KR20160125749A - Apparatus for attaching and detaching of aircraft mission payload - Google Patents

Abstract

The present invention provides an apparatus for attaching and detaching aircraft mission payload, which comprises: a base member; a lifting and lowering unit connected to the base member to move up and down; and a stacking unit arranged on an upper part of the lifting and lowering unit and formed to put an object on, wherein the stacking unit includes: a left and right moving member arranged on the upper part of the lifting and lowering unit; a left and right moving drive unit connected to the left and right moving member to move the left and right moving member to the left and right; a back and forth moving member arranged on an upper part of the left and right moving member; a back and forth moving drive unit connected to the back and forth moving member to move the back and forth moving member back and forth; a rotating member coupled to the back and forth moving member to be able to rotate the object; and a rotational stacking support arranged on an upper part of the rotating member and formed to enable the object to be seated on one surface. The present invention enhances workability, reduces work time and also prevents a damage to or a breakdown of the aircraft mission payload when the aircraft mission payload is mounted and separated.

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to an apparatus for attaching and detaching an aircraft,

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an apparatus for attaching and detaching an aircraft apparatus having a rotating function.

In general, an aircraft such as a fighter aircraft is required to be detached and attached to a main device such as an engine for maintenance, and an attaching / detaching operation equipment for an aircraft performing a given mission while flying, such as an RF tub, a camera and an electromagnetic wave transmitting / do.

The above-described detachment / attaching work is mainly performed at the bottom of an aircraft. It is generally mounted on a moving truck and moved to a mounting position and then mounted or separated manually by lifting up a single or a plurality of loads according to size, weight,

 When the load is manually mounted and dismounted, it is difficult to work and requires a lot of work. In addition, in the process of mounting and separating the heavy duty load equipment, there is a high possibility that the load is damaged or damaged by the fall, There were disadvantages.

Accordingly, in recent years, various devices have been developed for the maintenance of aircraft and the mounting and dismounting of mission equipment for aircraft.

An example of an aircraft engine mounting apparatus disclosed in Korean Patent Publication No. 10-1022460 (Mar. 15, 2011)

1, the aircraft engine mounting apparatus includes a base frame 100 for positioning an aircraft engine 140 on an upper side thereof, And a first side support pedestal 200 and a second side support pedestal 210 axially coupled to the base frame 100 by a shaft pin 230. Each of the side support pedestals 200 and 210 is configured to support both side surfaces of the aircraft engine 140 that are seated on the base frame 100.

The lower frame 110 is mounted on the base frame 100 at the bottom of the base frame 100 and connected to the lower front of the engine 140, (300, 310).

The lower coupling portions 300 and 310 are provided separately from the first lower coupling portion 300 and the second lower coupling portion 310, respectively. And a control bolt 301 passing through the base frame 100 and meshed with the penetrating base frame 100. A handle for rotating the adjustment bolt 301 is provided at the lower end of the adjustment bolt 301 303 are mounted.

In the conventional aircraft engine mounting apparatus described above, the engine is transferred and mounted in a separate device, so that it is possible to transfer and mount the engine in one apparatus, thereby reducing the troublesomeness in the operation of transferring and mounting the engine, The first side support pedestal 200 supporting the aircraft engine and the second side support pedestal 210 supporting the load are rotated only in the left and right directions, have.

First, in the above-described conventional aircraft engine mounting apparatus, the front portion of the aircraft engine, which is a load, can be moved up and down to some extent by the up and down movement of the lower coupling portions 300 and 310. However, , It can not be used for assembly and disassembly of various types of aircraft mission equipment.

In addition, since the conventional aircraft engine mounting apparatus can not move the load in the left-right direction and the back-and-forth direction, the mounting position and the separation position of the mission equipment for the aircraft can not be precisely adjusted and the mounting and dismounting operation is difficult. There is a drawback that the efficiency is lowered.

Particularly, in the conventional aircraft engine mounting apparatus, not only the structure in which the loading part where the load is mounted is not rotated but also the tilting operation can not be performed and the mounting and dismounting positions can not be set accurately, There is a disadvantage that the damage or durability of the mission equipment is deteriorated.

SUMMARY OF THE INVENTION The present invention provides an apparatus for attaching and detaching an aircraft equipment which is capable of moving forward and backward, left and right, and up and down, and rotating and tilting operations of a loading unit on which aircraft equipment is loaded.

According to another aspect of the present invention, there is provided an apparatus for attaching and detaching airplane equipment comprising a base member, an elevating means connected to the base member to be moved up and down, And the stacking portion includes a left and right moving member disposed at an upper portion of the elevating means and a left and right moving member connected to the left and right moving members to move the left and right moving members to the left and right A forward / backward movement driving unit connected to the forward / backward movement member to move the forward / rearward movement member back and forth; and a control unit for controlling the backward / A rotary member rotatably coupled to the back and forth movable member, And a loading table on which the load is seated on one surface.

According to one example related to the present invention, the rotary table includes a rotary table coupled to the rotary member and configured to have a plate shape for receiving the load, and a rotary table detachably coupled to the rotary table, And a stacking auxiliary member arranged to be spaced apart from each other so as to surround the load so as to prevent the load from being separated from the redistribution plate.

According to another aspect of the present invention, there is provided a portable terminal comprising: a first sliding member disposed on an upper portion of the base member and extending in one direction, the first sliding member having a first moving hole formed to penetrate along a direction of extension; And a second moving hole formed in the upper portion of the first sliding member so as to extend in one direction and penetrate in a direction extending from the first moving member, A sliding member and first and second link members interdigitated with each other, wherein a lower end of the first link member is coupled to the first moving shaft and an upper end of the second link member is coupled to the second moving shaft And a second driving shaft for moving the first moving shaft back and forth by rotation in order to provide a driving force for moving the first moving shaft in forward and backward directions. The routed may include a lifting screw jack.

The left and right moving member includes a left and right moving plate that is laterally moved, a first guide rail that is laterally disposed on the second sliding member, and a first guide that is coupled to the left and right moving plates to be connected to the first guide rail. Wherein the back and forth moving member includes a front and rear moving plate which is moved forward and backward, a second guide rail which is arranged forward and backward on the left and right moving plates, and a second guide rail which is connected to the front and rear moving plates 2 guide block.

The left and right movement driving unit may include a left and right moving screw jack to which a moving nut is coupled to the left and right moving plates and the back and forth movement driving unit may include a back and forth moving screw jack in which a moving nut is coupled to the front and rear moving plates.

According to another embodiment of the present invention, in order to prevent the left and right movable member, the back and forth movable member, and the rotation mount from being moved or rotated, the movement of the left and right movable member, And stopping means for stopping the stopping means.

The apparatus for attaching and detaching any one of the above-described aircraft devices includes a plurality of rolling means respectively installed at the ends of the base member, and a rolling means driving unit connected to the rolling means to adjust the height of the rolling means .

The rolling means includes a wheel portion and a wheel frame for supporting the wheel portion. The rolling means driving portion may include a screw jack for a rolling means, the screw shaft being coupled to the wheel frame to adjust the height of the rolling means .

According to the apparatus for attaching and detaching the aircraft equipment of the present invention, the aircraft equipment mounted on the loading unit can be moved by the rolling means, the aircraft equipment can be elevated and lowered by the elevating means in the vertical direction, It is possible to move the left and right shifting members in the left and right directions and to move the forward and backward shifting members in the forward and backward directions by the forward and backward movement drive unit. This improves the workability in mounting and separating the aircraft equipment, It is possible to prevent damage or breakage of the battery.

In addition, according to the apparatus for attaching and detaching an aircraft equipment of the present invention, the rotating mount table on which the aircraft equipment is mounted is rotated, so that the aircraft equipment can be rotated at an angle desired by the user, It is possible to adjust the elevation of the rolling means by rotating it in the opposite direction so that the aircraft equipment can be tilted so that the desired operation can be performed more conveniently and quickly by rotating and tilting the aircraft at appropriate angles during maintenance, , It is possible to accurately set the mounting and dismounting positions, thereby improving the precision in mounting and dismounting aircraft equipment.

1 is a perspective view showing a conventional aircraft engine mounting apparatus.
2 is a perspective view of an apparatus for attaching and detaching airplane equipment according to one embodiment of the present invention.
FIGS. 3A and 3B are a front view and a side view showing an apparatus for attaching and detaching the aircraft equipment shown in FIG. 2;
4A and 4B are perspective views showing a state in which a load is mounted on the apparatus for attaching and detaching the aircraft equipment shown in FIG.
Fig. 4C is a perspective view of the lifting screw jack shown in Fig. 2; Fig.
5A to 5C are a perspective view, a front view, and a rear view, respectively, of the loading section shown in Fig.
FIG. 5D is a perspective view showing a screw jack for a rolling means used as the rolling means driving portion shown in FIG. 2; FIG.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, an apparatus for attaching and detaching an aircraft equipment according to the present invention will be described in detail with reference to the accompanying drawings. In the present specification, the same or similar reference numerals are given to different embodiments in the same or similar configurations. As used herein, the singular forms "a", "an" and "the" include plural referents unless the context clearly dictates otherwise.

FIG. 2 is a perspective view showing an apparatus for attaching and detaching an aircraft equipment according to an embodiment of the present invention, FIGS. 3a and 3b are a front view and a side view showing an apparatus for attaching and detaching the aircraft equipment shown in FIG. 2, 4A and 4B are perspective views showing a state in which the load is mounted on the apparatus for attaching and detaching the aircraft equipment shown in FIG.

2 to 4B, an apparatus for attaching and detaching an aircraft according to an embodiment of the present invention can move the loading unit 3 up and down, back and forth, left and right, The lifting unit 2, the loading unit 3, the rolling means 5, the rolling means driving unit 6, and the moving handle 5 in order to improve workability and accuracy in mounting and dismounting, (7).

The base member 1 is formed in a substantially rectangular shape by a plate-shaped member, and the front and rear portions where the rolling means 5 is disposed are formed to protrude upward.

The elevating means 2 is a component for elevating and lowering the loading section 3 provided on the base member 1. The elevating means 2 may be a hydraulic driving system provided with a hydraulic cylinder if the loading section 3 can be raised or lowered, In this embodiment, the first sliding member 21, the first moving shaft 22, the second sliding member 23, the second moving shaft 24, the first moving member 22, A pair of driving arms 25, and a screw jack 26 for ascending and descending.

The first sliding member 21 is formed by bending a rectangular plate-shaped body and passing through the first moving hole 211 in the form of a long hole on both sides, and is provided on the base member 1 along the longitudinal direction.

The second sliding member 23 is a member arranged to face up and down the first sliding member 21 and has a structure in which a second moving hole 231 having a long hole shape penetrates through a rectangular plate-shaped body.

The first and second sliding members 21 and 23 may be formed by welding the " a " shaped steel to the base member 1 on both sides of the first and second sliding members 21 and 23. In this embodiment, however, And a moving hole is formed in the projecting portion.

The first moving shaft 22 is formed as a rod-like member inserted between the first moving holes 211 of both first sliding members 21 and horizontally, and the second moving shaft 24 is formed as a second sliding And is formed as a rod-like member by a member inserted between the second moving holes 231 of the member (23).

The first arm 251 and the second arm 252, which are formed in a substantially planar shape, are arranged in parallel to one side and the other side of the base member 1, The lower end of the first link member 251 is connected to the first moving shaft 22 and the upper end of the second link member 252 is connected to the second moving shaft 24 Respectively. The upper end of the first link member 251 is connected to the second pivot shaft 28 provided on the second sliding member 23 and the lower end of the second link member 252 is connected to the first pivot shaft 27 And is provided on the first sliding member 21.

The driving arm 25 is connected to the first moving shaft 22 which is moved by the moving nut 264 which is moved back and forth when the screw shaft 263 of the elevating screw jack 26 is rotated, Since the link member 251 is moved back and forth, the stacking unit 3 is lifted and lowered while being folded.

The lifting screw jack 26 is provided to apply a driving force so that the first moving shaft 22 is moved back and forth, and is generally composed of a mechanical element called a screw jack.

4C is a perspective view showing the lifting screw jack 26 shown in FIG.

4C, the lifting screw jack 26 includes a worm gear 262 installed inside the jack housing 261 and connected to the manual handle 265 for rotation, And a moving nut 264 screwed to the screw shaft 263 and moving forward and backward. The moving nut 264 is coupled to the first moving shaft 22 connected to the lower end of the first link member 251. The moving nut 264 rotates in the forward and reverse directions of the manual handle 265, When the screw shaft 263 is rotated by the screw 262, the moving nut 264 is moved in the forward and backward directions. Therefore, the driving arm 25 is folded back and forth by the back and forth movement of the first moving shaft 22, Is performed.

5A to 5C are a perspective view, a front view, and a rear view, respectively, of the loading section shown in Fig.

5A to 5C, the loading section 3 is disposed at an upper portion of the elevating means 2 and includes a left and right moving member 31, a left and right movement driving section 32, a back and forth moving member 33, A driving unit 34, a rotating member 35, and a rotating table 36.

The left and right movable member 31 is a component provided on the upper part of the elevating means 2 and is disposed above and above the loading base plate 313 coupled to the upper surface of the second sliding member 23, Left moving plate 311 and left and right moving guide means 312 arranged for smooth lateral movement of the left and right moving plates 311. [

5A and 5B, the left and right movement guiding means 312 includes a pair of first guide rails 312a disposed on the left and right of the loading base plate 313, The first guide rail 312a and the first guide block 312b are connected to the LM guide and the first guide block 312a is coupled to the bottom surface of the left and right moving plate 311 so as to be connected to the first guide rail 312a. And the detailed description of the structure will be omitted.

The left and right movement driving unit 32 is constituted by a left and right screw jack 32a configured to move the left and right movable members 31 to the left and right and to which a moving nut is coupled to the left and right moving plate 311.

The left and right screw jack 32a is a mechanical component commonly referred to as a screw jack and can be applied to the above-described lifting screw jack. However, in this embodiment, the screw shaft 32a is connected to the manual handle 321, (322), and a moving nut (323) screwed to the screw shaft and moving back and forth. Since the moving nut 323 is coupled to the bottom surface of the left and right moving plate 311 and moves in the left and right direction when the screw shaft 322 rotates in the forward and reverse directions according to the rotating operation of the manual handle 321 in the forward and reverse directions, (313) are interlocked and moved left and right.

The back and forth moving member 33 is provided on the upper portion of the left and right moving member 31 and includes a back and forth moving plate 331 which is moved forward and backward and a back and forth moving plate 331, And guiding means 332.

The back and forth movement guide means 332 includes a second guide rail 332a arranged on the upper surface of the left and right moving plate 311 and a front side moving plate 332a coupled to the bottom surface of the front and rear moving plate 331 so as to be connected to the second guide rail 332a And the second guide rail 332a and the second guide block 332b are generally formed of a mechanical element called an LM guide. Thus, a detailed description of the structure will be omitted .

The back and forth movement drive unit 34 is constituted by connecting and moving the front and rear movable member 33 to the left and right and is constituted by a back and forth moving screw jack 34a configured to be coupled to the back and forth moving plate 331 with a movement nut.

The screw jack 34a for moving back and forth can be configured similarly to the above-described screw jack for left and right movement. The screw jack 34a is connected to the manual handle 341 and rotates. A screw shaft 342 is screwed to the screw shaft, And a moving nut 343 is provided. The movable nut 343 is coupled to the front and rear moving plate 331 so that when the manual shaft 341 rotates in the normal and reverse directions and the screw shaft 342 rotates in the forward and reverse directions, ) Are interlocked and moved back and forth.

On the other hand, the rotary member 35 is arranged on the upper portion of the longitudinal moving member 33 as a component for rotatably supporting the rotary table 36 on which the load is mounted. The rotary member 35 includes a bearing 351 coupled to the front and rear movable member 33 and a support shaft (not shown) rotatably coupled to the center of the bearing 351.

Here, the bearing 351 may be a thrust bearing having excellent rigidity against vertical load.

On the other hand, the rotary table 36 is coupled to the upper portion of the rotary member 35 as a component in which the load task equipment for the aircraft is substantially mounted. The rotary table 36 is composed of a plate-like plate member formed of a disc-shaped plate member coupled to the support shaft of the rotary member 35.

In addition, as shown in FIG. 4A, the rotary table 36 is provided with a loading aid member 37 for easily loading a load such as an ELINT antenna p having a protruding portion formed in a circular body among aircraft equipment .

5A, a member having a substantially rectangular plate shape is formed in a shape of arc-like shape as shown in FIG. 5A, And a plurality of rotors are assembled along the periphery of the rotary table 36. [0031] The load assisting member 37 is detachably attached to the load fixing means 38 composed of a butterfly nut and a screw to prevent the load from coming off.

In addition, the rotating table 36 is provided with a rotating plate stopping means 39 so that the aircraft equipment is mounted and is not idle in a predetermined position. Here, the stopping means 39 for the rotating plate is constituted by a fixing pin formed with a handle, and is detachably attached to the back and forth moving plate 331.

On the other hand, the left and right movable member 31 and the back and forth movable member 33 are provided with stopping means (not shown) formed in a rotary bar shape or the like so as to intermittently move the movable member in a state .

The apparatus for detaching and attaching aircraft equipment having a rotating function according to the present invention includes a plurality of rolling means 5 for rolling movement on the corner portion of the base member 1 so as to enable the entire moving and tilting operation of the aircraft equipment, And a rolling means driving unit 6 for adjusting the height of the rolling means 5.

The rolling means 5 is constituted by a rolling wheel commonly referred to as a caster and comprises a wheel portion 51 and a wheel frame 52 for supporting the wheel portion 51. The wheel frame 52 is provided with a braking device that makes it impossible to rotate the wheels 51.

5D is a perspective view showing a screw jack 6a for a rolling means used as a rolling means driving portion shown in FIG.

The rolling means drive unit 6 may be a screw jack 6a for a rolling means to which a screw shaft is coupled to the wheel frame 52.

Referring briefly to the internal structure of the screw jack 6a for the rolling means, referring to Fig. 5d, the screw jack 6a for the rolling means is a mechanical element commonly referred to as a screw jack.

The screw means 6a for the rolling means includes a worm gear 62 connected to the manual handle 65 and rotated inside the jack housing 61 as shown in Figure 5d, A screw shaft 63 is provided. A connecting member 66 having a connecting hole is connected to the end of the screw shaft 63 so as to be connected to the wheel frame 52.

Described screw jack 6a for a rolling means is rotated forward and backward in the vertical direction while the screw shaft 63 is rotated by the worm gear 62 rotated in normal and reverse directions in accordance with the normal and rotational operation of the manual handle 65, The height of the rolling means 5 coupled to the connecting member 64 provided at the end portion of the rolling means 63 is adjusted. Adjusting the height of the rolling means 5 installed at each corner of the base member 1 in this manner can tilt the aircraft equipment p that is seated on the loading unit 3, Assembly, and disassembly, the desired operation can be performed more conveniently and quickly.

If the rolling means 5 and the rolling means driving portion 6 are provided, not only the overall movement of the base member 1 but also the adjustment of the height of the base member 1 in the longitudinal, the tilting operation of the pile (p) can be performed, so that the assembly and disassembly of the aircraft equipment can be performed more quickly and accurately.

The movable handle 7 is a constituent element provided on the base member 1 so that an external force can be applied when the movable handle 7 is moved. The movable handle 7 includes a column 71 provided on both sides of the upper surface of the base member 1, And a knob 72 bent and formed at the upper end of the handle.

Hereinafter, the operation of the apparatus for attaching and detaching airplane equipment according to one embodiment of the present invention will be briefly described.

The manual handle 265 of the elevating screw jack 26 of the elevating means 2 is operated in one direction so that the height of the loading portion 3 is lowered by folding the driving arm 25 as shown in FIG. So that it is easy to mount the aircraft equipment (p), then mounts the aircraft equipment and moves to the mounting position of the aircraft.

Thereafter, when the manual handle 265 of the elevating screw jack 26 is operated in the other direction, the screw shaft 263 is rotated to move the moving nut 264 forward, so that the moving nut 264 is moved by the moving nut 264 The first link member 251 connected to the first moving shaft 22 is pulled forward and the folded driving arm 25 is unfolded as shown in FIG. 4A, so that the loading unit 3 is extended to the mounting position of the aircraft equipment So that the aircraft equipment (p) can be assembled conveniently.

Here, when the load mounted on the loading section 3 is a mission apparatus for an aircraft such as a radome, the loading auxiliary member 37 assembled on the top of the rotary loading table 36 is removed And can be used similarly to the above-described method after loading the mission equipment for the aircraft.

 The apparatus for attaching and detaching aircraft equipment according to the present invention can move the loading unit 3 not only in the vertical direction but also in the forward and backward directions and in the left and right direction and can perform the turning operation and the tilting operation, Will be explained in detail.

5A to 5C, when the rotary table 36 on which the aircraft equipment p is mounted is moved to the left and right, the manual handle 321 of the left and right screw jack 32a is rotated in the forward and reverse directions The moving nut 323 is moved in the left and right direction while the screw shaft 322 is rotated in the forward and reverse directions, so that the left and right moving plate 311 is moved to the left and right to move the rotating table 36 to the left and right.

When the rotary table 36 on which the aircraft equipment p is mounted is to be moved back and forth, when the manual handle 341 of the forward and backward movement screw jack 34a is rotated in the forward and reverse directions, the screw shaft 342 The forward movement plate 331 is moved forward and backward and interlocked so that the rotary table 36 is moved back and forth as the moving nut 343 is moved forward and backward.

When the rotary table 36 on which the aircraft equipment p is mounted is to be rotated, the fixing pin of the stopping means 39 for the rotary plate is detached from the forward / backward moving plate 331, So that the rotary table 36 is angularly moved by a predetermined angle and then the rotary table 36 is fixed to the front and rear moving plate 331 by using the stopping means 39 for the rotary table.

When it is necessary to tilt the aircraft equipment p by a certain angle, the manual handle 65 of the screw means for the rolling means, which is the rolling means driving unit 6, is rotated in the forward and reverse directions to adjust the height of the rolling means 5 . If the height of the rolling means 5 installed at each corner of the base member 1 is adjusted in this way, the mission equipment p for an aircraft seated on the mount unit 3 can be tilted, ), It is possible to perform a desired operation more conveniently and quickly by tilting at an appropriate angle at the time of maintenance, assembly, and disassembly.

However, the scope of the present invention is not limited to the configuration and method of the embodiments described above, and all or some of the embodiments may be selectively combined so that various modifications may be made to the embodiments. In addition, the present invention can be applied to all equivalents of inventions, such as inventions that can be modified, added, deleted, or replaced at the level of those skilled in the art, It belongs to the scope is self-evident.

1: base member 2: elevating means
21: first sliding member 22: first moving shaft
23: second sliding member 24: second moving shaft
25: drive arm 26: lift screw jack
3: loading part 31: left-right moving member
32: a left / right movement driving part 33:
34: forward / backward movement driving part 35:
36: Rolling stock 5: Rolling stock
5: rolling means 51:
52: wheel frame 6: rolling means driving part
7: Movable handle 71: Holding
72: Handle

Claims (8)

A base member;
Elevating means connected to the base member to move up and down; And
And a loading unit disposed on the elevating means and configured to load the load,
The loading section
A left and right moving member disposed at an upper portion of the elevating means;
A left and right movement driving unit connected to the left and right moving members to move the left and right moving members left and right;
A front-rear movable member disposed on an upper portion of the left-right moving member;
A back-and-forth moving unit connected to the back-and-forth moving member to move the back-and-forth moving member back and forth;
A rotating member rotatably coupled to the back and forth movable member to rotate the load; And
And a rotary table disposed above the rotary member, wherein the rotary table is capable of being seated on one surface of the rotary table. The method according to claim 1,
The rotating mount plate
A redistributor coupled to the rotatable member and configured to have a plate shape for seating the load; And
And a stacking assisting member detachably attached to the stacking plate and spaced apart from each other so as to enclose the stacking member so as to prevent the stacking of the stacking member mounted on the stacking plate from being separated from the stacking plate. Apparatus for detachment of equipment. The method according to claim 1,
A first sliding member disposed on the base member, the first sliding member extending in one direction and having a first moving hole formed to penetrate along the extending direction;
A first moving shaft inserted and slidable in the first moving hole;
A second sliding member disposed on the first sliding member, the second sliding member being formed to extend in one direction and having a second moving hole formed to penetrate along the extending direction;
And a second link member coupled to the second link member so as to be coupled to each other, wherein a lower end of the first link member is coupled to the first movement shaft, Arm; And
And an elevating screw jack configured to move the first moving shaft back and forth by rotation to provide a driving force for moving the first moving shaft in the forward and backward directions. The method of claim 3,
Wherein the left-
A left and right moving plate which is laterally moved;
A first guide rail disposed laterally on the second sliding member; And
And a first guide block coupled to the left and right moving plates to be connected to the first guide rail,
Wherein the back-
A back and forth moving plate moved back and forth;
A second guide rail disposed back and forth on the left and right moving plates; And
And a second guide block coupled to the front and rear moving plates to be connected to the second guide rail. 5. The method of claim 4,
Wherein the left and right movement drive unit comprises a left and right movement screw jack to which the movement nut is coupled to the left and right movement plates,
Wherein the back-and-forth movement driving unit comprises a back-and-forth moving screw jack to which the moving nut is coupled to the back and forth moving plate. The method according to claim 1,
Further comprising a stopping means configured to fix the movement of the left and right movable member, the back and forth movable member, and the rotary table to prevent the left and right movable member, the back and forth movable member, and the rotary table from being moved or rotated Wherein the apparatus is for disassembly of aircraft equipment. The method according to any one of claims 1 to 6,
A plurality of rolling means respectively installed at the ends of the base member;
And a rolling means driving unit connected to the rolling means for adjusting the height of the rolling means. 8. The method of claim 7,
The rolling means comprises:
Wheels; And
And a wheel frame for supporting the wheel portion,
Wherein the rolling means drive unit comprises a screw jack for a rolling means, the screw shaft being coupled to the wheel frame to adjust the height of the rolling means.

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