KR101665526B1 - Pre-cast module for air beacon - Google Patents

Pre-cast module for air beacon Download PDF

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Publication number
KR101665526B1
KR101665526B1 KR1020160030793A KR20160030793A KR101665526B1 KR 101665526 B1 KR101665526 B1 KR 101665526B1 KR 1020160030793 A KR1020160030793 A KR 1020160030793A KR 20160030793 A KR20160030793 A KR 20160030793A KR 101665526 B1 KR101665526 B1 KR 101665526B1
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KR
South Korea
Prior art keywords
module
hole
height adjusting
height
string
Prior art date
Application number
KR1020160030793A
Other languages
Korean (ko)
Inventor
권득윤
Original Assignee
권득윤
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Publication date
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Priority to KR1020160030793A priority Critical patent/KR101665526B1/en
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Publication of KR101665526B1 publication Critical patent/KR101665526B1/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
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/18—Visual or acoustic landing aids
    • B64F1/20—Arrangement of optical beacons
    • E—FIXED CONSTRUCTIONS
    • E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
    • E01C5/00—Pavings made of prefabricated single units
    • E—FIXED CONSTRUCTIONS
    • E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
    • E01F9/00—Arrangement of road signs or traffic signals; Arrangements for enforcing caution
    • E01F9/50—Road surface markings; Kerbs or road edgings, specially adapted for alerting road users
    • E01F9/535—Kerbs or road edgings specially adapted for alerting road users
    • E01F9/547—Kerbs or road edgings specially adapted for alerting road users illuminated
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
    • F21S8/00—Lighting devices intended for fixed installation
    • F21S8/02—Lighting devices intended for fixed installation of recess-mounted type, e.g. downlighters
    • F21S8/022—Lighting devices intended for fixed installation of recess-mounted type, e.g. downlighters intended to be recessed in a floor or like ground surface, e.g. pavement or false floor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V21/00—Supporting, suspending, or attaching arrangements for lighting devices; Hand grips
    • F21V21/02—Wall, ceiling, or floor bases; Fixing pendants or arms to the bases
    • F21V21/04—Recessed bases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V21/00—Supporting, suspending, or attaching arrangements for lighting devices; Hand grips
    • F21V21/36—Hoisting or lowering devices, e.g. for maintenance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2203/00—Aircraft or airfield lights using LEDs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
    • F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
    • F21W2111/06—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Road Signs Or Road Markings (AREA)

Abstract

The present invention relates to a strip foundation pre-cast module for an airway beacon and a construction method thereof, wherein when constructing a lamp for an air beacon on an airstrip, connection wiring of a beacon apparatus for an airway beacon is easily distributed and installed. Moreover, without disassembling a conventional conduit, a newly established pipe is installed for working to be quick, and an up and down steel hole having excellent compatibility and an adjustable height and a height adjustable pre-cast module are constructed.

Description

PRE-CAST MODULE FOR AIR BEACON [0001]

The present invention relates to a line base precast module for an aviation light and a construction method using the same. More particularly, the present invention relates to a method of installing a lamp for an aviation lightening in an airplane runway, A pre-cast module for an air-conditioner, which is constructed by installing a new pipe without dismantling the existing conduit and constructing an up-down steel hole and a height-adjustable pre-cast module, And a method of using the same.

In general, when the four seasons are clear, the runway may be damaged or cracked due to severe snowfall in the winter, freezing of the runway due to cold, change of hot temperature in the summer, and the like. It was necessary to repackage the damaged area before it reached its end of life.

In order to induce safe operation of airplanes and automobiles, various structures are installed on runways and roads of airfields. As one of these structures, lamps for lighting have been installed, and maintenance of runways has been very difficult. It is necessary to remove the existing conduit tube at the time of constructing the substructure or substructure of the lower part of the surface, so that it takes a long time to work and there is a problem that it is difficult to use because it is overlapped with the place of the newly installed conduit.

Especially, the road pavement such as the runway equipped with the lamp for aviation lighting is mainly cured by concrete, and it takes a long time, and it is not possible to construct the horizontal height of the runway and the height of the lamp for air- .

Korean Registered Patent No. 10-0406482 (registered on November 07, 2003)

SUMMARY OF THE INVENTION Accordingly, the present invention has been made keeping in mind the above problems occurring in the prior art, and it is an object of the present invention to provide a precast module, And it is an object of the present invention to provide a construction method using the same.

The present invention relates to a line foundation precast module for aviation light which can be directly applied on site for replacement of a string base structure of an runway and can be adjusted in height so that the level of the runway surface and the precast module can be quickly and easily constructed, And to provide a construction method using the same.

It is an object of the present invention to provide a line-based precast module for an aviation light source that can be quickly, quickly, and safely replaced with a pre-cast construction method, thereby providing a convenient, quick, and easy-to- .

In addition, the present invention relates to a line-based pre-cast module for an aviation light source which can be easily installed in a connection wiring of a connecting wiring of an airplane for aviation lighting and can secure a new pipe with an existing conduit, And the like.

In addition, the present invention provides a precast module for airborne lighting string base structure which can be installed by adjusting the height of a lamp for air conditioning by providing a height adjusting hole for aviation equipments in the inner side of a string base precast module and a construction method using the same And the like.

In order to accomplish the above object, the present invention provides a structure of a runway which is composed of a lobster layer 102 and an ascon layer 104 and has a module hole 10 formed at the center thereof, And a string-based precast module (100) installed such that the height of the string-based precast module (100) is adjusted up and down, wherein the string-based precast module (100) comprises: a hypsoxial portion (106) formed on the inner side of the module hole (10); A base precast module 108 inserted into the inside diameter of the ultra-high speed part 106 and having a core hole 18 formed at the center thereof and a module body 16 having a height adjusting unit hole 13 formed therein; An up-down iron hole 110 installed in the inner side of the core hole 18 to adjust the height thereof; And a height adjusting unit hole (13) formed in the base precast module (108), and installed so as to be elevated up and down. And a height adjusting unit 114 installed to protrude from the lower surface.

The height adjusting unit 114 includes: a height adjusting bolt 29 coupled to the height adjusting unit hole 13; A module fixture (116) fixed to the module body (10) and fastened to the height adjustment bolt (29); And a lower fixing plate 30 fixed to the lower end of the height adjusting bolt 29.

The module fixture 116 includes a cylindrical plate-shaped plate body 32; And an upper fixing plate 34 fixed to the outer circumferential surface of the fixing plate body 32 in a horizontal direction.

The up-down iron hole 110 includes a cylindrical lower body 20, a plurality of coupling portions 22 formed on the inner side of the lower body 20, and a plurality of fixing brackets 23 And a plurality of fixing brackets 25 formed on the inner side of the upper body 24. The lower bracket 25 is fixed to the upper bracket 25 of the lower body 20, 23 and a height adjusting bolt 28 which is installed by fastening the fixing bracket 25 of the upper body 24 and adjusts the height of the upper body and the lower body.

The present invention provides a method of manufacturing an airway runway including a basement structure 200 formed of a rubble layer 102 and an ascon layer 104 and having a steel hole at a central portion thereof, ; Cutting and removing the foundation structure (200) to form a module hole (10); Pouring the bottom of the module hole (10) to pour the bottom of the module hole (10); Inserting the string base precast module after inserting the floor at the first speed; And injecting ultra fast velocity between the gaps of the string-based precast module inserted into the module hole 10.

The step of forming the string based precast module for an aviation arc includes the steps of installing a reinforcing bar and an earthing rod; Installing up-down iron holes; And a step of laying and wiring the cable.

According to the present invention, there is an effect of shortening the construction process by adjusting the horizontal height of the runway and the precast module at the time of constructing the line foundation structure of the runway for aerial lighting, and preventing the large-scale aviation safety accident.

In addition, since a steel hole capable of height adjustment is provided, it can be installed freely according to a place by a construction method using a precast module, so that there is an effect of excellent compatibility, and there is an effect of excellent on-site construction and workability.

BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a cross-sectional view showing the structure of a string base precast module for an airlight according to the present invention
2 is an exploded cross-sectional view showing the structure of a string base precast module for an airlight according to the present invention
3 is a view showing a construction method using a string base precast module for aviation light of the present invention
4 is a process diagram showing a construction method using a string base precast module for an aviation light of the present invention
Fig. 5 is a plan view showing the structure of a string base precast module for an airlight according to the present invention
Fig. 6A is a side sectional view of Fig. 5
Fig. 6B is a plan view of Fig.
6C is an enlarged view showing a structure of a height adjusting unit of a string base precast module for an aviation light of the present invention

BRIEF DESCRIPTION OF THE DRAWINGS The advantages and features of the present invention, and the manner of achieving them, will be apparent from and elucidated with reference to the embodiments described hereinafter in conjunction with the accompanying drawings.

It should be understood, however, that the invention is not limited to the disclosed embodiments, but is capable of many different forms and should not be construed as limited to the embodiments set forth herein; It is intended that the disclosure of the present invention be limited only by the terms of the appended claims.

In the following description, well-known functions or constructions are not described in detail since they would obscure the invention in unnecessary detail.

Rather, the embodiments disclosed herein are provided so that the disclosure can be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.

The terms first, second, etc. may be used to describe various components, but the components are not limited by the terms. The terms are used only for the purpose of distinguishing one component from another. For example, without departing from the scope of the present invention, the first component may be referred to as a second component, and similarly, the second component may be referred to as a first component.

Terms such as top, bottom, top, bottom, or top, bottom, etc. are used to distinguish relative positions in components. For example, in the case of naming the upper part of the drawing as upper part and the lower part as lower part in the drawings for convenience, the upper part may be named lower part and the lower part may be named upper part without departing from the scope of right of the present invention .

The terminology used in this application is used only to describe a specific embodiment and is not intended to limit the invention. The singular expressions include plural expressions unless the context clearly dictates otherwise. In this application, the terms "comprises", "having", and the like are used to specify that a feature, a number, a step, an operation, an element, a part or a combination thereof is described in the specification, But do not preclude the presence or addition of one or more other features, integers, steps, operations, components, parts, or combinations thereof.

Unless otherwise defined, all terms used herein, including technical or scientific terms, have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. Terms such as those defined in commonly used dictionaries are to be interpreted as having a meaning consistent with the meaning in the context of the relevant art and are to be construed as ideal or overly formal in meaning unless explicitly defined in the present application Do not.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, preferred embodiments of the present invention will be described with reference to the drawings, but it should be understood that the present invention is not limited thereto and may be applied to various uses and purposes.

FIG. 1 is a cross-sectional view showing a structure of a string base precast module for an aviation light of the present invention, and FIG. 2 is an exploded sectional view showing the structure of a string base precast module for an aviation arc of the present invention.

FIG. 3 is a view showing a construction method using a line base precast module for aviation light of the present invention, and FIG. 4 is a process diagram showing a construction method using a line base precast module for aviation light of the present invention.

5 is a plan view showing the structure of a string base precast module for an aviation according to the present invention, FIG. 6A is a side sectional view of FIG. 5, and FIG. 6B is a plan view of FIG. 6A.

6C is an enlarged view showing a structure of a height adjusting unit of a string base precast module for an airlight according to the present invention.

1 to 6 are intended to clearly illustrate only the main feature parts in order to provide a conceptual and clear understanding of the invention, and as a result various variations of the illustrations are to be expected, and the scope of the invention is limited by the specific shapes shown in the figures There is no need.

1 and 6, first, a burr layer 102 made of lumps is formed on a bottom portion of the burr layer 102, and the burr layer 102 is formed on a bottom portion of the burr layer 102, An ascon layer 104 made of an ascon is formed.

A string based precast module 100 is installed at the center of the rubble layer 102 and the ascon layer 104.

The string based precast module 100 may be formed in a square or rectangular shape, and may be formed in a rectangular shape as shown in FIG. 5 in the embodiment of the present invention.

At this time, the string base precast module 100 is inserted with a height adjusting unit 114 so that height adjustment can be performed up and down.

The height adjusting unit 114 (as shown in FIG. 6C) is preferably fastened by an adjusting bolt having a threaded portion so as to be vertically adjustable.

An up-down iron hole 110 is formed at the center of the string-based pre-cast module 100. An air lighting lamp 112 is provided at an upper portion of the up-down iron hole 110, A module layer 107 is formed on the side of the module layer 107 and a hypersensitive portion 106 is formed on the outer side of the module layer 107.

The up-down iron hole 110 comprises a lower body 20 and an upper body 24 and a lower iron hole 109 corresponding to a lower portion of the up-down iron hole 110.

More specifically, the up-down iron hole 110 is formed of a cylindrical lower body 20 and an upper body 24 provided to correspond to the upper end of the lower body 20, And an adjusting bolt 29 is fastened and connected to the inner side of the body 110.

At this time, it is preferable that the up-down iron hole 110 is installed such that the upper body 24 moves up and down by rotating the adjustment bolt 28.

That is, the height of the up-down iron hole 110 can be adjusted by moving the upper body 24 up and down by rotating the adjusting bolt 28 connecting the lower body 20 and the upper body 24.

2, an abrasive layer 102 is formed on the bottom, and an ascon layer 104 is formed on the abscissa layer 102. As shown in FIG.

A module hole 10 is formed in the center of the rubble layer 102 and the ascon layer 104.

The ultra-high speed cement 106 is installed in the module hole 10 by injecting ultra fast cement.

The gyroscopic part 106 is composed of a hypobuscule bottom part 12 and a hypoglossal side part 14. That is, at the lower bottom portion of the module hole 10, ultra rapid cement is injected and the ultra low speed floor portion 12 is installed.

Speed side light cement is injected into the left and right side portions of the module hole 10 to form a fast transit side portion 14.

The module pre-cast module 108 is coupled to the module hole 10.

The base precast module 108 is comprised of a module layer 107 which is comprised of a rectangular module body 16 having a core hole 18 Is formed.

The module layer 107 is made of concrete.

The lower hole (109) and the up-down hole (110) are preferably inserted into the hole (18).

Preferably, a height adjusting unit 114 protrudes from a lower surface of the base precast module 108.

The height adjusting unit 114 may be installed on the inner side of the base precast module 108 to adjust the height of the base precast module 108 to be horizontal with the surface of the runway.

That is, it is for adjusting the height of the string-based precast module 100 located at the upper portion of the neck 102.

The upper metal hole 110 is inserted into the core hole 18 and the lower metal hole 109 is formed on the same center line so as to correspond to the up-down metal hole 110.

The lower iron hole 109 has a body 21 formed in a cylindrical shape and a conduit 117 penetrating right and left through the inner side.

The up-down iron hole 110 includes a lower body 20 and an upper body 24. The inner body of the lower body 20 is formed with a plurality of coupling portions 22 protruding inwardly And a plurality of fixing brackets 23 formed with screw holes are formed in the upper portion of the coupling portion 22 in the inward direction.

Preferably, the coupling portion 22 is formed so that a conduit is drawn in to facilitate coupling. The shape of the coupling portion 22 may be a cylindrical shape and a threaded portion may be formed on the inner side or two conduction pipes facing each other may be connected to each other.

The upper body 24 has a cylindrical shape and a plurality of fixing brackets 25 having screw holes are protruded from the inner side of the upper body 24. A lamp mounting portion 26 is formed inside the upper end of the body 24 have.

The lower body 20 and the upper body 24 of the up-down iron hole 110 are fastened by a plurality of height adjusting bolts 28 to be adjusted up and down.

The lower ends of the height adjusting bolts 28 are fastened to the fixing bracket 23 of the lower body 20 and the upper ends of the height adjusting bolts 28 are fastened to the fixing bracket 25 of the upper body 24, . That is, when the lower end of the height adjusting bolt 28 is fixed and rotated clockwise, the upper body 24 moves downward while the lower end is fixed, and the upper end of the height adjusting bolt 28 is fixed The lower body 20 is pulled upward to adjust the height.

The operation for adjusting the height is selectively performed according to the convenience of the user, and therefore, it is not described in detail.

A lamp mount 26 is installed inside the upper end of the up-down iron hole 110. The lamp mount 112 is inserted into the lamp mount 26.

As described above, the height of the lamp 112 installed in the up-down iron hole 110 can be adjusted by adjusting the height by moving the up-down iron hole 110 up and down, and it is possible to construct the lamp by aligning it with the road surface of the runway.

FIG. 3 is a view showing a construction method of a line base precast module according to the present invention. First, a line base precast module 100 is manufactured.

The string based precast module 100 may comprise one single module, preferably at least one module, and be connected to each other.

The string based precast module 100 firstly forms a base precast module 108 and installs an up-down steel hole 110 in the base precast module 108, and the base precast module 108 Diameter portion 106 is formed on the outer side of the neck portion 106. [

At this time, a module layer 107 is formed on the outer side of the base precast module 108.

A plurality of height adjusting units 114 are installed on the lower surface of the base precast module 108 so as to adjust the height.

The height adjustment unit 114 adjusts the height of the string-based precast module 100 to align the level with the road surface of the runway.

After the string based precast module 100 is manufactured as described above, the existing substructure 200 is cut to have the same size as that of the string pre-cast module 100, the substructure 200 is removed, 10).

The first speed ultra low speed cement is injected into the bottom of the module hole 10 to pour the ultra low speed floor 12.

The string-based precast module 100 manufactured in the module hole 10 in which the ultra low-speed ground bottom 12 is placed is inserted and installed.

Second speed cement is injected into the clearance between the string base precast module 100 and the module hole 10 to form a fast transit side portion 14.

After the string-based precast module 100 is inserted as described above, the luminaire 112 is inserted into the upper end of the up-down iron hole 110.

Next, FIG. 4 is a view showing a construction process using the line base precast module of the present invention. First, the line precast module 100 for aviation equilibrium is manufactured.

The existing foundation structure 200 is cut and demolished and then the crushed stone layer made of the abrasive layer 102 and the ascon layer 104 is uniformly polished.

The cement having the first speed is first laid on the lower floor at the portion where the foundation structure 200 is removed.

The string-based pre-cast module 100 is inserted into the upper portion of the string of the second string.

After the installation of the string based precast module 100, an existing conduit is connected

Then, second-order ultra low speed cement is injected into the outer side of the string-based precast module 100.

And the lamp 112 is installed on the upper part of the string-based precast module 100 constructed by injecting the second quick-speed cement.

At least one or more string-based precast modules 100 may be installed continuously in the fabrication of the string-based precast module 100 constructed as described above.

At this time, when the string based precast module 100 is installed continuously, the reinforcing bars and the roots can be connected to each other.

After the up-down iron hole 110 is installed, a cable can be installed and connected to the coupling portion 22 to connect or connect the cable to other equipment.

In addition, a stabilizer (not shown) can be installed after cable installation and connection.

5 and 6, a rectangular module body 10 is first formed, and at the center of the module body 10, up-down iron holes 110 And the first and second up-down iron holes 113 and 115 are inserted into the left and right sides of the center up-down iron hole 110, respectively.

A square grouting groove 11 is formed in the upper and lower portions of the center of the module body 10.

A conduit 117 is connected to the front and rear left and right portions of the up-down iron hole 110 and a conduit 117 is connected to the up-down iron hole 110 and the up-down iron holes 113 and 115.

A height adjusting unit hole 13 is formed on the upper left and lower portions of the up-down iron hole 113 and a height adjusting unit hole 13 is formed on the upper right and lower portions of the up-down iron hole 115.

The above-described height adjusting unit 114 is fitted in the height adjusting unit hole 13.

Fig. 6A is a sectional side view of Fig. 5, in which a rubble layer 102 is formed on the bottom portion, and a very low speed bottom portion 12 of the ultra-high speed portion 106 is formed on the ridge layer 102. Fig.

A module layer 107 is formed on an upper portion of the ultra low speed tread 12 and a plurality of up-down iron holes 110, 113 and 115 are inserted into the module layer 107. The up-down iron holes 110, And a luminaire 112 is inserted into the upper portion thereof.

In the up-down iron holes 110, 113, and 115, the conduits 117 are installed to be connected to each other in the horizontal direction.

A height adjusting unit 114 for adjusting the height of the string base precast module 100 is installed at the left side of the up-down iron hole 113.

A height adjusting unit 114 is inserted in the right side of the up-down iron hole 115.

The height adjustment unit 114 can be adjusted to the height of the string based precast module 100 by rotating the adjustable bolt 29 using a later-described adjustment bolt 29 as shown in FIG. 6C.

6B and 6C are enlarged views showing the structure of the height adjusting unit according to the present invention in which a very low speed ground bottom portion 12 is formed on the upper part of the rubble layer 102, A module layer 107 composed of a module body 10 is formed.

At least one height adjusting unit 114 is inserted into the module body 10.

The height adjusting unit 114 is preferably inserted into the height adjusting unit hole 13 formed in the module layer 107.

The tubular body 33 may be inserted into the height adjustment unit hole 13.

6C, the height adjusting unit 114 is inserted into the module body 10 in a longitudinal direction. The height adjusting unit 114 includes height adjusting bolts 29 installed in the vertical direction, 29 and a module fixture 116 sandwiched between the height adjusting bolts 29 and the module fixing fixture 116. [

The height adjusting unit 114 is inserted into the inner side of the tube 33.

The module fixture 116 is cylindrical and has a fixed plate body 32 formed to fit the height adjusting bolts 29 and an upper fixed plate 34 fixed parallel to the outer side of the fixed plate body 32, Lt; / RTI >

The upper fixing plate 34 is preferably fixed to the fixing plate body 32 and has a flat plate shape extending horizontally outwardly, and is fixedly inserted into the module body 10.

The module fixing member 116 may further include a cylindrical support pipe 33 at a lower end of the height adjusting bolt 29. In other words, the support pipe 33 can be inserted into the height adjusting bolt 29 and the lower end portion can be firmly reinforced.

An upper fixing member 36 is fixed to an upper end of the height adjusting bolt 29.

The upper fixing member 36 is fixed to the height adjusting bolt 29 by using a nut.

The height adjusting unit 114 is capable of adjusting the height of the string-based precast module 100 by rotating and fixing the rotary member 118 to the upper fixing member 36.

The rotary member 118 uses a conventional wrench 40 and a connection fixture 38.

The height adjusting unit 114 thus installed fixes and connects the rotating member 118 to the upper fixing member 36 and rotates the rotating member 118.

Since the height adjusting bolt 29 is fixed to the upper fixing member 36, the height adjusting bolt 29 is rotated by the rotating member 118.

When the height of the string base precast module 100 is to be reduced, the upper fixing member 36 is rotated by rotating the rotary member 118, and the height adjusting bolt (29) is rotated.

At this time, when the height adjusting bolt 29 is rotated clockwise, the lower fixing plate 30 fixed to the lower portion of the height adjusting bolt 29 is pulled and moved upward.

The height of the string-based precast module 100 is lowered because the lower fixing plate 30 is pulled and brought into close contact with the lower surface of the module body 10.

On the other hand, when the height of the string-based precast module 100 is increased, the height adjusting bolt 29 is rotated in the counterclockwise direction by connecting the rotating member 118 to the height adjusting bolt 29, And is moved downward.

At this time, the lower fixing plate 30 fixed to the lower portion of the height adjusting bolt 29 is moved downward to contact with the bottom portion 12 at the initial speed and pushing downward to generate a reaction force, 100) is heard and the height becomes higher.

It will be apparent to those skilled in the art that various modifications, substitutions and substitutions are possible, without departing from the scope and spirit of the invention as disclosed in the accompanying claims. will be.

Therefore, the embodiments disclosed in the present invention and the accompanying drawings are intended to illustrate and not to limit the technical spirit of the present invention, and the scope of the technical idea of the present invention is not limited by these embodiments and the accompanying drawings . The scope of protection of the present invention should be construed according to the following claims, and all technical ideas within the scope of equivalents should be construed as falling within the scope of the present invention.

10: Module hole 12: Ultra low speed floor
14: fast speed side portion 16: module body
18: Core hole 20: Lower body
24: upper body
22: coupling portion 23, 25: fixed bracket
26: luminaire mounting part 28,29: height adjusting bolt
30: lower fixed plate 32: fixed plate body
34: upper fixing plate 36: upper fixing member
38: connection fastener 40: wrench
100: line base precast module 102: miscellaneous layer
104: Ascon layer 106:
108: Foundation precast module 110: Up-down steel hole
112: luminaire 114: height adjustment unit
116: Module fixture 118: Rotating member

Claims (6)

In a string based precast module for an aviation light which is coupled to a module hole (10) passing through an upper ascon layer (104) and reaching a lower lumped layer (102)
A hypsoxial portion 106 formed on the inner side of the module hole 10;
A base precast module 108 inserted in the inside of the ultra-high speed part 106 and having a core hole 18 formed at the center thereof and a module body 16 having a height adjusting unit hole 13 formed therein;
An up-down iron hole 110 installed in the inner side of the core hole 18 to adjust the height thereof; And
And a height adjusting unit 114 inserted into the height adjusting unit hole 13 formed in the base precast module 108 so as to be raised and lowered and installed to protrude from the lower surface,
The height adjustment unit (114)
A height adjusting bolt 29 coupled to the height adjusting unit hole 13;
A module fixture (116) fixed to the module body (16) and fastened to the height adjustment bolt (29); And
A lower fixing plate 30 fixed to the lower end of the height adjusting bolt 29; / RTI >
The module fixture (116)
A cylindrical plate-shaped plate body 32; And
An upper fixing plate 34 fixed to the outer circumferential surface of the fixing plate body 32 in a horizontal direction; / RTI >
The up-down iron hole (110)
A cylindrical lower body 20;
A plurality of coupling portions 22 formed on the inner side of the lower body 20;
A plurality of fixing brackets (23) formed on an upper portion of the coupling portion;
A cylindrical upper body 24;
A plurality of fixing brackets 25 formed on the inner side of the upper body 24; And
A height adjusting bolt 28 installed by fastening the fixing bracket 23 and the fixing bracket 25 to adjust the height of the upper body 24 and the lower body 20; To
Wherein the prefabricated string prefabricated module for an airborne sole is characterized in that the prefabricated string prefabricated module comprises a plurality
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101833782B1 (en) * 2017-07-21 2018-02-28 (주)새한기술그룹 Taxiy Way Insert Airport Light Installation

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0464726B2 (en) * 1984-07-24 1992-10-15 Hitachi Ltd
US6113245A (en) * 1998-07-10 2000-09-05 Reinert, Sr.; Gary L. Airport runway light container apparatus and method
KR100406482B1 (en) 2001-07-04 2003-11-17 조용성 Precast concrete module for paving of road and method of paving road using the same
KR20060082832A (en) * 2006-06-15 2006-07-19 한국유지관리 주식회사 Precast concrete panel using height-controller and its road repairing method
KR100655768B1 (en) * 2006-01-18 2006-12-08 주식회사 우전그린 Lighting lane system of road

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0464726B2 (en) * 1984-07-24 1992-10-15 Hitachi Ltd
US6113245A (en) * 1998-07-10 2000-09-05 Reinert, Sr.; Gary L. Airport runway light container apparatus and method
KR100406482B1 (en) 2001-07-04 2003-11-17 조용성 Precast concrete module for paving of road and method of paving road using the same
KR100655768B1 (en) * 2006-01-18 2006-12-08 주식회사 우전그린 Lighting lane system of road
KR20060082832A (en) * 2006-06-15 2006-07-19 한국유지관리 주식회사 Precast concrete panel using height-controller and its road repairing method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101833782B1 (en) * 2017-07-21 2018-02-28 (주)새한기술그룹 Taxiy Way Insert Airport Light Installation

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