KR101805401B1 - Standard Platform for Aircraft - Google Patents

Standard Platform for Aircraft Download PDF

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Publication number
KR101805401B1
KR101805401B1 KR1020150188122A KR20150188122A KR101805401B1 KR 101805401 B1 KR101805401 B1 KR 101805401B1 KR 1020150188122 A KR1020150188122 A KR 1020150188122A KR 20150188122 A KR20150188122 A KR 20150188122A KR 101805401 B1 KR101805401 B1 KR 101805401B1
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KR
South Korea
Prior art keywords
unit
assembly
upper plate
plate
support
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KR1020150188122A
Other languages
Korean (ko)
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KR20170078024A (en
Inventor
강강용
Original Assignee
한국항공우주산업 주식회사
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Priority to KR1020150188122A priority Critical patent/KR101805401B1/en
Publication of KR20170078024A publication Critical patent/KR20170078024A/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G1/00—Scaffolds primarily resting on the ground
    • E04G1/15—Scaffolds primarily resting on the ground essentially comprising special means for supporting or forming platforms; Platforms
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G5/00—Component parts or accessories for scaffolds
    • E04G5/08—Scaffold boards or planks
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G5/00—Component parts or accessories for scaffolds
    • E04G5/10—Steps or ladders specially adapted for scaffolds

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Tires In General (AREA)

Abstract

The present invention relates to a standard platform for aircraft, and more particularly to a platform for final assembly or subassembly work for the production of aircraft, in which the platform can be formed by assembly of platform units having various shapes and functions And a standard platform for standardized aircraft.

Description

Standard Platform for Aircraft {

The present invention relates to a standard platform for aircraft, and more particularly to a platform for final assembly or subassembly work for the production of aircraft, in which the platform can be formed by assembly of platform units having various shapes and functions And a standard platform for standardized aircraft.

In the final assembly and subassembly work for the production of aircraft, platforms for aircraft having various shapes and sizes are used.

The aircraft platform is designed, manufactured and installed on the ground, and generally performs a final assembly or subassembly operation for manufacturing an aircraft on a support portion fixed to the ground and an upper plate portion formed on the support portion.

At this time, for the efficient and safe operation of the aircraft platform, a dedicated platform corresponding to the shape and size of the object (aircraft body, part of the body of the airplane) to be operated is generally designed, manufactured and used.

However, since the platform for an aircraft is manufactured by using a dedicated platform according to the shape and size of the object, as described above, it can not be reused for the operation of objects having different shapes and sizes, There is a problem that another dedicated platform must be manufactured and used.

This is not efficient because it is not used in the production of aircraft having different shapes and sizes after using a dedicated platform for aircraft production.

That is, the design time is excessively required due to repetition of unnecessary design for the design of the dedicated platform of the aircraft, and it is difficult to recycle the parts and materials of the platform, resulting in an increase in the production cost of the aircraft.

As a prior art related to this, a universal platform for aircraft production has been disclosed in Korean Patent Publication No. 2010-0119266 ("Universal platform and method of assembling an aircraft using it, "

Korean Patent Publication No. 2010-0119266 ("Universal platform and method of assembling an aircraft using the same, "

SUMMARY OF THE INVENTION It is an object of the present invention to provide a platform for a final assembly or subassembly operation for manufacturing an aircraft, And to provide a standard platform for an aircraft that is standardized to be buildable by assembly.

A standard platform for an aircraft according to the present invention comprises a platform unit including an upper plate unit including a plate-shaped plate body and a support unit including a columnar column body, And a supporting portion formed by assembling the supporting unit in a vertical direction at a lower end of the upper plate portion.

The upper plate unit includes an upper plate assembly formed in a direction perpendicular to the lower surface of the plate body, and the upper plate assembly includes at least one upper plate assembly hole formed in a horizontal direction.

The upper plate unit includes a column assembly formed horizontally at a lower end of the upper plate assembly, wherein the column assembly includes at least one column assembly hole formed in a vertical direction.

In addition, the support unit includes a support assembly formed horizontally at both ends of the column shaft of the column body, and the support assembly includes at least one support assembly hole formed in the horizontal direction.

The upper plate unit includes a sliding plate slidably inserted in and drawn out from one end of the upper plate assembly part, a sliding guide formed horizontally in the upper plate assembly part to move the sliding plate, and at least one And a sliding unit including a sliding roller formed on the sliding unit.

The upper plate unit may include a folding plate formed in a horizontal direction at one end of the plate body, a folding plate hinged to be foldable in a vertical direction, and a lower plate extending horizontally from one end of the upper plate assembly below the folding plate, And a folding unit including a folding plate support portion formed to be capable of being drawn in and drawn out from one end of the upper plate assembly portion in a horizontal direction.

The upper plate unit may include an upper assembly including at least one upper assembly hole formed on an upper surface of the plate body.

In addition, the standard platform for an aircraft includes a guide part formed to be assembled with the upper assembly part, wherein the guide part includes a guide body, a guide assembly part formed in a horizontal direction of the lower end of the guide body so as to be assembled with the upper assembly part, And a guide unit including at least one guide assembly hole formed in the guide assembly.

In addition, the standard platform for an aircraft includes a moving part formed to connect the upper plate part to the ground, the moving part includes a movable supporting unit formed to be assembled with the upper plate part and the ground, Shaped pedestal unit and a movement guide unit that is assemblably formed on the movable support unit.

The moving support unit may include an upper movable support unit having an upper movable support unit including an upper movable support hole formed to be assembled with the upper plate assembly or the upper assembly of the upper plate unit, And a lower movement support unit having a lower movement support unit including a lower movement support hole formed at one end thereof, and the other end of the upper and lower movement support units is assemblable.

A standard platform for an aircraft according to the present invention is a platform for final assembly and subassembly work for the production of an aircraft. The platform is standardized so that it can be formed by assembly of platform units having various shapes and functions, There are advantages that can be used in work.

In particular, the standard platform for aircraft according to the present invention is standardized so that it can be formed by assembly of platform units having various formations and functions, so that it is not necessary to repeat unnecessary design, There is an advantage in that the manufacturing cost of the device is reduced.

1 shows a standard platform for an aircraft according to the invention;
Figure 2 is another diagram showing a standard platform for an aircraft in accordance with the present invention;
3 shows a top plate unit of a standard platform for an aircraft according to the invention.
4 is another view of a top plate unit of a standard platform for an aircraft according to the present invention.
5 shows a support unit of a standard platform for an aircraft according to the invention.
6 is a view showing a sliding unit of a top plate unit according to the present invention.
7 is a view showing a folding unit of a top plate unit according to the present invention.
8 is a view showing a guide part of a standard platform for an aircraft according to the present invention and a guide unit for forming the guide part.
9 is a view showing a moving part of a standard platform for an aircraft according to the present invention and a mobile unit for forming the moving part.

Hereinafter, a standard platform for an aircraft according to the present invention having the above-described features will be described in detail with reference to the accompanying drawings.

Prior to this, terms and words used in the present specification and claims should not be construed in a conventional or dictionary sense, and the inventor should appropriately define the concept of the term to describe its invention in the best possible way The present invention should be construed in accordance with the spirit and concept of the present invention.

Therefore, the embodiments described in the present specification and the configurations shown in the drawings are merely the most preferred embodiments of the present invention, and not all of the technical ideas of the present invention are described. Therefore, It is to be understood that equivalents and modifications are possible.

FIG. 1 is a view showing a standard platform 1000 for an aircraft according to the present invention, FIG. 2 is another view showing a standard platform 1000 for an aircraft according to the present invention, and FIG. 4 is a view showing another embodiment of the top plate unit 10 of the standard platform 1000 for an aircraft according to the present invention and FIG. And the support platform 20 of the standard platform 1000 is shown.

The standard platform 1000 for an aircraft according to the present invention is an aircraft platform formed for final assembling or subassembly for manufacturing an aircraft. The platform 1000 includes a top plate unit 10 having a plate-shaped plate body 11, And a platform unit (50) including a support unit (20) having a pillar body (21) of a shape.

In other words, since the platform can be formed by assembling the platform units 50 having various shapes and functions, the platform 1000 for an aircraft according to the present invention can provide a platform having a desired shape and size to bolts and nuts Can be easily formed by assembling by using.

1 and 2, the standard platform 1000 for an aircraft according to the present invention includes a top plate 100, which is a space for working, and a top plate 100, And a support portion 200 for fixing and supporting the support portion 200 so as to hold the support portion 200 therebetween.

The upper plate unit 100 may be formed by assembling the upper plate units 10 as one of the platform units 50 in a horizontal direction and the support unit 200 may be formed in the support unit 200, (20) may be formed by assembling the upper plate unit (10) forming the upper plate part (100) in a direction perpendicular to the lower end of the upper plate part (100).

In this case, the above-described horizontal direction and vertical direction are directions for describing the standard platform 1000 for an aircraft according to the present invention in detail, the horizontal direction is a direction parallel to the ground, and the vertical direction is a direction perpendicular to the ground It says.

3, the upper plate unit 10 is assembled with each other in the horizontal direction to form the upper plate unit 100, so that the upper plate unit 10 is perpendicular to the lower surface of the plate body 11 in a plate- And the upper plate assembly 12 includes at least one upper plate assembly hole 12-1 formed in the horizontal direction.

That is, the upper plate unit 10 includes an upper plate assembly hole 12-1 formed in a horizontal direction in an upper plate assembly 12 formed in a direction perpendicular to the lower surface of the plate body 11, The upper plate unit 10 can be assembled in a horizontal direction by using bolts and nuts through the holes 12-1 to form the upper plate unit 100. [

At this time, it is preferable that the upper plate assembling part 12 is formed on all four edges of the plate body 11 in the horizontal direction so that the plate body 11 can be assembled in all four directions in the horizontal direction, At least one or more upper plate assembly holes 12-1 of the assembly section 12 are formed in the upper plate assembly section 12 so that they can be prevented from being separated from each other when assembled between the upper plate units 10, It is preferable that the worker has a sufficient number of weight to stand the weight of the worker.

In addition, the upper plate assembly 120 may be formed only on the lower edge of the plate body 11, but in order to prevent the plate body 11 from being damaged by the weight of the operator and external force, It is needless to say that it may be formed as a lattice.

Reference numeral 11-1 denotes a long plate member which can be formed on the upper surface of the plate body 11. [ However, it is needless to say that the long plate member may be formed in various shapes and materials as one embodiment of the upper plate unit 10.

4, the upper plate unit 10 includes a column assembly part for assembling with the support unit 20 of the support part 200, which supports the upper plate part 100 so that the upper plate part 100 has a predetermined vertical height from the ground surface, (13).

The column assembly 13 is formed at the lower end of the upper plate assembly 12 and is formed in a horizontal direction to be assembled with the support unit 20.

The column assembly 13 includes a column assembly hole 13-b, which is formed in at least one vertical direction to be assembled with the support unit 20 using bolts and nuts, like the upper assembly 12, 1).

The column assembly hole 13-1 is formed in the column assembly 13 in the same manner as the upper plate assembly hole 12-1 and the assembly of the upper plate unit 10 and the support unit 20 It is preferable that the upper plate 100 is formed to have a number capable of supporting the upper plate 100 as well as being prevented from being separated from each other.

5, the support unit 20 forming the support unit 200 includes a columnar column body 21 and support assemblies (not shown) formed horizontally at both ends of the column axis of the column body 21, (22), wherein the support assembly (22) includes a support assembly hole (22-1) formed in at least one vertical direction.

That is, the support unit 20 includes a support assembly 22 formed to be in contact with the column assembly 13 of the upper plate unit 10, and the support assembly 22 supports the column assembly 13 and a support assembly hole 22-1 for assembling using bolts and nuts.

In this case, it is preferable that the support assembly hole 22-1 is formed to correspond to the position of the column assembly hole 13-1 in order to be assembled using the bolt and nut with the bolt hole 13-1 However, if the assembly can be easily and accurately assembled with the column assembly 13, the number of the column assembly holes 13-1 may be larger or smaller than the number of the column assembly holes 13-1.

As described above, since the support assembly 22 is formed at both ends of the column shaft 21, one end of the support unit 20 can be assembled with the upper plate unit 10, The other end of the unit 20 is formed so as to be able to be assembled (fixed) on the ground surface so that the support unit 20 can be fixed to the ground in a vertical direction, and the upper plate 100 can be fixed .

Of course, it is preferable that the other end of the column shaft of the support unit 20, which is formed so as to be able to be assembled (fixed) with the ground, has the shape of the support assembly 22 described above. However, It is of course possible to have a shape of a hole.

The support unit 20 can be assembled using bolts and nuts between the support units 20 by forming the support assembly 22 at both ends of the column body 21, Can be controlled in the vertical direction.

As shown in FIG. 5, the columnar body 21 of the support unit 20 is preferably of a cylindrical shape. However, if the support portion 200 can support the upper plate portion 100 with a certain strength, However, it is needless to say that various embodiments of the column body may be used.

FIG. 6 is a view showing the sliding unit 10a of the top-fin unit 10 according to the present invention, and FIG. 7 is a view showing a folding unit 10b of the top plate unit 10 according to the present invention.

When the operation of the object (aircraft body, aircraft body unit body, etc.) (1) for the operation is completed, when the final assembly or subassembly of the aircraft is performed using the platform, When the object 10 is pulled out from the platform, there is a fear of coming into contact with the upper plate portion and being broken.

Therefore, among the upper units 10 forming the upper plate 100, the upper plate unit 10, which is in contact with the object 1, is formed so as to be able to control the area in the horizontal direction to prevent contact with the object 1 .

As described above, the upper plate unit 10 of the standard platform 1000 for an aircraft according to the present invention is slid from the upper plate assembly 12 so as to control the area in the horizontal direction, And a folding unit 10b which is hinged from the plate body 11 so as to be foldable.

6, the sliding unit 10a of the upper plate unit 10 includes a sliding plate 10a-1 slidably inserted into and drawn out from one end of the upper plate assembly, A sliding guide 10a-1 formed horizontally on the sliding guide 10a-1 for moving the sliding plate 10-1a and a sliding roller 10a-3 formed on the sliding guide 10a-1, do.

The sliding plate 10a-1 is formed slidably from the upper plate assembly 12 along a sliding guide 10a-2 formed in parallel with the plate body 11 of the upper plate unit 10, Out operation from the assembly section 12 is possible.

The sliding roller 10a-3 is rotatably formed on the sliding guide 10a-2 so that the sliding plate 10a-1 is slidable along the sliding guide 10a-2 So that the sliding plate 10a-1 can be pulled out from the upper plate assembly 12.

That is, the upper plate unit 10 includes a sliding unit 10a, and the sliding plate 10a-1 is formed to be capable of being pulled out from the upper plate assembly 12, The sliding plate 10a-1 is drawn into the upper plate assembly 12 to prevent the object 1 from being damaged by being in contact with the upper plate 100 when the object 1 is pulled in and drawn out from the platform In addition, during the assembling work, the sliding plate 10a-1 is pulled out to enable safe movement and operation of the operator.

7, the folding unit 10b of the upper plate unit 10 is formed in a horizontal direction at one end of the plate body 11 and includes a folding plate 10b- 1 and a folding plate support portion 10b-2 extending horizontally from one end of the upper plate assembly portion 12 below the folding plate 10b-1 to support the folding plate 10b-1 .

At this time, the folding plate support portion 10b-2 is not only supported by the folding plate 10b-1 but also horizontally pulled in from the one end of the upper plate assembly portion 12 for safe pull- And is drawable.

The folding plate 10b-1 is hinged to be foldable in the vertical direction and is preferably folded upward to prevent contact with the object 1 and prevent contact with the supporting portion 200 It is not limited to one.

The upper plate unit 10 includes a folding unit 10b and the folding unit 10b is hinged from the plate body 11 so as to be vertically foldable so that the sliding unit 10a It is possible to prevent the object 1 from being damaged by contact with the upper plate 100 when the object 1 is pulled in or taken out from the platform, and also enables safe movement and operation of the worker.

8 is a view showing a guide unit 300 of a standard platform 1000 for an aircraft according to the present invention and a guide unit 30 forming the same.

1 to 2 and 8, an upper plate unit 10 of a standard platform 100 for an aircraft according to the present invention includes an upper assembly hole (not shown) formed on the upper surface of the plate body 11 The standard platform 1000 for an aircraft according to the present invention further includes a guide part 300 formed to be assembled with the upper assembly part 14 .

Since the upper plate portion 100 is formed by the support portion 200 so as to have a predetermined height in the vertical direction from the ground for assembling the object 1, the guide portion 300 prevents the safety of the worker and the falling of the device As shown in FIG.

The guide unit 300 is formed by assembling a guide unit 30. The guide unit 30 includes a guide body 31 and a lower end of the guide body 31 so as to be assembled with the upper assembly unit 14. [ A guide assembly 32 formed in a horizontal direction and a guide assembly hole 32-1 formed in at least one guide assembly 32. [

The guide body 31 may have various shapes such as a lattice shape shown in FIG. 8 or a column shape only in a vertical direction, and the guide assembly 32 may be formed in the upper assembly hole 14-1 so that the upper assembly hole 14-1 and the guide assembly hole 32-1 face each other by using bolts and nuts So that the guide part 300 can be assembled to the upper plate part 100.

9 is a view showing a moving part 400 of the standard platform 1000 for an aircraft according to the present invention and a moving unit 40 forming the moving part 400. [

Since the upper plate 100 of the standard platform 1000 for an aircraft according to the present invention is formed to have a predetermined height in the vertical direction from the ground by the support portion 200, as shown in FIGS. 1 to 2 and 9 And a stair-like moving part 40 connecting the ground and the upper plate part 100, including a stepping foot on which an operator can walk.

The moving part 400 can also be formed by assembling between the platform units 50, and the moving part 400 is formed by assembling the moving units 40.

The moving unit 40 includes a top supporting unit 10 of the top plate 100 and a moving supporting unit 41 including a moving supporting part 41-1 formed at both ends so as to be assembled with the ground.

The movable support unit 410 is preferably formed obliquely from the ground because it serves to fix and support the foot plate so that the operator can move between the top plate 100 and the ground using a foot plate.

The movable support unit 41 includes an upper movable support hole 41a formed to be assembled with the upper plate assembly 12 of the upper plate unit 10 or the upper assembly portion 140 of the upper plate unit 10, 2 that includes an upper movable support unit 41a formed at one end thereof and an upper movable support hole 41b-2 formed so as to be assembled with the ground, And a lower moving support unit 41b having one end 41b-1 formed at one end thereof.

That is, the movable support unit 41 can be formed as a unit having a predetermined length, and the upper movable support portion 41a-1, which is formed to be assembled with the upper plate portion 100, And a lower moving support unit 41b having a unit 41a and a lower moving support unit 41b-1 formed at one end so as to be assembled with the ground surface. The upper and lower movable support units 41a and 41b- 41b, respectively.

Furthermore, the moving support unit 41 may include a central movement support unit (not shown) formed to be assemblable between the upper and lower movable support units 41a and 41b.

The central moving support unit can be assembled between the upper and lower movable supporting units 41a and 41b so that the length of the movable supporting unit 41 corresponding to the height between the ground and the upper plate 100 .

Of course, in addition to the above-described configuration, the upper movable support unit 41a and the lower movable support unit 41b are slidable with respect to each other so that one of them can be pulled out and drawn out, It is possible to make an embodiment of various shapes.

The mobile unit 40 includes a pedestal unit 42 having a pedestal body 42-1 formed to be assembled with the mobile support unit 41, May be assembled using the moving support unit 41 and the bolts and nuts including the footplate assembly holes 42-2 formed at both ends of the body 42-1.

It is preferable that the footrest unit 42-1 is formed in a plate shape so that an operator or the like can move on the foot, and the footrest unit 42 should be assembled in a horizontal direction for the safe movement of the worker.

Therefore, as shown in FIG. 9, the foot punching unit 42 can be assembled with the projecting hole 41-2 of the protruding portion 41-1, which protrudes horizontally from the movable support unit 41, The footrest assembly hole 42-2 can be formed.

However, it should be understood that the present invention is not limited thereto, and that the pedestal unit 42 can be assembled with the movable support unit 41 by various assembling methods.

The moving unit 40 includes a moving guide unit 43 formed to be assembled with the moving support unit 41. The moving guide unit 43 includes a moving guide body 43-1 And a movement guide assembly hole 43-2a formed on the lower surface of the movement guide body 43-1 so as to be assembled with an upper movement hole 41-3 formed in the upper direction of the movement support unit 41, And a movement guide assembling part 43-2 including the guide part 43-2.

Needless to say, it is needless to say that the movement guide unit 43 is not limited to the structure in which it is assembled with the movable support unit 41, but may be variously constructed.

1000: Standard platform for aircraft
100: upper plate part 200: support part
300: guide part 400: moving part
10: Top plate unit
11: plate body
12: upper plate assembly part 12-1: upper plate assembly hole
13: Column assembly section 13-1: Column assembly hole
14: upper assembly hole 14-1: upper assembly hole
10a: Sliding unit 10a-1: Sliding plate
10a-2: Sliding guide 10a-3: Sliding roller
10b: Folding unit
10b-1: Folding board 10b-2: Folding board
20: Column unit
21: column body
22: Support assembly part 22-1: Support assembly hole
30: guide unit 31: guide body
32: Guide assembly part 32-1: Guide assembly hole
40: mobile unit
41:
41-1: protrusion 41-2: protrusion hole
41-3: Upper moving hole
41a: upper moving support unit
41a-1: Upper moving supporting part 41a-2: Upper moving supporting hole
41b: a lower movable support unit
41b-1: Lower movable supporting part 41b-2: Lower movable supporting hole
42: Scaffolding unit
42-1: foot body 42-2: foot assembly hole
43: movement guide unit 43-1: movement guide body
43-2: Movement guide assembly part 43-2a: Movement guide assembly hole

Claims (10)

A platform unit including an upper plate unit 10 including a plate-shaped plate body 11 and a support unit 20 including a columnar column body 21 is assembled and formed,
An upper plate 100 formed by assembling the upper plate units 10 in a horizontal direction,
And a support part 200 formed by assembling the support unit 20 in a vertical direction at a lower end of the upper plate part 100,
The upper plate unit 10
And an upper plate assembly 12 formed in a vertical direction on the lower surface of the plate body 11 and including upper plate assembly holes 12-1 formed in at least one horizontal direction in each of four directions in the horizontal direction , Assembled and disassembled in the horizontal direction in which the upper plate units (10) are selected using bolts and nuts through the upper plate assembly hole (12-1)
And a column assembly 13 including a column assembly hole 13-1 formed in a horizontal direction at a lower end of the upper plate assembly 12 and formed in at least one vertical direction, -1), the upper plate unit 10 and the support unit 20 can be assembled and disassembled,
The support unit (20)
And a support assembly (22) formed to have an area selected in the horizontal direction at both ends of the column shaft of the column body (21)
The support assembly 22 includes at least one support assembly hole 22-1 formed in the vertical direction and supports the column assembly 13 selected at the upper portion through the support assembly hole 22-1. And can be fixed to and released from the column assembly portion 13 using bolts and nuts or can be fixed and released to the column assembly portion 13 through bolts and nuts through the support assembly holes 22-1, Or can be fixed and released in the vertical direction between the support units 20 by means of bolts and nuts through the support assembly holes 22-1 so that the upper surface of the upper plate 100 Wherein the height of the standard platform is adjustable.
delete delete delete The method according to claim 1,
The upper plate unit 10
A sliding plate 10a-1 slidably inserted in and drawn out from one end of the upper plate assembly 12 in a horizontal direction,
A sliding guide 10a-2 formed horizontally in the upper plate assembly 12 to move the sliding plate 10a-1,
, And a sliding unit (10a) including at least one sliding roller (10a-3) formed in the sliding guide (10a-2).
The method according to claim 1,
The upper plate unit 10
A folding plate 10b-1 formed horizontally at one end of the plate body 11 and hinged to be vertically foldable,
The folding plate 10b-1 is horizontally extended from one end of the upper plate assembly 12 so as to be able to support the folding plate 10b-1. And a folding unit (10b) including a folding board support (10b-2) formed to be capable of being drawn in and pulled out.
The method according to claim 1,
The upper plate unit 10
And an upper assembly part (14) including an upper assembly hole (14-1) formed at least on the upper surface of the plate body (11).
8. The method of claim 7,
The standard platform 1000 for an aircraft
And a guide part (300) formed to be assembled with the upper assembly part (14)
The guide part 300
A guide assembly 32 formed in a horizontal direction at a lower end of the guide body 31 so as to be assembled with the upper assembly 14 and at least one Is formed by assembling a guide unit (30) including a guide assembly hole (32-1).
The method according to claim 1,
The standard platform for an aircraft (1000)
And a moving part 400 formed to connect the upper plate part 100 and the ground,
The moving unit 400
A movable support unit 41 formed to be assembled with the top plate 100 and the ground,
A plate-shaped pedestal unit 41 formed to be assembled in the horizontal direction to the movable support unit 41,
And a movement guide unit (43) formed so as to be assembled on the upper portion of the mobile support unit (41).
10. The method of claim 9,
The moving support unit (41)
An upper moving supporting portion 41a-1 including an upper moving supporting hole 41a-2 formed to be assembled with the upper plate assembling portion 12 or the upper assembling portion 14 of the upper plate unit 10 is formed at one end An upper moving support unit 41a,
(41b-1) including a lower movable support hole (41b-2) formed so as to be able to be assembled with the ground, is formed at one end of the lower movable support unit
And the other end of the upper and lower movable support units (41a, 41b) is formed to be assembled.
KR1020150188122A 2015-12-29 2015-12-29 Standard Platform for Aircraft KR101805401B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020150188122A KR101805401B1 (en) 2015-12-29 2015-12-29 Standard Platform for Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020150188122A KR101805401B1 (en) 2015-12-29 2015-12-29 Standard Platform for Aircraft

Publications (2)

Publication Number Publication Date
KR20170078024A KR20170078024A (en) 2017-07-07
KR101805401B1 true KR101805401B1 (en) 2018-01-10

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US11718426B1 (en) 2020-05-29 2023-08-08 United Launch Alliance, L.L.C. Highly adaptable platform

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KR102364678B1 (en) 2017-06-20 2022-02-18 엘지전자 주식회사 Mobile terminal
KR102174213B1 (en) 2018-12-04 2020-11-04 한국항공우주산업 주식회사 Smart platform for aircraft
KR102591224B1 (en) * 2023-05-08 2023-10-20 (주)대산이엔지 Scaffolding with avoidance type space structure

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US11718426B1 (en) 2020-05-29 2023-08-08 United Launch Alliance, L.L.C. Highly adaptable platform

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