KR101659985B1 - A head apparatus for removing paint coating and an automatic system for removing paint coating comprising thereof - Google Patents

Abstract

A head device for removing a coating layer according to the present invention and an automation system for removing a coating layer containing the same are disclosed. A head device for removing a coating layer according to the present invention includes an intrinsic type xenon A lamp, at least one dry ice ejection opening for ejecting the dry ice pellet against the target point at which the xenon lamp generates high temperature glare, a flash generated from the xenon lamp, and dry ice pellets ejected from the at least one dry ice ejection opening And a reflective structure for forming an arcuate reflector at a radius a predetermined distance away from said intuitive xenon lamp.

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to a head device for removing a coating layer, and a coating layer removal automation system including the same. 2. Description of the Related Art [

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a head device for removing a coating layer and an automation system for removing a coating layer containing the same.

In general, internal and external coatings are treated with polyurethane to protect the surfaces of aircraft and fighters, and new paint coating operations are performed after periodic removal of existing paint layers for corrosion prevention and crack inspection . For this purpose, coating layers such as airplanes and fighters must be removed at certain points of time. Removal of the coating layer can be classified into a remover, a sanding method, and a PMB (Plastic Media Blasting) method depending entirely on manpower.

The inventor of the present patent application has proposed a technical concept by inventing a system for automating the removal of a paint coating layer based on heat shock in Patent Application No. 2013-0080034 filed prior to the present application in order to automate coating layer removal, The research and development on the technical field has been continued, and automation of the removal of coating layers such as aircraft and fighter aircraft has been completed by specific technical means.

Dry ice blaster cleaning using dry ice in relation to removal of paint layer is carried out by utilizing the physical characteristics of dry ice. In order to accelerate the dry ice pellet with high pressure compressed air and spray it at high speed through a nozzle or the like, Due to the difference in temperature from the periphery, shrinkage occurs and cracks are generated, and dry ice, which has penetrated into the cracks, instantaneously shows an expansion rate of several hundreds times, thereby separating only foreign matter.

However, when spraying only dry ice pellets, it is possible only when the paint layer is thin, and there is a limit to apply to removal of thick paint paint layers such as polyurethane paint paint layers used in aircraft or fighter aircraft.

Regarding the surface cleaning of the substrate to which the present invention belongs and the removal of the coating layer, Japanese Patent Application Laid-Open No. 2012-236459 of the prior patent publication discloses a cleaning pump for feeding cleaning water to the spray nozzle through a pipe and a branch pipe; A piston and an actuator provided inside the cylinder; The piping and the branch pipe are communicated with each other by the pressure of the washing water when the washing water is supplied, and when the washing water is not supplied, the piping and the branch pipe are blocked by the biasing means in the actuator And at the same time, the branch nozzle swings as the injection nozzle moves away from the aircraft. However, in the prior art document 1, since only the cleaning water is supplied by the operation of the injection nozzle, the cylinder structure and the actuator, even though a part of the waste of the aircraft can be removed, it is not suitable for removing paint from an aircraft or a fighter. I have the problem.

Korean Patent Laid-Open Publication No. 2011-0028532 as a prior patent document 2 discloses a cleaning method capable of suppressing pattern collapse when a cleaning liquid is supplied to a substrate for fabricating a semiconductor device having a pattern on its surface and the substrate is cleaned, Liquid erosion, liquid helium, and liquid carbon dioxide as one of liquid cleaning liquids on the surface of the substrate. However, in the prior art document 2, liquid xenon, that is, liquid xenon is utilized for cleaning the surface of the substrate, but this is for maintaining a fine pattern of the substrate by Leidenfrost phenomenon, There is a limit to apply to cleaning of surface of aircraft such as aircraft or fighter.

[1] Japanese Patent Laid-Open Publication No. 2012-236459 [2] Korean Patent Laid-Open Publication No. 2011-0028532

The present invention aims at solving the problem that it is impossible to remove a thick paint paint layer such as a polyurethane paint paint layer by a paint layer cleaning apparatus using dry ice.

In particular, it is an object of the present invention to provide a head device for removing a paint coating layer or a paint layer which can remove waste paint on a base such as an aircraft or a fighter, and a paint layer removal automation system including the same.

As a first aspect according to the present invention, a head device for removing a coating layer is disclosed. The head device (10) for removing the coating layer comprises: an intrinsic type xenon lamp (11) which generates high-temperature flashes at a target point (T); One or more dry ice nozzles (12) for spraying dry ice pellets against the target point (T) at which the xenon lamp generates high temperature flashes; A dust collecting suction part (13) for sucking the scintillation generated from the xenon lamp and the coating layer waste removed by the dry ice pellets jetted from the at least one dry ice jetting port from the target point; And a reflective structure (14) forming an arcuate reflector at a radius a predetermined distance away from said intuitive xenon lamp.

Preferably, the xenon lamp 11 may be one of a short arc Xenon lamp, a long arc Xenon lamp, and a xenon flash lamp. The xenon lamp 11 may form a water-cooled structure on the straight tube side of the xenon lamp in order to cool the heat due to generation of high-temperature flash on the surface. For example, And a water-cooling circulation structure is formed at the outer periphery so that the fluid can flow in one end of the major axis direction and the fluid can be discharged to the other end.

Preferably, the number of the dry ice nozzles 12 may be two to ten.

The head unit 10 for removing the coating layer may further include a sensor unit 15. The sensor unit 15 detects a distance from the xenon lamp and the at least one dry ice nozzle to the target point, A distance sensor for measuring the distance; A temperature sensor for measuring a temperature in the coating layer removing apparatus and outputting an alarm sound when the temperature falls within a predetermined temperature range; And an impact sensor for measuring the amount of impact applied to the target point T by the xenon lamp and the at least one dry ice nozzle.

Preferably, the head device 10 for removing the coating layer can remove the coating layer by moving at a speed of 3 cm to 20 cm per second.

On the other hand, as a second aspect according to the present invention, a paint layer removal automation system including a head device for removing a paint layer is disclosed. The coating layer removal automation system includes a head device (10) for removing a coating layer; An accompanying device 20 for removing the coating layer; And a piping structure (L) for connecting the head device and the accompanying device.

The head device 10 of the paint layer removal automation system may be a head device according to the first aspect of the present invention, and the supporting device 20 for removing the coating layer may include a moving speed of the head device for removing the coating layer, An operating unit (21) for setting a driving temperature of the xenon lamp and an injection amount per hour of the dry ice pellet injected from the at least one dry ice supplying unit; A control unit 22 for controlling the high voltage power supply unit 23, the dry ice pellet manufacturing unit 26, the waste treatment unit 27, and the head device 10 according to the specifications set by the operation unit 21; A high voltage power supply unit 23 for supplying driving power of the xenon lamp; A liquid carbon dioxide storage section (24) for liquefying and storing carbon dioxide; A compression unit (25) for compressing the liquid carbon dioxide; A dry ice pellet producing unit (26) for producing the dry ice pellets jetted from the at least one dry ice jetting port; And a waste treatment unit 27 for treating the paint layer waste transferred from the dust suction unit.

According to the head device for removing the paint layer and the automation system for removing the paint layer according to the present invention, it is possible to automate the paint layer and / or the waste material on the base such as aircraft or fighter by spraying the flash light and the dry ice pellet generated from the xenon lamp. It is possible to realize an automatic cleaning taking into consideration the thickness of the coating layer and the cleaning power through the operation panel.

In addition, since it can easily remove the paint layer and / or waste on the aircraft such as airplane or fighter aircraft, it saves time for maintaining and repairing aircraft or fighter aircraft, and can extend the service life of aircraft or fighter aircraft Will be recognized.

Those skilled in the art will recognize that the effects of the present invention can be widely accepted without being limited to the foregoing description.

1 is a conceptual diagram for explaining a configuration and an example of a head device for removing a coating layer of the present invention and an automation system for removing a coating layer containing the same.
2 shows a two-dimensional embodiment for explaining a process of removing a paint layer in a head device for removing a paint layer according to the present invention.
FIG. 3 is an embodiment showing the two-dimensional view of FIG. 2 in three dimensions.
FIG. 4 shows an embodiment of a supporting device for removing a coating layer connected to a head device for removing a coating layer.
FIG. 5 is a functional block diagram for explaining a paint layer removal automation system according to the present invention from a whole viewpoint.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, preferred embodiments of a head device for removing a coating layer according to the present invention and an automated system for removing a coating layer including the same will be described with reference to the accompanying drawings. The embodiments of the present invention can be modified into various other forms, and the scope of the present invention is not limited to the embodiments described below. Furthermore, embodiments of the present invention are provided to more fully describe the present invention to those skilled in the art.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS In the following description of the preferred embodiments of the present invention, reference will now be made, by way of example only, to the accompanying diagrammatic drawings in which: The configuration related to the present invention will be described in detail.

In the present specification, the term " comprising " means that a corresponding feature, component, or element exists, but does not include only those features, elements, and elements, And / or additional space.

The term "exemplary" is used herein to mean "serving as an example, instance, or illustration," and that the "exemplary" aspects are to be understood as preferred or advantageous over other aspects .

Also, it is to be understood that the present invention covers one or more than one form unless expressly specified to designate the singular form in this specification.

In the drawings attached to the specification, elements having substantially the same features and functions will be denoted by the same reference numerals, and the shapes, sizes, etc. of the elements shown in the drawings may be exaggerated for clarity.

≪ Example of use centered on head device for coating layer removal >

1 is a conceptual diagram for explaining a configuration and an example of a head device for removing a coating layer of the present invention and an automation system for removing a coating layer containing the same. The automation system for removing paint layers according to the present invention comprises a head device 10 for removing a paint layer, a carrying device 20 for removing a coating layer, and a pipe structure L connecting the devices 10 and 20 do.

As shown, since the accompanying device 20 for removing the coating layer has a moving means (for example, a plurality of wheels), the head device for removing the paint on the surface of the aircraft or the fighter 10 moves in accordance with the moving speed set on the system, but moves to a range not covered by the piping structure L, the supporting device 20 for removing the coating layer itself can move.

For example, the head device 10 for removing the coating layer according to the present invention can move at a speed of 1 cm to 30 cm per second from the target point T, preferably 2 cm to 15 cm per second, The moving speed of the coating layer 10 can be set on the operation panel or the like of the supporting device 20 for removing the coating layer. When the head device 10 moves away from the coverable distance by the piping structure L, by moving the supporting device 20 itself for removing the coating layer, the cleaning process by removing paint or waste matter on the gas is continued .

≪ Head device for removing coating layer >

FIG. 2 shows a two-dimensional embodiment for explaining a process of removing a paint layer in a head device for removing a paint layer according to the present invention. FIG. 3 is a cross- Yes.

A head device (10) for removing a coating layer according to the present invention comprises an intrinsic type xenon lamp (11) for generating high temperature flashes at a target point, At least one dry ice supply port (12) for spraying ice pellets, a scintillation light generated from the xenon lamp, and a coating layer waste removed by dry ice pellets jetted from the at least one dry ice supply port, , A reflective structure (14) forming an arcuate reflector at a radius a predetermined distance away from said intuitive xenon lamp.

First, the xenon lamp 11 is usually used for a DC point lamp, and an anode and a cathode are separated at intervals of a few millimeters, and the main luminescent material is injected with water pressure of xenon gas. A driving voltage of a high voltage (several tens kV, for example, 10 kV or more, 20 to 30 kV or more) is required when the internal pressure of the xenon lamp 11 is high (internal air pressure is 1 to 10 atm and 20 to 40 atmospheres during lighting) Because it is in a gas state, unlike other discharge lamps, the time required for lighting and re-lighting is short.

It is known that when the xenon lamp 11 is normally turned on, it reaches 80% of the maximum output in a short time, and it is possible to re-visit from time to time. It is known that the lamp voltage is low but the lamp current is three times higher than that of the mercury lamp . Also, it is known that the temperature of the arc of the xenon lamp 11 is 5000K or more, and the spectrum is continuous over the entire wavelength range.

The Xenon lamp 11 according to the present invention may be one of a short arc Xenon lamp, a long arc Xenon lamp and a Xenon flash lamp, It can be a xenon flash lamp.

Among them, the short arc Xenon lamp is in the form of a point light source and is close to natural light and is known to have excellent color rendering properties. On the other hand, long arc xenon lamps have electrodes formed on both ends of a quartz tube having a major axis direction and are turned on by alternating current. The xenon flash lamp is a quartz tube of an intrinsic type or a U-shape, or an electrode is provided at both ends of a glass tube, and a xenon gas of several tens to several hundred Torr is sealed to discharge the energy accumulated in the capacitor instantaneously, I will.

Due to its physical and optical properties, such a xenon lamp 11 can be used to remove the solidified polyurethane paint coating layer on the surface of aircraft or fighter aircraft, and the flashing period of the xenon lamp 11 and / The thickness of the coating layer and the cleaning power can be taken into account when setting the strength.

Referring to FIG. 2, which is two-dimensionally illustrated in FIG. 2 and three-dimensionally, the Xenon lamp 11 is a rectangle or the like, and when a driving voltage is applied to the Xenon lamp 11, The white light of the blue color is generated and the high temperature flash is generated at the target point T. [

3, the Xenon lamp 11 may be installed in the center of the head unit 10 for removing the coating layer, for example, in the form of a straight tube or the like. The head unit 10 Includes a reflective structure 14 spaced apart from the xenon lamp 11 by a predetermined distance so that the vertical cross section has a semi-elliptical shape. Preferably, the reflective structure 14 may be a reflector structure of metallic material capable of shielding hot flashes, dry ice pellets, or solid particles generated from the xenon lamp 11.

On the other hand, one side of the xenon lamp 11 and the reflective structure 14 has one or more dry ice nozzles 12 for spraying dry ice pellets or solid particles, And a dust inlet 13 having a structure capable of sucking paint layer waste that is removed by pellets or solid particles from the dry ice jetting port 12.

The head device 10 for removing the coating layer is spaced from the surface of the base (e.g., a fighter plane or an aircraft) by a predetermined distance (within several centimeters), but since the flashlight of the xenon lamp 11 is extremely hot, For the sake of safety of the head device for removing the coating layer and the system including the same, the xenon lamp 11 forms a water-cooling structure. For example, as shown in FIG. 3, the Xenon lamp 11 is of an intrinsic type, in which the fluid circulates along the long axis direction of the intaglio type, or the fluid circulation dope is transferred to the outermost surface of the xenon lamp 11 Cooling structure can be provided. That is, the Xenon lamp 11 can have a water-cooling circulation structure by having a structure in which the fluid flows in one end of the long axis direction and the fluid can be discharged to the other end.

One or more dry ice nozzles 12 may be arranged to have more than one (e.g., four) dry ice nozzles, although only two are shown in Figures 2 and 3 for clarity of illustration. The at least one dry ice nozzle 12 may spray the dry ice pellet to the target point at which the xenon lamp 11 generates high temperature glare, or may simultaneously spray the solid ice particles with the dry ice pellet.

Specifically, at least one of the one or more dry ice ejection openings 12 has a rectangular nozzle orifice, and the dry ice pellets and / or particles are ejected by an instantaneous pressure difference. In this case, (Not shown) for spraying the air of the dry ice ejection port (not shown), respectively, rather than immediately exposing the dry ice to a high temperature due to the flash of the xenon lamp 11 at the time of supplying dry ice, 12, the high-pressure air layer functions as a protective layer to delay the exposure time to a high temperature.

The dust suction portion 13 is provided to suck the scintillation generated from the xenon lamp and the coating layer waste which is removed by the dry ice pellets and / or particles sprayed from the at least one dry ice supply portion from the cleaning target point. 3, the dust inlet 13 may have a length equal to the length of the xenon lamp 11 in the form of a straight tube or the like, and even though it is shown as a single in Fig. 3, The coating layer waste can be sucked from the surface of the aircraft or the fighter by strong speed and suction force.

In order to form an arch that is spaced a certain distance from the xenon lamp 11 of the head device 10 for removing the coating layer according to the present invention and does not shield between the xenon lamp 11 and the target point T, A reflective structure 14 may be provided. For example, the reflective structure 14 may be in the form of a reflector that surrounds the xenon lamp 11 by attaching the rectangular piece having the same width and length in continuous close contact.

This reflector, that is, the reflective structure 14, prevents heat due to the flash generated from the xenon lamp 11 from affecting other components of the head device 10 for removing the coating layer, To concentrate on the removal of paint or waste coating layers on the surface of the substrate. In addition, the reflective structure 14 may also include other configurations of the head device 10 for removal of the coating layer when the dry ice pellets and / or particles are ejected from the dry ice nozzle 12 to the target point T. [ It is possible to prevent a pure impact amount from being applied.

As described above, when power is applied to the xenon lamp 11, flash light of a high temperature instantaneously several hundreds or thousands of degrees Celsius is repeatedly generated at a cycle of a short time (for example, several msec to several seconds) By spraying the dry ice pellets or particles in the ice nozzle 12, the coating layer on the surface of the aircraft or fighter plane is removed.

Since the moving speed of the head device can be controlled on the head device for removing the coating layer in this manner and the system including the same, it is possible to automate the removal of the coating layer, and the gas layer on the base such as an aircraft or a fighter, Because it is easy to remove wastes, it can save time for maintenance and repair of aircraft or fighter aircraft, and extend the life span of aircraft or fighter aircraft.

≪ Attachment device for removing coating layer >

FIG. 4 shows an embodiment of a supporting device for removing a coating layer connected to a head device for removing a coating layer.

As described in connection with FIG. 1, the accompanying device 20 for removing coating layers comprises a moving means (e. G., A plurality of wheels), thus removing paint on the surface of the aircraft or fighter When the head device 10 moves in accordance with the moving speed set on the system but moves to a range that can not be covered by the piping structure L, the supporting device 20 for removing the coating layer itself can move.

On the other hand, a portion not shown on the right side of the supporting device 20 for removing the coating layer represents the piping structure L and can be connected to the head device 10 for removing the coating layer.

The accompanying device 20 for removing the paint layer includes a high voltage power supply 23, a compressor 24, a liquid carbon dioxide storage 25, a dry ice pellet production 26 and a waste treatment unit 27 The operator of the coating layer removal automation system may also include a head unit 10 for removing the coating layer and an operation unit (not shown in FIG. 4) for adjusting the specification of the operation of the handling unit 20, May be implemented integrally with reference numerals 23 to 26, or may be implemented in the form of a separate display panel or key panel.

The high voltage power supply unit 23 for supplying the driving power of the xenon lamp 11 is provided with a power supply for activating the water cooling structure of the xenon lamp 11 and a head device 10 for removing the coating layer, The high voltage power supply unit 23 preferably supplies the driving power for periodically generating the high temperature flash of the xenon lamp 11. Also, a power source for operating the water-cooling structure of the xenon lamp 11 and / or a power source for driving the head unit 10 itself may be provided from a general power supply unit (not shown).

The compression section 24, the liquid carbon dioxide storage section 25 and the dry ice pellet manufacturing section 26 are for producing dry ice pellets or particles which are injected from the at least one dry ice ejection opening 12 to a target point. Specifically, the liquid carbon dioxide storage unit 25 stores LCO ₂ (Liquid Carbon Dioxide) at a suitable pressure and temperature for liquefying and storing carbon dioxide.

The compression section 24 adjusts the pressure to liquefy the carbon dioxide and store it in the liquid carbon dioxide storage section 25 and / or to compress the stored liquid carbon dioxide, and the dry ice pellet production section 26 comprises one or more dry ice supply sections The liquid dry ice is solidified with dry ice pellets and / or fine particles sprayed from the dry ice pellets and / or fine particles.

The waste treatment unit 27 receives the coating layer waste on the surface of the fighter jet or the surface of the air taken from the dust suction inlet 13, condenses or condenses it, and discharges the coating layer to the outside from the supporting device for removal of the coating layer.

The high-voltage power supply unit 23, the compression unit 24, the liquid carbon dioxide storage unit 25, the dry ice pellet production unit 26, and the waste treatment unit 27 described above are mainly described for their main functions and purposes And is not limited by the means for implementing the additional functions or the main functions as long as the functions and purposes described are being performed.

<Functional Configuration of Automated System for Removing Coating Layer>

FIG. 5 is a functional block diagram for explaining the automation system for removing paint layers according to the present invention from a whole viewpoint. The automation system for removing paint layers comprises a head device 10 and a heading device 20.

The head device 10 for removing the coating layer and the supporting device 20 for removing the coating layer are connected by a piping structure L and the piping structure L is an arm structure having one or more connecting members And may be a structure that can be operated with a constant radius of rotation around the connecting member.

First, the head device 10 for removing the coating layer includes an intrinsic type xenon lamp 11 for generating a high temperature flash (several hundreds of degrees Celsius to several thousands of degrees Celsius) with respect to a target point T, , One or more dry ice nozzles (12) for spraying dry ice pellets with respect to a target point (T) for making a coating layer (12), a scintillation light generated from a xenon lamp, and a coating layer A dust collecting suction portion 13 for sucking waste from the target point, a reflecting structure 14 for forming an arcuate reflecting glaze at a predetermined distance from the intangible xenon lamp, a head device 10 for removing the coating layer And a sensor unit 15 for optimized operation in which a xenon lamp 11, one or more dry ice nozzles 12, a dust collection unit 13, a reflective structure 14, Tufted locations and can be applied the same or similar.

The sensor unit 15 includes a distance sensor for measuring the distance from the xenon lamp and the at least one dry ice nozzle to the target point; A temperature sensor for measuring a temperature in the coating layer removing apparatus and outputting an alarm sound when the temperature falls within a predetermined temperature range; And an impact sensor for measuring the amount of impact applied to the target point T by the xenon lamp and the at least one dry ice nozzle.

4, includes a high-voltage power supply unit 23, a compressor 24, a liquid carbon dioxide storage unit 25, a dry ice pellet manufacturing unit (not shown) 26 and a waste treatment section 27. The operation section 21 for operating these components and the control measurement value inputted or adjusted by the operation section 21 are transmitted to the high voltage power supply section 23 to the waste treatment section 27) is operated in accordance with the adjusted control measurement value. The detailed description of the high-voltage power supply 23, the compression section 24, the liquid carbon dioxide storage section 25, the dry ice pellet manufacturing section 26, and the waste disposal section 27 corresponds to the matters described with reference to FIG. 4, Is omitted.

The operation unit 21 can be operated by a touch screen / display panel according to a signal input by a mechanical operation and / or an electronic display technique such as a keypad, a wheel, etc., so that an operator can perform high pressure power supply, compression function, liquid carbon dioxide storage amount, dry ice pellet manufacture, It is possible to selectively operate and operate the specifications required for waste treatment and the like.

The control unit 22 includes a high voltage power supply unit 23, a compression unit 24, a liquid carbon dioxide storage unit 25, a dry ice pellet manufacturing unit 26 ), The input specification of the operation unit 21 for operating in the waste treatment unit 27, and the operation to be basically processed in the supporting device 20 for removal of the coating layer.

The operation unit 21 and the control unit 22 may be implemented according to a PLC (Power Line Communication) control method, as an example, not by way of limitation. In the case of the PLC control method, not only the adjustment of the functional constitution diagram included in the supporting device 20 for removing the coating layer but also the adjustment of the function of the coating layer is performed in cooperation with the sensor part 15 of the head device 10 for removing the coating layer, The moving distance of the head device 10 for removal, the xenon lamp 11, the dry ice nozzle 12, the dust suction unit 13, and the like.

According to the paint layer removal automation system according to an embodiment of the present invention, the paint layer and / or the waste material on the base such as an airplane or a fighter plane can be automatized by spraying the flash light and the dry ice pellet generated from the xenon lamp, In addition, it can easily remove the paint layers and / or waste on the aircraft such as airplanes and fighters, thus reducing the time required for maintenance and repair of airplanes and fighters, and the use of airplanes and fighters It is possible to extend the age.

It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are not intended to limit the invention to the particular forms disclosed. It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.

10: Head device for coating layer removal
11: Xenon lamp 12: Dry ice nozzle
13: dust collecting suction part 14: reflective structure
15:
20: Attachment for removal of coating layer
21: operation unit 22:
23: high voltage power supply unit 24:
25: liquid carbon dioxide storage part 26: dry ice pellet manufacturing part
27: waste treatment section
T: Target point
L: piping structure

Claims (8)

1. A coating layer removal automation system comprising a head device for removing a coating layer, a supporting device having a moving means, and a piping structure for connecting the head device and the supporting device,
The head device includes:
An intrinsic type xenon lamp which generates high-temperature flashes at a target point and forms a transparent structure on the outer surface of the water-cooled circulating film structure so that the fluid can flow in one end of the long axis direction and the fluid can be discharged to the other end;
One or more dry ice nozzles for spraying dry ice pellets against the target point at which the xenon lamp generates high temperature glare; And
And a multi-suction structure dust suction unit for sucking the scintillation generated from the xenon lamp and the coating layer waste removed by the dry ice pellets jetted from the at least one dry ice jet opening from the target point,
The above-
A high-voltage power supply for supplying a driving power of the xenon lamp, a water-cooling circulating epilation structure, and a power supply for operating the head unit;
A liquid carbon dioxide storage unit for liquefying and storing carbon dioxide;
A compression unit for compressing the liquid carbon dioxide;
A dry ice pellet producing unit for producing the dry ice pellets for solidifying the carbon dioxide stored in the liquid carbon dioxide storage unit to spray the at least one dry ice pellet;
A waste treatment unit for treating the coating layer waste transferred from the dust suction unit; And
An operating panel for setting the moving speed of the head device for removing the coating layer, the driving temperature of the xenon lamp, the injection amount of the dry ice pellet injected from the one or more dry ice nozzles per hour and the storage amount of the liquid carbon dioxide,
/ RTI &gt;
Automated paint removal system.
The method according to claim 1,
Wherein the Xenon lamp is one of a Short Arc Xenon Lamp, a Long Arc Xenon Lamp, and a Xenon Flash Lamp.
Automated paint removal system.
delete 3. The method of claim 2,
Further comprising a reflective structure for forming an arcuate reflector at a radius a predetermined distance away from said intuitive xenon lamp,
Automated paint removal system.
5. The method of claim 4,
A distance sensor for measuring the distance from the xenon lamp and the at least one dry ice nozzle to the target point; And
A temperature sensor for measuring the temperature in the paint layer removing apparatus and outputting an alarm sound when the temperature is outside the predetermined temperature range
Further included,
Automated paint removal system.
6. The method of claim 5,
Wherein the head device for removing the coating layer moves at a speed of 2 cm to 15 cm per second.
Automated paint removal system.
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