CN108060731A - Overhang big all-wing aircraft type unitized curtain wall system and its installation method - Google Patents

Overhang big all-wing aircraft type unitized curtain wall system and its installation method Download PDF

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Publication number
CN108060731A
CN108060731A CN201711145635.0A CN201711145635A CN108060731A CN 108060731 A CN108060731 A CN 108060731A CN 201711145635 A CN201711145635 A CN 201711145635A CN 108060731 A CN108060731 A CN 108060731A
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CN
China
Prior art keywords
tie
wing aircraft
crossbeam
fixed
aluminium sheet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
CN201711145635.0A
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Chinese (zh)
Inventor
付小兵
龚导
彭群
兰亦标
李锋
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Jangho Group Co Ltd
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Jangho Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jangho Group Co Ltd filed Critical Jangho Group Co Ltd
Priority to CN201711145635.0A priority Critical patent/CN108060731A/en
Publication of CN108060731A publication Critical patent/CN108060731A/en
Withdrawn legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/88Curtain walls
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/88Curtain walls
    • E04B2/96Curtain walls comprising panels attached to the structure through mullions or transoms
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/88Curtain walls
    • E04B2/96Curtain walls comprising panels attached to the structure through mullions or transoms
    • E04B2/965Connections of mullions and transoms

Abstract

A kind of to overhang big all-wing aircraft type unitized curtain wall system and its installation method, curtain wall system includes main body girder steel and all-wing aircraft unit;Main body girder steel lateral surface is equipped with several connecting corner yards;All-wing aircraft unit includes two all-wing aircraft crossbeams, and each all-wing aircraft crossbeam inner end is individually fixed on the inside of a connecting corner yard;All-wing aircraft crossbeam is fixedly connected with the first tie-beam, the second tie-beam, the 3rd tie-beam, the 4th tie-beam, the 5th tie-beam;The top and bottom of main body girder steel have been respectively fixedly connected with the 6th tie-beam and the 7th tie-beam;In same all-wing aircraft unit, the end between corresponding first tie-beam, the second tie-beam, the 3rd tie-beam, the 4th tie-beam, the 5th tie-beam, the 6th tie-beam, the 7th tie-beam is connected by support beam;The first aluminium sheet, the second aluminium sheet, the 3rd aluminium sheet, the 4th aluminium sheet, the 5th aluminium sheet, the 6th aluminium sheet are equipped with outside the all-wing aircraft unit.The present invention can reduce field installation procedure, greatly reduce installation cost, and the appearance of building can be effectively ensured.

Description

Overhang big all-wing aircraft type unitized curtain wall system and its installation method
Technical field
It is particularly a kind of to overhang big all-wing aircraft type unitized curtain wall system and its peace the invention belongs to external decoration curtain wall technology field Dress method.
Background technology
In the existing big all-wing aircraft type unitized curtain wall of overhanging, big all-wing aircraft part generally use tower structure system is overhang, Keel use aluminium alloy extrusions or steel part, and each scattered component uses factory process form, live peace is transported to after machining Dress.Such mode has the following disadvantages:
1st, the installation of each separate components of big all-wing aircraft such as bearing, keel and panel, sealing gluing etc. use in-site installation Mode, on-site construction processes are complicated, and are affected by construction quality, it is difficult to ensure architectural appearance effect;
2nd, the steel joist welding connecting mode that big all-wing aircraft used in the past is overhang, site welding process is more, and there are security against fires Hidden danger;
3rd, frame-generic formula structural system, construction speed is slower, and construction precision is difficult to control.
The content of the invention
The object of the present invention is to provide a kind of big all-wing aircraft type unitized curtain wall system of overhanging and its installation methods, use factory Change processing, reduce field installation procedure, improve construction and installation efficiency, greatly reduce installation cost, and can be effectively ensured and build The appearance built.
To achieve the above object, the present invention takes following technical scheme:
A kind of big all-wing aircraft type unitized curtain wall system of overhanging, if it include with the main body girder steel of the fixed level of building body and Dry all-wing aircraft unit;The main body girder steel lateral surface is fixed with the connecting corner yard of several L-types;The connecting corner yard, which has, to be mutually perpendicular to The first face and the second face, which is fixedly connected with the main body girder steel, which is equipped with horizontal adjusting slot hole;This flies Wing unit includes two all-wing aircraft crossbeams, and each all-wing aircraft crossbeam inner end is individually fixed on the inside of a connecting corner yard, and passes through the adjusting Adjusting bolt in slot hole is fixedly connected;The all-wing aircraft crossbeam is vertical with the subject beam and extends outwardly;In the middle part of the all-wing aircraft crossbeam Top and bottom be respectively fixedly connected with the first tie-beam and the second tie-beam, which is fixedly connected with the 3rd Tie-beam, the all-wing aircraft crossbeam inner end bottom surface are equipped with the 4th tie-beam, and the is equipped between the 4th tie-beam and second tie-beam Five tie-beams;The top and bottom of the main body girder steel have been respectively fixedly connected with the 6th tie-beam and the 7th tie-beam;Same all-wing aircraft In unit, corresponding first tie-beam, the second tie-beam, the 3rd tie-beam, the 4th tie-beam, the 5th tie-beam, the 6th connection End between beam, the 7th tie-beam is connected by support beam;
The first aluminium sheet is equipped between at the top of first tie-beam and the 6th tie-beam, first tie-beam and the 3rd connect It connects and the second aluminium sheet is equipped between back portion, the second aluminium sheet section is L-shaped;The is equipped between the top and bottom of 3rd crossbeam Three aluminium sheets;The 4th aluminium sheet is equipped between second tie-beam and the 3rd tie-beam bottom, the 4th aluminium sheet section is L-shaped;It should The 5th aluminium sheet is equipped between second tie-beam and the 5th tie-beam bottom;5th tie-beam and the 7th tie-beam bottom it Between be equipped with the 6th aluminium sheet.
Further, horizontal operating platform is equipped between the 4th tie-beam and the 3rd tie-beam bottom, it should Operating platform side is fixedly connected with the 5th tie-beam bottom.
Further, the outer end top surface of the all-wing aircraft crossbeam is fixed with the fixed corner code of L-type, adjacent all-wing aircraft unit It is fixed together between the vertical side of fixed corner code by the first fixed plate, the all-wing aircraft crossbeam of adjacent all-wing aircraft unit Inner end top surface is fixed together by the second fixed plate.
Further, the adjacent connecting corner yard bottom surface is equipped with horizontal support plate, and each support plate top surface is connected with this Corner brace is welded, and side is welded with the subject beam.
Further, the 6th aluminium sheet has the bending part of several L-types.
Further, the opening direction of two U-shaped and adjacent all-wing aircraft crossbeams of the section of the all-wing aircraft crossbeam it is consistent and It is horizontal.
Further, be welded and fixed on the inside of the 3rd tie-beam with a horizontal fixed beam, the fixed beam end and The all-wing aircraft crossbeam side is welded and fixed.
Further, it is fixedly connected between first face and the subject beam by connecting bolt, while passes through weldering It connects and is fixedly connected.
A kind of installation method of the big all-wing aircraft type unitized curtain wall system of overhanging, it comprises the following steps:
All-wing aircraft crossbeam and the first tie-beam, the second tie-beam, the 3rd tie-beam, the 4th tie-beam and the 5th tie-beam are existed Factory process simultaneously assembles integral, opens up mounting hole close to one end of the 4th tie-beam in the all-wing aircraft crossbeam, the other end, which opens up, to be hung Fill hole;It is fixedly connected by operating platform lateral arrangement, and with the 3rd crossbeam, the 4th crossbeam and the 5th crossbeam bottom;Installation is outer 3rd aluminium sheet of side, the 4th aluminium sheet and the 5th aluminium sheet of bottom, point and with the 3rd tie-beam, the second tie-beam and the 5th tie-beam It is fixed, then seal gluing;
Horizontal adjusting slot hole is opened up in the second face of connecting corner yard, and the first face and subject beam side are fixed, it will The all-wing aircraft crossbeam is fixed with connecting corner yard by adjusting bolt, and is tightened after front and rear adjusting in place, then by all-wing aircraft crossbeam and company Connect corner brace reinforcement of weld, the adjacent all-wing aircraft sequence of unit installation in left and right;
The first fixed plate and the second fixed plate are connected as one between the all-wing aircraft crossbeam of adjacent all-wing aircraft unit;6th is connected It connects beam and the 7th tie-beam is fixed with subject beam, the 6th aluminium sheet of bottom is installed, and pass through operating platform installation top the One aluminium sheet and the second aluminium sheet, then seal gluing.
Further, in the factory, using assembly platform of the moulding bed as all-wing aircraft unit, which includes two assemblings Frame, two assembling frame bottoms are fixedly connected by cross bar;Interlayer floor is simulated using moulding bed, moulding bed is fixed on chemical anchor bolts Steel structure assembling is carried out in place;
Then, the assembly of all-wing aircraft unit is carried out on moulding bed:Screw rod is used first by the root of the all-wing aircraft crossbeam of all-wing aircraft unit Portion fastens, and is fixed on the assembling frame, the other end is sling using steel wire rope makes its smooth;Then the first tie-beam, second are carried out The installation of tie-beam, the 3rd tie-beam, the 4th tie-beam, the 5th tie-beam carries out the 3rd aluminium sheet, the bottom in outside after being completed 4th aluminium sheet in portion and the installation of the 5th aluminium sheet;
All-wing aircraft unit is after the completion of factory-assembled, and using moulding bed as transport shelf, moulding bed is covered with protectiveness flexible material, All-wing aircraft unit is made to be contacted with the protection flexible material of moulding bed;
After showing up, all-wing aircraft unit carries out handling using tower crane, and suspension centre is per 8 liftings laid in Pin all-wing aircraft beam surfaces Ear;All-wing aircraft crossbeam will be sling using tower crane, be lifted by crane again after being adjusted according to angle when installing in place first;It is lifted to During position to be installed, tower crane large arm slowly recycles again, makes all-wing aircraft unit gradually close to structural edge;Treat that all-wing aircraft unit plate is close During structural edge, company that construction personnel will be in advance welded on the all-wing aircraft crossbeam of all-wing aircraft unit and main body girder steel by haulage tail rope It connects corner brace to be attached by screw, and carries out full weld in all-wing aircraft crossbeam root and fix, complete the installation of all-wing aircraft unit.
The beneficial effects of the invention are as follows:The present invention, which overhangs big all-wing aircraft curtain wall unit system, is not influencing curtain wall system and building Site operation installation procedure is considerably reduced on the premise of main body connective stability, and greatly reduce construction and installation synthesis into This, while the precision of construction and installation is improved, the appearance of elevation of building is effectively ensured.
Description of the drawings
Fig. 1 is the structure diagram that the present invention overhangs big all-wing aircraft type unitized curtain wall system.
Fig. 2 is the schematic cross-sectional view in A-A directions in Fig. 1.
Fig. 3 is the schematic cross-sectional view in B-B directions in Fig. 1.
Fig. 4 is the structure diagram for the moulding bed that the present invention overhangs big all-wing aircraft type unitized curtain wall system.
Fig. 5 is the assembling schematic diagram for the all-wing aircraft unit that the present invention overhangs big all-wing aircraft type unitized curtain wall system.
Specific embodiment
In order to absolutely prove the technological means and creation characteristic of realizing the present invention, With reference to embodiment, into one Step illustrates the present invention.
As shown in Figure 1-Figure 3, the present invention provides a kind of big all-wing aircraft type unitized curtain wall system of overhanging, it includes and building body The main body girder steel 1 of fixed level and several all-wing aircraft units.1 lateral surface of main body girder steel is fixed with the connection of several L-types Corner brace 11.The connecting corner yard 11 has orthogonal first face, 111 and second face 112, first face 111 and the main body girder steel 1 is fixedly connected, which is equipped with horizontal adjusting slot hole 113.Pass through company between first face 111 and the subject beam 1 Connecting bolt 114 is fixedly connected, and is fixedly connected by welding simultaneously, to increase structural strength.Adjacent 11 bottom surface of connecting corner yard Equipped with horizontal support plate 12, each 12 top surface of support plate is welded with the connecting corner yard 11, and side is welded with the subject beam 1.
The all-wing aircraft unit includes two all-wing aircraft crossbeams 2, and the section of the all-wing aircraft crossbeam 2 is U-shaped, and adjacent two all-wing aircraft horizontal strokes The opening direction of beam 2 is consistent and horizontal.Each 2 inner end of all-wing aircraft crossbeam is individually fixed in 11 inside of connecting corner yard, and passes through this The adjusting bolt 115 adjusted in slot hole 113 is fixedly connected.The all-wing aircraft crossbeam 2 is vertical with the subject beam 1 and extends outwardly.It should The top and bottom at 2 middle part of all-wing aircraft crossbeam have been respectively fixedly connected with the first tie-beam 21 and the second tie-beam 22, the all-wing aircraft crossbeam 2 Outer end is fixedly connected with the 3rd tie-beam 23, which is equipped with the 4th tie-beam 24, the 4th tie-beam 24 The 5th tie-beam 25 is equipped between second tie-beam 22.The top and bottom of the main body girder steel 1 have been respectively fixedly connected with Six tie-beams 26 and the 7th tie-beam 27.In same all-wing aircraft unit, corresponding first tie-beam 21, the second tie-beam the 22, the 3rd End between tie-beam 23, the 4th tie-beam 24, the 5th tie-beam 25, the 6th tie-beam 26, the 7th tie-beam 27 passes through branch Support crossbeam 28 connects.The inside of 3rd tie-beam 23 is welded and fixed with a horizontal fixed beam 29,29 end of fixed beam and 2 side of all-wing aircraft crossbeam is welded and fixed.
First tie-beam 21 and the 6th tie-beam are equipped with the first aluminium sheet 3,21 He of the first tie-beam between 26 top 3rd tie-beam is equipped with the second aluminium sheet 4 between 23 top, and 4 section of the second aluminium sheet is L-shaped.The top of 3rd crossbeam 23 and The 3rd aluminium sheet 5 is equipped between bottom.The 4th aluminium sheet 6 is equipped between 23 bottom of second tie-beam 22 and the 3rd tie-beam, it should 4th aluminium sheet, 6 section is L-shaped.The 5th aluminium sheet 7 is equipped between 25 bottom of second tie-beam 22 and the 5th tie-beam.5th The 6th aluminium sheet 8 is equipped between 27 bottom of tie-beam 25 and the 7th tie-beam, the 6th aluminium sheet 8 has the bending part of several L-types.
For the ease of installation, horizontal operating platform is equipped between the 4th tie-beam 24 and 23 bottom of the 3rd tie-beam 9, which is fixedly connected with 25 bottom of the 5th tie-beam.
The outer end top surface of the all-wing aircraft crossbeam 2 is fixed with the fixed corner code 20 of L-type, is installed in adjacent all-wing aircraft unit Afterwards, it is fixed together between the vertical side of the fixed corner code 20 of adjacent all-wing aircraft unit by the first fixed plate 201, phase The inner end top surface of the all-wing aircraft crossbeam 2 of adjacent all-wing aircraft unit is fixed together by the second fixed plate 202, strong to improve structure Degree.
The present invention also provides a kind of installation methods of the above-mentioned big all-wing aircraft type unitized curtain wall system of overhanging, it includes following step Suddenly:
By 2 and first tie-beam 21 of all-wing aircraft crossbeam, the second tie-beam 22, the 3rd tie-beam 23, the 4th tie-beam 24 and Five tie-beams 25 are in factory process and assemble integral, and installation is opened up close to one end of the 4th tie-beam 24 in the all-wing aircraft crossbeam 2 Hole, the other end open up hole for hoist;By 9 lateral arrangement of operating platform, and with the 3rd crossbeam 23, the 4th crossbeam 24 and the 5th crossbeam 25 bottoms are fixedly connected;3rd aluminium sheet 5, the 4th aluminium sheet 6 and the 5th aluminium sheet 7 of bottom in outside are installed, divides and is connected with the 3rd Beam 23, the second tie-beam 22 and the 5th tie-beam 25 are fixed, then seal gluing;
Open up horizontal adjusting slot hole 113 in the second face 112 of connecting corner yard 11, and by the first face 111 and subject beam 1 Side is fixed, which is fixed with connecting corner yard 11 by adjusting bolt 115, and is tightened after front and rear adjusting in place, so Afterwards by 11 reinforcement of weld of all-wing aircraft crossbeam 2 and connecting corner yard, the adjacent all-wing aircraft sequence of unit installation in left and right;
The first fixed plate 201 and the second fixed plate 202 are connected as one between the all-wing aircraft crossbeam 2 of adjacent all-wing aircraft unit; 6th tie-beam 26 and the 7th tie-beam 27 with subject beam 1 are fixed, the 6th aluminium sheet 8 of bottom is installed, and it is flat to pass through operation First aluminium sheet 3 and the second aluminium sheet 4 at the installation of platform 9 top, then seal gluing.
Wherein, in the factory, using assembly platform of the moulding bed 10 as all-wing aircraft unit, as shown in Figure 4, Figure 5, the moulding bed 10 Including two assembling framves 101, each group shelves 4.7 meters of 101 length, 2.4 meters high, and two 101 bottoms of assembling frame are fixed by cross bar 102 Connection;Interlayer floor is simulated using moulding bed 10, moulding bed 10 with chemical anchor bolts is fixed and carries out steel structure assembling in the venue.
The assembly of all-wing aircraft unit is carried out on moulding bed 10;Bullet puts three horizontal linemarks first on moulding bed 10, pushes up the bottom line of ink marker Steelframe top bottom size is controlled, the intermediate line of ink marker controls 11 height of connecting corner yard, makes whole product all-wing aircraft absolute altitude disengaging unified.Make first The root of the all-wing aircraft crossbeam 2 of all-wing aircraft unit is fastened with screw rod, after being adjusted to absolute altitude, is fixed on the assembling frame 101, the other end Being sling using steel wire rope 103 makes its smooth.Then steel wire rope the first tie-beam 21, second of progress set according to the line of ink marker and drawing in advance The installation of tie-beam 22, the 3rd tie-beam 23, the 4th tie-beam 24, the 5th tie-beam 25, according to line of ink marker bullet after being completed The lattice size gone out controls net as aluminium sheet lattice, carries out the 3rd aluminium sheet 5, the 4th aluminium sheet 6 and the 5th aluminium sheet 7 of bottom in outside Installation.
All-wing aircraft unit is after the completion of factory-assembled, and using moulding bed 10 as transport shelf, moulding bed 10 is covered with protectiveness flexibility Material makes all-wing aircraft unit be contacted with the protection flexible material of moulding bed 10, damaged to prevent all-wing aircraft unit.During transport, per Pin all-wing aircraft lists Member is on respective moulding bed 10, and number entrucking in sequence, transports to scene;To prevent all-wing aircraft element deformation, fly in transport Wing unit keeps flat, and forbids standing up.
It after showing up, is unloaded as far as possible using fork truck, crane, avoids repeatedly carrying the damage for causing all-wing aircraft unit.
All-wing aircraft unit plate carries out handling using tower crane, and suspension centre is per 8 liftings laid on 2 surface of Pin all-wing aircrafts crossbeam Ear.All-wing aircraft crossbeam 2 will be sling using tower crane, be lifted by crane again after being adjusted according to angle when installing in place first.In addition, With a distance from structural edge it is 20~30 meters when all-wing aircraft lifts by crane to avoid high wind.
When being lifted to position to be installed, tower crane large arm slowly recycles again, makes all-wing aircraft unit gradually close to structural edge.It waits to fly When wing unit plate is close to structural edge, construction personnel is by haulage tail rope by the 2 grafting position of all-wing aircraft crossbeam of all-wing aircraft unit and master The connecting corner yard 11 being welded in advance on body girder steel 1 is attached by screw, and is carried out full weld in 2 root of all-wing aircraft crossbeam and consolidated It is fixed, complete the installation of all-wing aircraft unit.
The present invention is overhang the big modular tectonic sieving of all-wing aircraft system, is had using main panel of the aluminum veneer as overhanging all-wing aircraft Effect solves the deficiency on existing overhanging all-wing aircraft Curtain Wall Design.The present invention overhangs big all-wing aircraft and uses main steel (or aluminium alloy) skeleton and portion Subpanel reduces field installation procedure into tectonic sieving modular Pin, processing factory, improves construction and installation efficiency, significantly Reduce the installation synthesis cost for overhanging big all-wing aircraft curtain wall, remarkable in economical benefits.Unit plate is mainly using bolt form with building It builds main body to fix, and uses the adjustable design of error, site safety risk is reduced while curtain wall installation accuracy is improved, effectively It ensure that the appearance of building.
There is no the technical characteristic being described in detail in the present invention for the prior art, above are only and illustrate the principle of the present invention, have Body embodiment is present pre-ferred embodiments, not for limitation the application.It is all in the technical field of the invention It, should be by the application's without departing from spirit disclosed herein and all equivalent modifications completed under technological thought or change Claim is covered.

Claims (10)

1. a kind of big all-wing aircraft type unitized curtain wall system of overhanging, which is characterized in that it includes the master with the fixed level of building body Body girder steel and several all-wing aircraft units;The main body girder steel lateral surface is fixed with the connecting corner yard of several L-types;The connecting corner yard has There are orthogonal first face and the second face, which is fixedly connected with the main body girder steel, which is equipped with horizontal tune Save slot hole;The all-wing aircraft unit includes two all-wing aircraft crossbeams, and each all-wing aircraft crossbeam inner end is individually fixed on the inside of a connecting corner yard, and It is fixedly connected by the adjusting bolt in the adjusting slot hole;The all-wing aircraft crossbeam is vertical with the subject beam and extends outwardly;This flies Top and bottom in the middle part of wing crossbeam have been respectively fixedly connected with the first tie-beam and the second tie-beam, which fixes The 3rd tie-beam is connected with, which is equipped with the 4th tie-beam, the 4th tie-beam and second tie-beam Between be equipped with the 5th tie-beam;The top and bottom of the main body girder steel have been respectively fixedly connected with the 6th tie-beam and the 7th connection Beam;In same all-wing aircraft unit, corresponding first tie-beam, the second tie-beam, the 3rd tie-beam, the 4th tie-beam, the 5th connection End between beam, the 6th tie-beam, the 7th tie-beam is connected by support beam;
The first aluminium sheet, first tie-beam and the 3rd tie-beam are equipped between at the top of first tie-beam and the 6th tie-beam The second aluminium sheet is equipped between top, the second aluminium sheet section is L-shaped;The 3rd aluminium is equipped between the top and bottom of 3rd crossbeam Plate;The 4th aluminium sheet is equipped between second tie-beam and the 3rd tie-beam bottom, the 4th aluminium sheet section is L-shaped;This second The 5th aluminium sheet is equipped between tie-beam and the 5th tie-beam bottom;It is set between 5th tie-beam and the 7th tie-beam bottom There is the 6th aluminium sheet.
2. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 1, it is characterised in that:4th tie-beam with Horizontal operating platform is equipped between the 3rd tie-beam bottom, which consolidates with the 5th tie-beam bottom Fixed connection.
3. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 1 or 2, it is characterised in that:The all-wing aircraft crossbeam Outer end top surface be fixed with the fixed corner code of L-type, pass through between the vertical side of the fixed corner code of adjacent all-wing aircraft unit One fixed plate is fixed together, and the inner end top surface of the all-wing aircraft crossbeam of adjacent all-wing aircraft unit is fixed by the second fixed plate to be connected It is connected together.
4. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 3, it is characterised in that:The adjacent joint angle Code bottom surface is equipped with horizontal support plate, and each support plate top surface is welded with the connecting corner yard, and side is welded with the subject beam.
5. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 1 or 2, it is characterised in that:6th aluminium sheet Bending part with several L-types.
6. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 1 or 2, it is characterised in that:The all-wing aircraft crossbeam The U-shaped and adjacent two all-wing aircraft crossbeams in section opening direction it is consistent and horizontal.
7. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 1 or 2, it is characterised in that:3rd connection It is welded and fixed on the inside of beam with a horizontal fixed beam, which is welded and fixed with the all-wing aircraft crossbeam side.
8. the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 1 or 2, it is characterised in that:First face with It is fixedly connected by connecting bolt between the subject beam, is fixedly connected by welding simultaneously.
It is 9. a kind of such as the installation method of the big all-wing aircraft type unitized curtain wall system of overhanging described in any item of the claim 1 to 8, spy Sign is that it comprises the following steps:
By all-wing aircraft crossbeam and the first tie-beam, the second tie-beam, the 3rd tie-beam, the 4th tie-beam and the 5th tie-beam in factory It processes and assembles integral, open up mounting hole close to one end of the 4th tie-beam in the all-wing aircraft crossbeam, the other end opens up hole for hoist; It is fixedly connected by operating platform lateral arrangement, and with the 3rd crossbeam, the 4th crossbeam and the 5th crossbeam bottom;The of installation outside Three aluminium sheets, the 4th aluminium sheet and the 5th aluminium sheet of bottom divide and are fixed with the 3rd tie-beam, the second tie-beam and the 5th tie-beam, Gluing is sealed again;
Horizontal adjusting slot hole is opened up in the second face of connecting corner yard, and the first face and subject beam side are fixed, this is flown Wing crossbeam is fixed with connecting corner yard by adjusting bolt, and is tightened after front and rear adjusting in place, then by all-wing aircraft crossbeam and joint angle Code reinforcement of weld, the adjacent all-wing aircraft sequence of unit installation in left and right;
The first fixed plate and the second fixed plate are connected as one between the all-wing aircraft crossbeam of adjacent all-wing aircraft unit;By the 6th tie-beam It is fixed with the 7th tie-beam with subject beam, the 6th aluminium sheet of bottom is installed, and passes through first aluminium at operating platform installation top Plate and the second aluminium sheet, then seal gluing.
10. the installation method of the big all-wing aircraft type unitized curtain wall system of overhanging according to claim 9, which is characterized in that in work In factory, using assembly platform of the moulding bed as all-wing aircraft unit, which includes two assembling framves, and two assembling frame bottoms pass through horizontal stroke Bar is fixedly connected;Interlayer floor is simulated using moulding bed, moulding bed with chemical anchor bolts is fixed and carries out steel structure assembling in the venue;
Then, the assembly of all-wing aircraft unit is carried out on moulding bed:The root of the all-wing aircraft crossbeam of all-wing aircraft unit is fastened using screw rod first Tightly, it is fixed on the assembling frame, the other end is sling using steel wire rope makes its smooth;Then the first tie-beam, the second connection are carried out The installation of beam, the 3rd tie-beam, the 4th tie-beam, the 5th tie-beam carries out the 3rd aluminium sheet, the bottom in outside after being completed The installation of 4th aluminium sheet and the 5th aluminium sheet;
All-wing aircraft unit is after the completion of factory-assembled, and using moulding bed as transport shelf, moulding bed is covered with protectiveness flexible material, makes to fly Wing unit is contacted with the protection flexible material of moulding bed;
After showing up, all-wing aircraft unit carries out handling using tower crane, and suspension centre is per the 8 lifting ears laid in Pin all-wing aircraft beam surfaces; All-wing aircraft crossbeam will be sling using tower crane, be lifted by crane again after being adjusted according to angle when installing in place first;It is lifted to and treats During installation site, tower crane large arm slowly recycles again, makes all-wing aircraft unit gradually close to structural edge;Treat all-wing aircraft unit plate close to knot During structure edge, connection that construction personnel will be in advance welded on the all-wing aircraft crossbeam of all-wing aircraft unit and main body girder steel by haulage tail rope Corner brace is attached by screw, and is carried out full weld in all-wing aircraft crossbeam root and fixed, and completes the installation of all-wing aircraft unit.
CN201711145635.0A 2017-11-17 2017-11-17 Overhang big all-wing aircraft type unitized curtain wall system and its installation method Withdrawn CN108060731A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112942795A (en) * 2021-02-04 2021-06-11 广东世纪达建设集团有限公司 Flying wing curtain wall and roof steel structure decoration line construction method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002235396A (en) * 2001-02-07 2002-08-23 Sekisui House Ltd Vertical wall panel mounting structure
CN202767300U (en) * 2012-06-21 2013-03-06 湖北弘毅建筑装饰工程有限公司 Large cantilever multi-way adjustment changeover piece for panel wall
CN203716290U (en) * 2013-08-09 2014-07-16 江苏誉盛铂特建材科技有限公司 Sunshine room
KR20160116274A (en) * 2015-03-27 2016-10-07 (주)엔아이스틸 Wing Wall With Integrated Structural
CN106968371A (en) * 2017-03-20 2017-07-21 广州珠江工程建设监理有限公司 A kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002235396A (en) * 2001-02-07 2002-08-23 Sekisui House Ltd Vertical wall panel mounting structure
CN202767300U (en) * 2012-06-21 2013-03-06 湖北弘毅建筑装饰工程有限公司 Large cantilever multi-way adjustment changeover piece for panel wall
CN203716290U (en) * 2013-08-09 2014-07-16 江苏誉盛铂特建材科技有限公司 Sunshine room
KR20160116274A (en) * 2015-03-27 2016-10-07 (주)엔아이스틸 Wing Wall With Integrated Structural
CN106968371A (en) * 2017-03-20 2017-07-21 广州珠江工程建设监理有限公司 A kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112942795A (en) * 2021-02-04 2021-06-11 广东世纪达建设集团有限公司 Flying wing curtain wall and roof steel structure decoration line construction method

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Application publication date: 20180522