missile test method capable of performing periodic inspection around an ammunition store in storage without transferring a rocket such as a guided missile to a rocket inspection facility.

In order to achieve the above object of the present invention, an embodiment of the mobile guided missile inspection apparatus according to the present invention includes a guided missile inspection space into which a guided missile to be inspected is inserted, and surrounds the guided missile inspection space to prevent damage to the guided missile. A trailer unit including an explosion-proof body, a vehicle body capable of transporting and running the trailer unit, a jig body for fixing a guided missile that is located in the guided missile inspection space and fixed at the position of the target guided missile, and whether the guided missile located in the guided missile inspection space is operating normally It characterized in that it comprises a guided missile inspection unit to inspect.

In the present invention, the explosion-proof body may include a front explosion-proof wall portion positioned in front of the guided missile inspection space, and the front explosion-proof wall portion may include a replaceable explosion-proof wall member that is stacked in plural and can be replaced.

In the present invention, the replaceable explosion-proof wall member is a general explosion-proof wall member made of fiber-reinforced cement, a compression explosion-proof wall member made of compression-rolled steel stacked with rolled steel and positioned in front of the general explosion-proof wall member, and the compression explosion-proof wall It is located in front of the member and may include a mesh-shaped metal mesh member.

In the present invention, the replaceable explosion-proof wall member is a first compressed explosion-proof wall member made of compression-rolled steel stacked with rolled steel, a first metal mesh member in the form of a mesh located in front of the first compressed explosion-proof wall member, the A second compressed explosion-proof wall member located in front of the first metal mesh member and made of a compression-rolled steel material stacked with rolled steel materials, and a second metal mesh member in the form of a mesh located in front of the second compressed explosion-proof wall member. can do.

In the present invention, a thickness of the first compressed explosion-proof wall member may be greater than a thickness of the second compressed explosion-proof wall member, and a thickness of the first metal mesh member may be greater than a thickness of the second metal mesh member.

In the present invention, the replaceable explosion-proof wall member is a general explosion-proof wall member made of fiber-reinforced cement, located in front of the general explosion-proof wall member, and the first steel plate and the second steel plate having different specific gravity are among the upper side and the lower side. The explosion-proof wall members for the first penetrating bullets and the explosion-proof wall members for the first penetrating bombs stacked alternately in a form inclined to one side, and the third and fourth steel plates having different specific gravity are located on the upper side and It may include a second explosion-proof wall member for the second penetrating bomb alternately stacked in an inclined form to the other side of the lower side.

In the present invention, the replaceable explosion-proof wall member includes a plurality of explosion-proof wall members for the first penetrating bomb, and the plurality of explosion-proof wall members for the second penetrating bullet, and the explosion-proof wall member for the first penetrating bullet and the second penetrating bullet It can be configured by alternately stacking wall members.

In the present invention, the explosion-proof body is positioned by inserting a plurality of the replaceable explosion-proof wall members on the front side, and the explosion-proof wall insertion part that is opened and closed by the wall insertion space opening and closing part is located, and an embodiment of the mobile guided missile inspection apparatus according to the present invention is It may further include a support wall member movably positioned within the explosion-proof wall insertion portion and a support wall moving device for linearly moving the support wall member.

In the present invention, the jig body for fixing the guided missile is a jig housing member into which a guided missile to be inspected is inserted, a jig for fixing a guided missile that is located in the jig housing member and is located in a plurality spaced apart in the length direction of the guided missile to fix the position of the guided missile. May contain wealth.

In the present invention, the guided missile fixing jig portion is hinged to the guided missile support portion and one end side of the guided missile support portion on which the guided missile is seated and rotates around the hinge to cover the upper portion of the guided missile mounted on the guided missile support. It may include a guided missile position fixing unit for fixing the position of the missile.

In the present invention, the guided missile support portion may be positioned on the upper surface of the V-groove in which a portion of the guided missile is inserted and seated.

In the present invention, the guided missile support portion forms a V groove, and a first elastic pad member is positioned on each of the first and second slopes facing each other on which the guided missile to be inspected is seated, and a second elastic pad member is positioned on the inner side of the guided missile position fixing unit. The elastic pad member may be located.

In the present invention, the jig part for fixing the guided missile may further include a locking part for locking or unlocking the position of the guided missile position fixing part on the guided missile support part.

In the present invention, the locking unit may include an electromagnet unit positioned on the guided missile support unit and a magnetic material positioned at the other end of the guided missile position fixing unit and attachable to the electromagnet unit by magnetic force.

In the present invention, the locking unit may further include a contact sensor positioned on the guided missile support unit to detect that the guided missile position fixing unit is seated.

In the present invention, a hinge motor capable of opening and closing the upper portion of the guided missile support portion may be positioned at the hinge portion by rotating the guided missile position fixing portion.

In the present invention, the guided missile support portion is a first support block member on which a first slope forming a V-groove is positioned, a second support block member on which a second inclined surface forming the V-groove is positioned, and the first support block member and the first 2 It may include a block moving device for moving the support block member in a direction in which the gap is narrowed or in a direction in which the gap is increased.

In the present invention, the guided missile position fixing portion may include a curved arc portion at one end side and a seating portion seated on the upper surface of the guided missile support portion at the end side of the arc portion.

In the present invention, the guided missile position fixing unit includes a plurality of rod members rotatably connected to a hinge and a joint motor for rotating any one of two rod members connected to each other by being located on a hinge rotatably connected to the rod member. Can include.

In the present invention, the jig body for fixing the guided missile is located on the inner surface of the jig housing member and may further include a fire extinguishing wall portion formed with a fire extinguishing agent.

In the present invention, the fire extinguishing wall part may include at least one of a front fire extinguishing wall part located on the front side of the missile, a rear fire extinguishing wall part located on the rear side of the missile, and side fire extinguishing wall parts located on both sides of the missile.

In the present invention, the jig body for fixing the guided missile may further include an inclination angle adjustment unit for tilting the guided missile to be inspected.

In the present invention, the inclination angle adjustment unit is a jig base member that has a plurality of jig portions for fixing the guided missiles positioned at the top, and is hinged to the front side of the jig base member and is hinged to the front side of the jig base member. It may include a jig elevating device for raising and lowering the front side of the.

The jig body for fixing the guided missile may further include a block member for modulating an explosion wave, which is located at the front side of the guided missile in the inside of the jig housing member to change a path of fragments in the event of an explosion accident of the guided missile.

In the present invention, the blast wave modulating block member may have a triangular cross-sectional shape in which a first inclined surface for changing a path is located on an upper side and a second inclined surface for changing a path is located on a lower side.

In the present invention, the blast wave modulating block member has a V-groove formed on a surface facing the guided missile, thereby reducing the power of dispersed fragments.

In one embodiment of the guided missile inspection method according to the present invention, the vehicle body inspects the trailer unit including an explosion-proof body in which the guided missile inspection space into which the guided missile to be inspected is inserted is located, and surrounds the guided missile inspection space and prevents damage to the guided missile. A trailer moving step in which the target guided ammunition is moved to the operating unit stored in the ammunition, a guided ammunition insertion step in which the guided ammunition stored in the ammunition station is placed into the guided ammunition inspection space after the trailer moving step, and a regular inspection of the guided ammunition after the guided ammunition insertion step It may include steps.

The present invention has the effect of greatly reducing the consumption of manpower, time, and cost for inspecting the guided missile, since it is possible to perform a periodic inspection around the ammunition in storage without transferring the guided missile to the guided missile inspection facility.

The present invention has the effect of preventing the application of stress such as vibration and impact due to the transfer of the guided missile, stably storing the guided missile, and preventing the occurrence of failure and deterioration of the performance of the guided missile that may occur during the transfer of the guided missile. .

The present invention can prevent a gap in the combat readiness posture of a corresponding operating unit due to the transfer of guided missiles, and has the effect of securing inspection safety by securing safety for inspection of guided missiles before shooting.

1 is a schematic diagram showing an embodiment of a mobile guided missile inspection apparatus according to the present invention.
Figure 2 is a schematic diagram illustrating the outer shape of the jig housing member in the mobile guided missile inspection apparatus according to the present invention.
3 and 4 are views showing an embodiment of the front explosion-proof wall in the mobile guided missile inspection apparatus according to the present invention.
5 is a view showing an embodiment of a jig portion for fixing a guided missile in a mobile guided missile inspection device.
6 is a view showing another embodiment of a jig portion for fixing a guided missile in a mobile guided missile inspection device.
Figure 7 is a schematic diagram showing another embodiment of the mobile guided missile inspection apparatus according to the present invention.
Figure 8 is a schematic diagram showing another embodiment of the mobile guided missile inspection apparatus according to the present invention.
Figure 9 is a process diagram showing an embodiment of the guided missile inspection method according to the present invention.

The present invention will be described in more detail.

The preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. Prior to the detailed description of the present invention, terms or words used in the present specification and claims to be described below should not be construed as being limited to their conventional or dictionary meanings. Accordingly, the embodiments described in the present specification and the configurations shown in the drawings are only the most preferred embodiments of the present invention, and do not represent all the technical spirit of the present invention. It should be understood that there may be equivalents and variations.

1 is a schematic diagram showing an embodiment of a mobile guided missile inspection apparatus according to the present invention, and referring to FIG. 1, an embodiment of a mobile guided missile inspection apparatus according to the present invention is a trailer unit in which a guided missile, which is an inspection target, is located inside ( 100), and a vehicle body 300 capable of transporting and driving the trailer unit 100.

The vehicle body 300 includes a driving unit including an engine that enables a driver to ride and drive the vehicle, and a trailer support unit located at the rear side of the driving unit and positioned at the top of the trailer unit 100.

A plurality of driving wheels of the vehicle body 300 may be located under the driver's seat and a plurality of the trailer support.

The vehicle body 300 may be variously modified and implemented into a known trailer vehicle capable of driving, and a more detailed description thereof will be omitted.

In addition, an explosion-proof body 200 in which a guided missile to be inspected is located is located inside the trailer unit 100.

In the explosion-proof body 200, a guided missile inspection space 200a in which a guided missile to be inspected is inserted and positioned therein is located therein.

The explosion-proof body 200 is formed to surround the guided missile located in the guided missile inspection space 200a so as to prevent damage to the explosion of the guided missile.

The explosion-proof body 200 includes a front explosion-proof wall part 210 located in front of the guided missile testing space 200a, a rear explosion-proof wall part 220 located in the rear of the guided missile testing space 200a, and a lower portion of the guided missile testing space 200a. It is positioned so as to surround the guided missile inspection space 200a in which the guided missile is located, including the lower explosion-proof wall portion 250 and the side explosion-proof wall portions 230 that block both sides of the guided missile inspection space 200a.

As an example, the guided missile includes a general guided missile, an anti-tank guided missile, and an invasive guided missile.

The front explosion-proof wall part 210, the rear explosion-proof wall part 220, the side explosion-proof wall part 230, the upper explosion-proof wall part 240, and the lower explosion-proof wall part 250 each absorb the impact generated when the guided bomb is exploded, and fragments, etc. It is revealed that it can be variously modified and implemented using a known explosion-proof wall that does not scatter to the outside.

It should be noted that the explosion-proof body 200 forms a guided missile inspection space 200a therein, and can be transformed into various shapes that can wrap a guided missile positioned in the guided missile inspection space 200a.

In the guided missile inspection space 200a, a guided missile to be inspected is inserted into the inside, and a jig body 400 for fixing a guided missile for fixing the position of the guided missile is positioned.

The jig body 400 for fixing the guided missile is located in the jig housing member 400a and the jig housing member 400a into which the guided missile to be inspected is inserted, and is spaced apart in the longitudinal direction of the trailer unit 100, that is, in the longitudinal direction of the guided missile. It is located in plurality and includes a jig portion 400b for fixing the guided missile to fix the position of the guided missile.

The jig housing member 400a may be separated by inserting a guided missile into the upper portion of the jig housing member 400a and withdrawing the inserted guided missile.

In addition, it should be noted that the jig housing member 400a is made of an explosion-proof wall made of fiber-reinforced cement as an example, and can be made of an explosion-proof wall of a structure in which rolled steel is laminated.

The guided missile fixing jig portion 400b includes a guided missile support portion 410 on which the guided missile is seated, and a guided missile position fixing portion 420 covering the upper portion of the guided missile mounted on the guided missile support portion 410 to fix the position of the guided missile. do.

The guided missile position fixing part 420 is connected to the guided missile support part 410 in a structure capable of opening and closing the upper side of the guided missile support part 410, and one end side is hinged to the guided missile support part 410, for example. The hinge is rotated around the upper part of the guided missile support part 410 to open the upper part of the guided missile support part 410 so that the guided missile can be raised.

The jig body 400 for fixing guided missiles includes a jig base member 500 in which a plurality of guided missile fixing jig portions 400b are movably positioned, and according to the type of guided missile to be inspected, the jig portion 400b for fixing guided missiles You can change the location.

In addition, an embodiment of the mobile guided missile inspection apparatus according to the present invention may further include a jig moving part (not shown) for moving the jig part 400b for fixing the guided missile along the jig base member 500.

Although the jig moving part is not shown, it is rotatably positioned on the jig part 400b for fixing guided missiles, and has a brake structure that rotates the driving wheel that is rolled by contact with the jig base member 500 by the driving motor, and fixes the position of the driving wheel. As an example, in addition to the ball screw structure linear actuator, hydraulic cylinder, a bar that can be variously modified and implemented using a variety of known linear movement structures such as a rack and pinion structure, a more detailed description will be omitted.

An embodiment of the mobile guided missile inspection apparatus according to the present invention includes a guided missile inspection unit that checks whether or not the guided missile located in the guided missile inspection space 200a operates normally.

Although not shown, the guided missile inspection unit may be variously implemented with known inspection equipment used to inspect the guided missile, and a more detailed description thereof will be omitted.

The trailer unit 100 has a trailer opening and closing unit 110 for opening and closing the guided missile inspection space 200a on the rear side.

The trailer opening/closing unit 110 opens the rear of the guided missile inspection space 200a so that the jig body 400 for fixing the guided missile can be inserted into the guided missile inspection space 200a.

When the trailer opening/closing part 110 is opened, the guided missile fixing jig body 400 is inserted into the guided missile inspection space 200a from the rear side of the trailer part 100 and positioned.

It turns out that the trailer opening and closing part 110 is configured to include a rear explosion-proof wall part 220.

As an example, the trailer opening/closing unit 110 may have a structure that is rotated and opened and closed about a hinge positioned at the lower portion, and may have an electric rotational opening/closing structure by being positioned at the hinge.

It should be noted that the trailer opening/closing unit may be variously modified and implemented using a known electric opening/closing structure, and a more detailed description thereof will be omitted.

The guided missile to be inspected is lifted by a lifting device such as a overhead crane or a crane, and then inserted into the opened jig housing member 400a and placed on a plurality of spaced apart guided missile support portions 410, and the guided missile position fixing portion 420 ) To fix the position of the missile by covering the top of the missile.

In addition, when the rear of the guided missile inspection space 200a is opened by the operation of the trailer opening/closing unit 110 while the guided missile to be inspected is positioned in the jig housing member 400a, the guided missile inspection space 200a is inserted and positioned.

In addition, the jig body 400 for fixing the guided missile is located on the inner surface of the jig housing member 400a and may further include a fire extinguishing wall part 600 formed including a fire extinguishing agent.

The fire extinguishing wall part 600 may include a front fire extinguishing wall part 610 located on the front side of the missile.

As an example, the front fire extinguishing wall part 610 is mounted and fixed on the front side within the jig housing member 400a.

In addition, the fire extinguishing wall part 600 may include a rear fire extinguishing wall part 620 located on the rear side of the guided missile.

As an example, the rear fire extinguishing wall part 620 is mounted and fixed to the rear side within the jig housing member 400a.

In addition, the fire extinguishing wall part 600 may include side fire extinguishing wall parts 630 located on both sides of the guided missile.

As an example, the side fire extinguishing wall portions 630 are provided in a pair and are mounted and fixed on both sides of the jig housing member 400a, respectively.

The fire extinguishing wall part 600 may prevent the flame from being transmitted to the outside when a flame or the like is generated from the guided bomb during the inspection, and extinguish the flame to prevent an explosion accident due to a fire during the inspection.

On the other hand, the front explosion-proof wall part 210 may include a replaceable explosion-proof wall member 211 that can be stacked and replaced in plural.

The replaceable explosion-proof wall member 211 can be used by replacing only the damaged ones by being stacked and positioned in plural, and when the guided bomb is exploded or launched during inspection by stacking different types of explosion-proof walls, You can control the impact.

That is, the explosion-proof body 200 has an explosion-proof wall insertion portion 200b in which a plurality of replaceable explosion-proof wall members 211 are inserted and positioned on the front side, and the trailer portion 100 is an explosion-proof wall insertion portion 200b A wall insertion space opening and closing part (not shown) for opening and closing is positioned.

The wall insertion space opening/closing unit may have a sliding opening/closing structure on the side of the trailer unit 100, may have a rotational opening/closing structure, and may be variously modified and implemented using a known opening/closing structure, and a more detailed description is omitted. Make it clear.

The plurality of replaceable explosion-proof wall members 211 may be replaced with explosion-proof walls suitable for the type of guided missile to be inspected by opening and closing the explosion-proof wall insertion portion 200b as a wall insertion space opening and closing portion.

Figure 2 is a schematic diagram illustrating the outer shape of the jig housing member 400a in the mobile guided missile inspection apparatus according to the present invention, and referring to Figure 2 (a), both sides of the jig housing member 400a may be formed in a curved surface. Also, referring to (b) of FIG. 2, both sides of the jig housing member 400a may be formed in a plane.

When both sides of the jig housing member 400a are curved as shown in FIG. 2(a), there is an advantage in that safety is increased, and both sides of the jig housing member 400a are flat as shown in FIG. 2(b). In the case of forming it, there is an advantage of minimizing manufacturing cost and ease of manufacture.

It should be noted that the shape of the jig housing member 400a may be modified and implemented in various other shapes, and the specific shape is not limited.

3 and 4 are views showing an embodiment of the front explosion-proof wall portion 210 in the mobile guided missile inspection apparatus according to the present invention.

3 shows an example of the front explosion-proof wall portion 210 used for inspection of anti-tank guided missiles, and FIG. 4 shows an example of the front explosion-proof wall portion 210 used in inspection of an invasive guided missile.

Referring to Figures 3 and 4, an embodiment of the movable guided missile inspection device according to the present invention linearly moves the support wall member 700 and the support wall member 700, which are movably positioned within the explosion-proof wall insertion part 200b. It may further include a supporting wall moving device 800 to allow.

The support wall moving device 800 is an example of a hydraulic cylinder having a plurality of piston rods supporting the support wall member 700, and is positioned within the explosion-proof wall insertion part 200b by moving the support wall member 700. The plurality of replaceable explosion-proof wall members 211 are pushed so as to be in close contact with the front side of the explosion-proof wall insertion part 200b.

Since the plurality of replaceable explosion-proof wall members 211 are stacked in a suitable type according to the guided missile to be inspected and inserted into the explosion-proof wall insertion part 200b, the explosion-proof wall insertion part according to the type of the stacked explosion-proof wall, that is, the size. A free space can be formed in (200b).

When a plurality of replaceable explosion-proof wall members 211 forming a free space in the explosion-proof wall insertion part 200b are located in the explosion-proof wall insertion part 200b, the support wall moving device 800 includes the support wall member 700. By pushing and moving forward, the plurality of replaceable explosion-proof members stacked forward in the explosion-proof wall insertion part 200b are positioned in close contact with each other, so that the role of the explosion-proof wall can be effectively performed.

In more detail, Figure 3 (a) is an example of the front explosion-proof wall portion 210 used when inspecting an anti-tank guided missile having one warhead, and referring to Figure 3 (a), a plurality of replaceable explosion-proof wall members ( 211) is located in front of the general explosion-proof wall member 212 made of fiber-reinforced cement, the general explosion-proof wall member 212, and the compression explosion-proof wall member 213 made of compression-rolled steel laminated with rolled steel, compression explosion-proof It is located in front of the wall member 213 and may include a metal mesh member 214 in the form of a mesh.

In addition, (b) of FIG. 3 is an example of the front explosion-proof wall part 210 used when inspecting an anti-tank guided missile having two warheads, and referring to FIG. 3 (b), a plurality of replaceable explosion-proof wall members 211 ) Is a first compressed explosion-proof wall member 213a made of compression-rolled steel stacked with rolled steel, and is located in front of the first compressed explosion-proof wall member 213a, and is a mesh-shaped first metal mesh member 214a, 1 It is located in front of the metal mesh member 214a and is located in front of the second compressed explosion-proof wall member 213b and the second compressed explosion-proof wall member 213b made of compression-rolled steel stacked with rolled steel. It may include a second metal mesh member (214b).

In addition, the thickness of the first compressed explosion-proof wall member 213a is greater than that of the second compressed explosion-proof wall member 213b, and the thickness of the first metal mesh member 214a is greater than the thickness of the second metal mesh member 214b. Take the big one as an example.

Referring to Figure 3, the front explosion-proof wall part 210 is a compression explosion-proof wall member 213 stacked with rolled steel and a mesh-shaped metal mesh member 214 are stacked to allow anti-tank guided bullets containing bullets scattered in the form of fragments to penetrate through. You can effectively block things from becoming.

In more detail, Figure 4 (a) is an example of the front explosion-proof wall part 210 used when inspecting a general penetration-type guided missile, and referring to Figure 4 (a), a plurality of replaceable explosion-proof wall members 211 Is located in front of the general explosion-proof wall member 212 and the general explosion-proof wall member 212 made of fiber-reinforced cement, and the first steel plate 215a and the second steel plate 215b having different specific gravity are on the upper side and the lower side. A third steel having a curved shape inclined and bent to one of the sides and positioned in front of the first explosion-proof wall members 215 for the first penetration bomb and the first explosion-proof wall members 215 stacked alternately with each other, and having a different specific gravity The plate 216a and the fourth steel plate 216b may include a second explosion-proof wall member 216 stacked alternately with each other having a curved shape inclined by bending to the other side of the upper side and the lower side.

The first steel plate 215a, the second steel plate 215b, the third steel plate 216a, and the fourth steel plate 216b each have a curved shape, but the angle gradually increases, that is, the curvature gradually decreases. It has a shape curve.

The first steel plate 215a and the second steel plate 215b are compression-rolled steel materials in which rolled steel materials are stacked, and any one of the first steel plate 215a and the second steel plate 215b is emphasized with different specific gravity. Is formed of a material having a higher specific gravity than the other.

In addition, the third steel plate 216a and the fourth steel plate 216b are compression-rolled steel materials in which rolled steel materials are stacked, and the weights of the third steel plate 216a and the fourth steel plate 216b are different from each other. One is formed of a material having a greater specific gravity than the other.

In addition, (b) of FIG. 4 is an example of the front explosion-proof wall part 210 used when inspecting a penetration-type guided missile for a special purpose, and referring to FIG. 4 (b), a plurality of replaceable explosion-proof wall members 211 ) Includes a plurality of explosion-proof wall members 215 for first penetrating bullets, and a plurality of explosion-proof wall members 216 for second penetrating bullets, and the explosion-proof wall member 215 for the first penetrating bullet and the explosion-proof wall member for second penetrating bullets ( 216) may be stacked alternately.

Referring to Figure 4, the plurality of replaceable explosion-proof wall members 211 have a curved shape in which the first steel plate 215a and the second steel plate 215b having different specific gravity are bent to either side of the upper side and the lower side. The first explosion-proof wall members 215 for penetrating bombs stacked alternately with each other, the third steel plate 216a and the fourth steel plate 216b having different specific gravity are curved to the other side of the upper side and the lower side to form an inclined curve By stacking the second explosion-proof wall members 216 alternately stacked with each other, it is possible to effectively block penetration of the penetrating missile by changing the movement path of the penetrating guided missile launched by a malfunction in an inclined direction.

FIG. 5 is a view showing an embodiment of a jig portion 400b for fixing a guided missile in a mobile guided missile inspection device, and FIG. 6 is a view showing another embodiment of a jig portion 400b for fixing a guided missile in a mobile guided missile inspection device to be.

Referring to FIGS. 5 and 6, the guided missile support part 410 is positioned on the upper surface of the V-groove in which a part of the guided missile is inserted and seated so that guided missiles having various diameters can be stably seated.

In addition, the guided missile support portion 410 may have a V-groove portion, and a first elastic pad member 410a may be positioned on a first slope and a second slope facing each other on which the guided missile to be inspected is seated.

The guided missile position fixing part 420 has a hinge part hinged to the guided missile support part 410 at one end side, and is rotated around the hinge part to cover a part of the guided missile and press the other end side to the guided missile support part 410. It is detachably coupled to fix the position of the guided missile seated on the guided missile support 410.

In addition, the jig part 400b for fixing the guided missile may include a locking part 430 that locks or unlocks the position of the guided missile position fixing part 420 on the guided missile support part 410.

The locking part 430 is an electromagnet part 431 located at the guided missile support part 410, a magnetic body 432 which is located at the other end side of the guided missile position fixing part 420 and can be magnetically attached to the electromagnet part 431 ).

In addition, the locking part 430 may further include a contact sensor 433 that is positioned on the guided missile support part 410 and detects that the guided missile position fixing part 420 is seated.

The contact sensor 433 controls the operation of the electromagnet part 431 by confirming that the guided missile position fixing part 420 is seated on the guided missile support part 410.

The locking part 430 is operated in a state in which the other end side of the guided missile position fixing part 420 is seated on the guided missile support part 410 to fix the position of the seating part 422 by magnetic force. I can.

In addition, a second elastic pad member 420a may be positioned on an inner surface of the guided missile position fixing part 420.

The first elastic pad member 410a and the second elastic pad member 420a absorb a load or impact applied to the missile when the missile is positioned so that the location of the missile can be more stably fixed.

On the other hand, the guided missile support part 410 includes a first support block member 411 on which a first inclined surface forming a V-groove is positioned, a second support block member 412 in which a second inclined surface forming a V-groove is located, and It may include a block moving device 413 for moving the first support block member 411 and the second support block member 412 in a direction in which the gap is narrowed or in a direction in which the gap is increased.

Although the block moving device 413 is not shown, a jig moving screw and a jig moving screw that are screwed in opposite directions through the first support block member 411 and the second support block member 412 are clockwise or counterclockwise. It may include a screw rotation motor that rotates in the direction.

As an example, the moving screw is screwed in the left screw direction through the first support block member 411, and screwed in the right screw direction through the second support block member 412, or to be coupled in the opposite direction. May be.

Since the first support block member 411 and the second support block member 412 are screwed in opposite directions to the jig moving screw, they move in opposite directions according to the rotation direction of the moving screw to narrow the gap or reverberate each other. Can be moved to a wider gap.

Since the distance between the first support block member 411 and the second support block member 412 can be adjusted according to the diameter of the guided missile to be inspected, guided missiles of various diameters can be seated and inspected stably.

Referring to FIG. 5 in more detail, the guided missile position fixing part 420 is seated on the upper surface of the guided missile support part 410 at the end side of the curved arc part 421 at one end side and the arc part 421. It may include a part 422.

An example is that a hinge motor 423 capable of opening and closing the upper portion of the guided missile support portion 410 by rotating the guided missile position fixing portion 420 is positioned at the hinge portion.

The hinge motor 423 rotates the guided missile position fixing part 420 to automatically open and close the upper part of the guided missile support part 410 without an operator, thereby improving safety during operation.

In addition, the electromagnet part 431 magnetically fixes the seating part 422 when closing the upper part of the guided missile support part 410 with the guided missile position fixing part 420, and the guided missile support part with the guided missile position fixing part 420 ( When the upper portion of the 410 is opened, magnetic force is released so that the guided missile position fixing unit 420 can be rotated by the hinge motor 423.

The locking unit 430 can unlock the position of the guided missile position fixing unit 420 using the electromagnet unit 431, so that the operator locks the position of the guided missile position fixing unit 420 in the guided missile inspection space 200a Do not perform the disarming operation, thereby improving safety during regular inspection of guided missiles.

Referring to FIG. 6, the guided missile position fixing unit 420 includes a plurality of rod members 424 rotatably connected to a hinge, and a joint motor 425 respectively positioned on a hinge to which the rod member 424 is rotatably connected. It may include.

The joint motor 425 positioned at the hinge connecting the rod member 424 rotates any one of the two connected rod members 424 so that the plurality of rod members 424 can be folded or unfolded.

The guided missile position fixing part 420 may wrap and fix a portion of the upper side of the guided missile having various diameters, including a plurality of rod members 424 connected by hinges, and the joint motors 425 positioned at each hinge are each The rod member 424 is rotated electrically so that the guided bullet is automatically wrapped and fixed.

A second elastic pad member 420a and a pressure sensor 426 are positioned on the inner side of each rod member 424, respectively.

The guided missile position fixing part 420 rotates the plurality of rod members 424 with the joint motor 425 to wrap the guided missiles placed on the guided missile support part 410 and sense it with a pressure sensor 426 to have a diameter It automatically wraps around other missiles so they can be secured.

In addition, at least one rod member 424 positioned on the other end of the plurality of rod members 424 may be seated on the guided missile support portion 410 and locked by the electromagnet portion 431.

That is, the guided missile position fixing unit 420 is automatically rotated by the operation of the motor 425 for each joint after the missile is mounted on the guided missile support unit 410, and the guided missile support unit ( It is possible to wrap a part of the guided missile placed on 410), and at least one rod member 424 positioned on the other end side is placed on the guided missile support part 410, and then it is automatically operated by the operation of the electromagnet part 431. It can be locked by and minimizes the case where the operator is located within the guided missile inspection space 200a during inspection, thereby improving safety during inspection.

7 is a schematic diagram showing another embodiment of the mobile guided missile inspection apparatus according to the present invention, Figure 8 is a schematic diagram showing another embodiment of the mobile guided missile inspection apparatus according to the present invention.

Referring to FIGS. 7 and 8, the jig body 400 for fixing the guided missile may further include an inclination angle adjustment unit 900 for tilting the guided missile to be inspected.

The inclination angle adjustment unit 900 includes a jig base member 500 in which a plurality of jig parts 400b for fixing guided missiles are positioned at the top and rotatable with a hinge at the rear end side, and the front side of the jig base member 500 It may include a jig elevating device 910 that is hinged to and elevates the front side of the jig base member 500.

The jig elevating device 910 is an example of a hydraulic cylinder, and the end side of the piston rod protruding from the cylinder body is hinged to the jig base member 500 to lift the front side of the jig base member 500. By descending, the jig base member 500 may be tilted.

It should be noted that the jig elevating device 910 can be variously modified and implemented using a known elevating structure such as a linear actuator having a ball screw structure in addition to a hydraulic cylinder.

That is, the jig lifting and descending device 910 generates a protective power gain by tilting the guided missile to be inspected and changing the direction of the warhead. For example, when the guided missile is tilted at 30°, a gain of 15% protection power may occur, and when the guided missile is tilted at 45°, a gain of 30% protection power may occur.

In addition, the jig body 400 for fixing the guided missile may further include a block member 1000 for modulating an explosion wave which is located at the front side of the guided missile and changes the path of fragments in the event of an explosion of the guided missile.

The block member 1000 for modulating the explosion wave can minimize damage caused by fragments by increasing the path of fragments or collecting and concentrating fragments scattered widely during an explosion accident of a guided missile during inspection.

In more detail, referring to FIG. 7, the block member 1000 for modulating the explosion wave has a triangular cross-sectional shape in which a first path change slope is located on an upper side and a second path change slope is located on the lower side. Let's take an example.

The block member 1000 for modulating an explosion wave having a triangular cross-sectional shape may increase a moving path of fragments during an explosion accident of a guided missile including a liner such as an anti-tank guided missile, thereby generating a gain of protection power.

In addition, referring to FIG. 8, the block member 1000 for modulating the explosion wave has a V-groove formed on a surface facing the guided bomb, thereby reducing the power of dispersed fragments, thereby generating a gain of protection power.

A block member 1000 for modulating an explosion wave having a V-groove formed on a surface facing the guided missile may be used to weaken the dispersion of the fragments when inspecting the surface-to-air and air-to-air missiles in which the fragments are dispersed.

On the other hand, Figure 9 is a process diagram showing an embodiment of the guided missile inspection method according to the present invention. 1 and 9, in an embodiment of the guided missile inspection method according to the present invention, a guided missile inspection space 200a into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space 200a. A trailer moving step (S100), a trailer moving step (S100) in which the trailer unit 100 including the explosion-proof body 200 to prevent damage to the vehicle body 300 is moved to the operating unit in which the guided bullets to be inspected are stored in the ammunition storage unit. After), a guided missile insertion step (S200) of placing the guided missile stored in the ammunition storage into the guided missile inspection space (200a), and an inspection step (S300) of performing a periodic inspection of the guided missile after the guided missile insertion step (S200). .

That is, the vehicle body 300 may move the trailer unit 100 including the explosion-proof body 200 to the operating unit of the corresponding guided missile that is stored in the ammunition storage, that is, a number of guided missiles that need to perform periodic inspection.

And, the guided missile insertion step (S200) is a process of inserting the guided missile to be inspected into the jig housing member 400a of the jig body 400 for fixing the guided missile with an open top after being lifted by a lifting equipment such as a overhead crane or a crane. Including the process of fixing the position by seating in the jig part 400b for fixing guided missiles in the housing member 400a, and inserting the jig housing member 400a into the guided missile inspection space 200a of the trailer part 100 .

A trailer opening/closing part is located at the rear of the trailer part 100 to open the trailer opening/closing part and insert the jig housing member 400a from the rear of the trailer part 100 into the guided missile inspection space 200a of the trailer part 100.

The guided missile to be inspected is wrapped with an explosion-proof body 200 in the trailer unit 100 while being located in the jig body 400 for fixing the guided missile made of an explosion-proof wall, that is, the jig housing member 400a, thereby preventing double-safe explosion protection. By having a structure, periodic inspections can be safely carried out.

The inspection step (S300) is known as a predetermined periodic inspection according to the type of the guided missile and may be variously performed, so a more detailed description will be omitted.

In the present invention, it is possible to perform periodic inspection in the vicinity of an ammunition in storage without transferring the guided missile to the guided missile inspection facility, so that the consumption of manpower, time, and cost for inspecting the guided missile can be greatly reduced.

The present invention has the effect of preventing the application of stress such as vibration and impact to the guided missile, stably storing the guided missile, and preventing the occurrence of failure and performance degradation of the guided missile that may occur during the transfer of the guided missile. .

The present invention can prevent a gap in the combat readiness posture of a corresponding operating unit due to the transfer of guided missiles, and has the effect of securing inspection safety by securing safety for inspection of guided missiles before shooting.

It should be noted that the present invention is not limited to the above-described embodiments, but various modifications can be made without departing from the gist of the present invention, and this is included in the configuration of the present invention.

100: trailer unit 110: trailer opening and closing unit
200: explosion-proof body 200a: guided missile inspection space
200b: explosion-proof wall insertion part 210: front explosion-proof wall part
211: replaceable explosion-proof wall member 212: general explosion-proof wall member
213: compression explosion-proof wall member 213a: first compression explosion-proof wall member
213b: second compressed explosion-proof wall member 214: metal mesh member
214a: first metal mesh member 214b: second metal mesh member
215: explosion-proof wall member for the first penetrating bomb 215a: first steel plate
215b: second steel plate 216: explosion-proof wall member for second penetrating bullets
216a: steel plate 3 216b: steel plate 4
220: rear explosion-proof wall part 230: side explosion-proof wall part
240: upper explosion-proof wall part 250: lower explosion-proof wall part
300: vehicle body 400: jig body for fixing guided missiles
400a: jig housing member 400b: jig portion for fixing guided missiles
410: guided missile support portion 410a: first elastic pad member
411: first support block member 412: second support block member
413: block moving device 420: guided missile position fixing unit
420a: second elastic pad member 421: arc portion
422: seat 423: hinge motor
424: rod member 425: joint motor
426: pressure detection sensor 430: locking part
431: electromagnet part 432: magnetic body
433: contact sensor 500: jig base member
600: fire extinguishing wall part 610: front fire extinguishing wall part
620: rear fire extinguishing wall part 630: side fire extinguishing wall part
700: support wall member 800: support wall moving device
900: tilt angle adjustment unit 910: jig elevating device
1000: block member for blast wave modulation

Claims (28)

A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The explosion-proof body includes a front explosion-proof wall portion positioned in front of the guided missile inspection space,
The front explosion-proof wall portion includes a replaceable explosion-proof wall member that is stacked in plurality and can be replaced,
The replaceable explosion-proof wall member,
General explosion-proof wall member made of fiber-reinforced cement;
A compression explosion-proof wall member positioned in front of the general explosion-proof wall member and made of compression-rolled steel in which rolled steel is stacked;
A mobile guided missile inspection device, characterized in that it is located in front of the compression explosion-proof wall member and comprises a mesh-shaped metal mesh member.
delete delete A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The explosion-proof body includes a front explosion-proof wall portion positioned in front of the guided missile inspection space,
The front explosion-proof wall portion includes a replaceable explosion-proof wall member that is stacked in plurality and can be replaced,
The replaceable explosion-proof wall member,
A first compression explosion-proof wall member made of compression-rolled steel in which rolled steel is laminated;
A first metal mesh member located in front of the first compression explosion-proof wall member and having a mesh shape;
A second compression explosion-proof wall member positioned in front of the first metal mesh member and made of compression-rolled steel in which rolled steel is stacked; And
A mobile guided missile inspection device, comprising: a second metal mesh member in the form of a mesh and positioned in front of the second compression explosion-proof wall member.
The method of claim 4,
A mobile guided missile inspection apparatus, wherein the first compressed explosion-proof wall member has a thickness greater than that of the second compressed explosion-proof wall member, and the first metal mesh member has a thickness greater than that of the second metal mesh member.
A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The explosion-proof body includes a front explosion-proof wall portion positioned in front of the guided missile inspection space,
The front explosion-proof wall portion includes a replaceable explosion-proof wall member that is stacked in plurality and can be replaced,
The replaceable explosion-proof wall member,
General explosion-proof wall member made of fiber-reinforced cement;
An explosion-proof wall member for a first penetrating bomb in which a first steel plate and a second steel plate having different specific gravity are alternately stacked with each other in a form inclined toward one of an upper side and a lower side, and positioned in front of the general explosion-proof wall member; And
Explosion-proof for a second penetration bomb in which a third steel plate and a fourth steel plate with different specific gravity are alternately stacked with each other in an inclined form to the other of the upper side and the lower side, located in front of the explosion-proof wall member for the first penetrating bomb Mobile guided missile inspection device comprising a wall member.
The method of claim 6,
The replaceable explosion-proof wall member,
A plurality of explosion-proof wall members for the first penetrating bullets, and a plurality of explosion-proof wall members for the second penetrating bullets, and the first explosion-proof wall members for the first penetrating bullets and the second explosion-proof wall members for the second penetrating bullets are alternately stacked to each other. Mobile guided missile inspection device.
The method according to any one of claims 1, 4, 6,
The explosion-proof body is positioned by inserting a plurality of the replaceable explosion-proof wall members on the front side, and an explosion-proof wall insertion part that is opened and closed by a wall insertion space opening and closing part is located,
A support wall member movably positioned within the explosion-proof wall insertion portion;
Mobile guided missile inspection device, characterized in that it further comprises a support wall moving device for linearly moving the support wall member.
The method according to any one of claims 1, 4, 6,
The jig body for fixing the guided missile,
A jig housing member into which a guided missile to be inspected is inserted; And
A mobile guided missile inspection apparatus comprising a jig portion for fixing a guided missile located in the jig housing member and positioned in a plurality of spaced apart in the length direction of the guided missile to fix the position of the guided missile.
The method of claim 9,
The jig portion for fixing the guided missile,
Guided missile support on which the guided missile is seated; And
One end side is hinged to the guided missile support portion by a hinge portion and rotates around the hinge portion to cover the upper portion of the guided missile mounted on the guided missile support portion, and a guided missile position fixing portion for fixing the position of the guided missile. Mobile guided missile inspection device.
The method of claim 10,
The guided missile support part,
A mobile guided missile inspection device, characterized in that the V-groove portion in which a part of the guided missile is inserted and seated is located on the upper surface.
The method of claim 11,
The guided missile support portion forms a V-groove, and a first elastic pad member is positioned on each of the first and second inclined surfaces facing each other on which the guided missile to be inspected is seated,
A mobile guided missile inspection device, characterized in that a second elastic pad member is positioned on an inner surface of the guided missile position fixing part.
The method of claim 10,
The jig portion for fixing the guided missile,
Mobile guided missile inspection apparatus, characterized in that it further comprises a locking unit for locking or unlocking the position of the guided missile position fixing unit on the guided missile support.
The method of claim 13,
The locking part,
An electromagnet part positioned on the guided missile support part; And
A mobile guided missile inspection apparatus comprising a magnetic body positioned on the other end of the guided missile position fixing unit and magnetically attached to the electromagnet.
A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The jig body for fixing the guided missile,
A jig housing member into which a guided missile to be inspected is inserted; And
It is located in the jig housing member and includes a jig portion for fixing a guided missile that is positioned in a plurality of spaced apart in the length direction of the guided missile to fix the position of the guided missile,
The jig portion for fixing the guided missile,
Guided missile support on which the guided missile is seated;
A guided missile position fixing unit whose one end side is hinged to the guided missile support portion by a hinge portion and rotates around the hinge portion to cover an upper portion of the guided missile mounted on the guided missile support portion to fix the position of the guided missile; And
And a locking part for locking or unlocking the position of the guided missile position fixing part on the guided missile support part,
The locking part,
An electromagnet part positioned on the guided missile support part;
A magnetic body positioned on the other end of the guided missile position fixing unit and magnetically attached to the electromagnet unit; And
A mobile guided missile inspection apparatus comprising a contact sensor positioned on the guided missile support portion and detecting that the guided missile position fixing portion is seated.
A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The jig body for fixing the guided missile,
A jig housing member into which a guided missile to be inspected is inserted; And
It is located in the jig housing member and includes a jig portion for fixing a guided missile that is positioned in a plurality of spaced apart in the length direction of the guided missile to fix the position of the guided missile,
The jig portion for fixing the guided missile,
Guided missile support on which the guided missile is seated; And
One end side is hinged to the guided missile support portion by a hinge portion and rotates around the hinge portion to cover the upper portion of the guided missile mounted on the guided missile support portion, and a guided missile position fixing portion for fixing the position of the guided missile,
A mobile guided missile inspection apparatus, wherein a hinge motor capable of opening and closing an upper portion of the guided missile support portion by rotating the guided missile position fixing portion is positioned at the hinge portion.
The method of claim 11,
The guided missile support part,
A first support block member on which a first inclined surface forming a V-groove is positioned;
A second support block member on which a second inclined surface forming a V-groove is positioned; And
And a block moving device for moving the first supporting block member and the second supporting block member in a direction in which the gap is narrowed or in a direction in which the gap is increased.
The method of claim 10,
The guided missile position fixing part,
An arc part curved in a curve at one end side; And
Mobile guided missile inspection device, characterized in that it comprises a seating portion to be seated on the upper surface of the guided missile support portion at the end side of the arc portion.
The method of claim 10,
The guided missile position fixing part,
A plurality of rod members rotatably connected by hinges; And
A mobile guided missile inspection apparatus comprising a motor for joints that rotates any one of two rod members connected to each other by being positioned on a hinge to which the rod member is rotatably connected.
A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The jig body for fixing the guided missile,
A jig housing member into which a guided missile to be inspected is inserted;
A jig portion for fixing a guided missile, which is located in the jig housing member and is positioned in plurality to be spaced apart in the length direction of the guided missile to fix the position of the guided missile; And
A mobile guided missile inspection device comprising a fire extinguishing wall part positioned on the inner surface of the jig housing member and including a fire extinguishing agent.
The method of claim 20,
The fire extinguishing wall part includes at least one of a front fire extinguishing wall part located at the front side of the guided missile, a rear fire extinguishing wall part located at the rear side of the guided missile, and side fire extinguishing wall parts located at both sides of the guided missile. Device.
The method of claim 9,
The jig body for fixing the guided missile is
Mobile guided missile inspection device, characterized in that it further comprises an inclination angle adjustment unit for positioning the guided missile to be inspected inclined.
The method of claim 22,
The tilt angle adjustment unit,
A jig base member having a plurality of jig portions for fixing the guided missiles positioned at an upper portion thereof and rotatably positioned with a hinge at a rear end thereof; And
And a jig elevating device that is hinged to the front side of the jig base member and elevates the front side of the jig base member.
A trailer unit including an explosion-proof body in which a guided missile inspection space into which a guided missile to be inspected is inserted is positioned, and surrounds the guided missile inspection space and prevents damage to the guided missile;
A vehicle body capable of transporting and driving the trailer unit;
A jig body for fixing a guided missile which is located in the guided missile inspection space and fixed at a position of a target guided missile; And
It includes a guided missile inspection unit for checking whether a guided missile located in the guided missile inspection space is in normal operation,
The jig body for fixing the guided missile,
A jig housing member into which a guided missile to be inspected is inserted; And
It is located in the jig housing member and includes a jig portion for fixing a guided missile that is positioned in a plurality of spaced apart in the length direction of the guided missile to fix the position of the guided missile,
The jig housing member further comprises a block member for modulating an explosion wave, which is located in the front side of the guided missile in the jig housing member and changes a path of fragments in the event of an explosion accident of the guided missile.
The method of claim 24,
The blast wave modulating block member has a triangular cross-sectional shape in which a first path change slope is located on an upper side and a second path change slope is located on a lower side.
The method of claim 24,
The blast wave modulating block member is a mobile guided missile inspection device, characterized in that the V groove is formed on a surface facing the guided missile to reduce the power of the dispersed fragments.
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