CN106968371B - A kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction - Google Patents

A kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction Download PDF

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Publication number
CN106968371B
CN106968371B CN201710167360.4A CN201710167360A CN106968371B CN 106968371 B CN106968371 B CN 106968371B CN 201710167360 A CN201710167360 A CN 201710167360A CN 106968371 B CN106968371 B CN 106968371B
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steel
wing
construction
curtain wall
wing aircraft
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CN106968371A (en
Inventor
刘昭民
严飞虎
盖曙辉
张志勇
王咸帅
胡勃
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Guangzhou Pearl River Construction Supervision Co Ltd
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Guangzhou Pearl River Construction Supervision Co Ltd
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    • 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

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Load-Bearing And Curtain Walls (AREA)

Abstract

The invention discloses a kind of construction methods of the high wing articulated structure drifted by wind of curtain wall construction, the high wing articulated structure drifted by wind of curtain wall construction includes all-wing aircraft glass and connector, connector is steel construction, and one end is used to connect the aluminium alloy glass slot of all-wing aircraft glass, and cushion block is arranged in all-wing aircraft glass both sides.Only by setting up the overhanging about 1m in part, the wing that floatd greatly by curtain wall, large cantilever Deepen Design and live institute execution conditions are combined closely, and are constructed and are met curtain wall construction design requirement, while accelerating construction speed, achieve significant economic benefit and social benefit.

Description

A kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction
Technical field
The present invention relates to building curtain wall design and construction techniques, especially there is the curtain wall of big all-wing aircraft and large cantilever modeling structure The construction method of the high wing articulated structure drifted by wind of the combination of high wing articulated structure and construction technology drifted by wind, specially curtain wall construction.
Background technology
It is curtain wall construction, elevation of building big the float wing, large cantilever because moulding needs, in construction in skyscraper external decoration Full hall scaffold operating platform, which can not be set up, only can set up local scaffold operating platform, if do not floatd greatly the wing, big outstanding in curtain wall The Deepen Design stage chosen is combined with site operation actual conditions, and the later stage will appear constructional difficulties during practice of construction, The case where operating expenses is substantially increased or can not construct at all causes prodigious influence to the coordination of engineering master control construction speed.
Invention content
To solve the above-mentioned problems, the high wing merogenesis drifted by wind of curtain wall construction of the invention and construction method, are to be directed to curtain wall knot The high wing drifted by wind of structure is carried out because that can not set up full hall foot hand operating platform but can set up builder's jack operating platform.
A kind of high wing articulated structure drifted by wind of curtain wall construction, including all-wing aircraft glass and connector, connector are steel construction, one end Cushion block is arranged in aluminium alloy glass slot for connecting all-wing aircraft glass, all-wing aircraft glass both sides, and girder steel is arranged in the other end, and girder steel is setting Reeded section steel beam is provided with convex built-in fitting in the installation place of the wing that floats greatly, large cantilever and vertical structure root, and the convex is pre- The section steel beam of embedded part and groove is in mating connection, and the section steel beam of the groove is provided with bolt hole, and is bolted connection Convex built-in fitting.
In addition, a kind of construction method of curtain wall construction height wing merogenesis drifted by wind is:
Step 1), the scaffold operating platform for setting up overhanging about 1m, at concrete structure conversion steel construction overhanging 0.5m Merogenesis, remaining cantilever part are connect without plate pattern with steel structure bolt using the hanging list of back cover;
It is 50mm that can freely adjust surplus when step 2), steel structure bolt connection;
Step 3) installs convex built-in fitting in the big wing that floats, large cantilever and vertical structure root, by the way that steel side is logical or I-steel Stretch out to be connected with the steel side of the wing that floats greatly, large cantilever parallel direction is logical or I-steel is formed groove and connect, using welding or Bolted mode, total to overhang size no more than partial operation body panel, the wing, large cantilever are floatd greatly in remaining overhanging part can piecemeal The unit plate of bottom panel is housed for different sizes;
Step 4) is docked by tower crane or other lifting modes with crossbeam, is adopted in welded or bolted way;
Wherein, handling process is:Box cell cube is directly lifted using tower crane;Box all-wing aircraft cell cube is in rack over-assemble Tower crane puts rope connection lifting ear plate after the completion, chooses four angle position otic placodes of arm and pulls calabash using 16 diameter steel cord lifting ropes connection 2T Reed chooses two otic placode sling points in arm and makees all-wing aircraft protection lifting rope using 20 diameter steel cords, and tower crane directly lifts, all-wing aircraft turnover area Domain, installation on-station position respectively arrange a tower crane commander;Tower crane, which is hoisted to above installation region, to be stopped, and has been drawn traction rope, has been drawn Position is arranged above box all-wing aircraft floor, tower crane and is fixed temporarily on steel part draws close to steel construction at a slow speed.
Using above-mentioned technical proposal, the beneficial effects of the invention are as follows:
Only by setting up the overhanging about 1m in part, the wing that floats greatly by curtain wall, large cantilever Deepen Design and live institute execution conditions It combines closely, construction meets curtain wall construction design requirement, while accelerating construction speed, achieves significant economic benefit and society It can benefit.
Meanwhile gap requires between meeting the plate of Curtain Wall Design, reduces the generation to rigid concrete strong constraint stress, The generation of steel construction and concrete column structure crack is prevented, concrete overhanging curtain wall construction is solved and is not required to set up full hall crosshead The problem of, make arrangement and method for construction and curtain wall construction Deepen Design perfect adaptation.
Description of the drawings
The attached drawing for constituting the part of the present invention is used to provide further understanding of the present invention, schematic reality of the invention Example and its explanation are applied for explaining the present invention, is not constituted improper limitations of the present invention.In the accompanying drawings:
Fig. 1 is the wing glass articulated structure schematic diagram that floats of the present invention
Fig. 2 is the lifting operation chart of the present invention
Fig. 3 is floor all-wing aircraft merogenesis lifting schematic diagram
Fig. 4 is roof all-wing aircraft merogenesis lifting schematic diagram
Specific implementation mode
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the present invention can phase Mutually combination.The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
It elaborates below in conjunction with the accompanying drawings to the embodiment of the present invention.
A kind of high wing articulated structure drifted by wind of curtain wall construction, including all-wing aircraft glass 1 and connector 2, connector are steel construction, one Hold the aluminium alloy glass slot 3 for connecting all-wing aircraft glass, all-wing aircraft glass both sides that cushion block is set, shaped steel with groove is arranged in the other end Beam 4 is provided with convex built-in fitting 5, the convex built-in fitting and groove in the installation place of the wing that floats greatly, large cantilever and vertical structure root Section steel beam it is in mating connection, the section steel beam of the groove is provided with bolt hole, and is bolted connection convex built-in fitting.
In addition, a kind of construction method of curtain wall construction height wing merogenesis drifted by wind is:
Step 1), the scaffold operating platform for setting up overhanging about 1m, at concrete structure conversion steel construction overhanging 0.5m Merogenesis, remaining cantilever part are connect without plate pattern with steel structure bolt using the hanging list of back cover;
It is 50mm that can freely adjust surplus when step 2), steel structure bolt connection;
Step 3) installs convex built-in fitting in the big wing that floats, large cantilever and vertical structure root, by the way that steel side is logical or I-steel Stretch out to be connected with the steel side of the wing that floats greatly, large cantilever parallel direction is logical or I-steel is formed groove and connect, using welding or Bolted mode, total to overhang size no more than partial operation body panel, the wing, large cantilever are floatd greatly in remaining overhanging part can piecemeal The unit plate of bottom panel is housed for different sizes;
Step 4) is docked by tower crane or other lifting modes with crossbeam, is adopted in welded or bolted way;
Wherein, handling process is:Box cell cube is directly lifted using tower crane;Box all-wing aircraft cell cube is in rack over-assemble Tower crane puts 6 connection lifting ear plate 10 of rope after the completion, chooses four angle position otic placodes of arm and is pulled using 16 diameter steel cord lifting ropes 7 connection 2T Cucurbit 8 chooses two otic placode sling points in arm and makees all-wing aircraft protection lifting rope 9 using 20 diameter steel cords, and tower crane directly lifts, all-wing aircraft week Turn region, installation on-station position respectively arranges a tower crane commander;Tower crane, which is hoisted to above installation region, to be stopped, and traction rope has been drawn, Distracted position is arranged above box all-wing aircraft floor, tower crane and is fixed temporarily on steel part draws close to steel construction at a slow speed.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.

Claims (1)

1. a kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction, the high wing articulated structure drifted by wind of curtain wall construction includes all-wing aircraft Glass and connector, connector are steel construction, and one end is used to connect the aluminium alloy glass slot of all-wing aircraft glass, and all-wing aircraft glass both sides are set Cushion block is set, girder steel is arranged in the other end, and girder steel is that reeded section steel beam is arranged, in big the float wing, large cantilever and vertical structure root Installation place be provided with convex built-in fitting, the section steel beam of the convex built-in fitting and groove is in mating connection, the shaped steel of the groove Beam is provided with bolt hole, and is bolted connection convex built-in fitting;
It is characterized by comprising the following steps:
Step 1), the scaffold operating platform for setting up overhanging about 1m are saved in concrete structure conversion steel construction overhanging 0.5m punishment, Remaining cantilever part is connect using the hanging unit plate pattern of back cover with steel structure bolt;
It is 50mm that can freely adjust surplus when step 2), steel structure bolt connection;
Step 3) installs convex built-in fitting in the big wing that floats, large cantilever and vertical structure root, is led to by steel side or I-steel stretches out It is connected with the steel side of the wing that floats greatly, large cantilever parallel direction is logical or I-steel is formed groove, using welding or be bolted Mode, it is total to overhang size and be not more than partial operation body panel, remaining overhanging part float greatly the wing, large cantilever can piecemeal be different rulers The very little unit plate equipped with bottom panel;
Step 4) is docked by way of tower crane lifting with crossbeam, is adopted in welded or bolted way;
Wherein, handling process is:Box cell cube is directly lifted using tower crane;Box all-wing aircraft cell cube is completed in rack over-assemble Tower crane puts rope connection lifting ear plate afterwards, chooses four angle position otic placodes of arm and connects 2T chain blocks using 16 diameter steel cord lifting ropes, chooses Two otic placode sling points make all-wing aircraft protection lifting rope using 20 diameter steel cords in arm, and tower crane directly lifts, and all-wing aircraft has enough to meet the need region, peace It fills on-station position and respectively arranges a tower crane commander;Tower crane, which is hoisted to above installation region, to be stopped, and traction rope, distracted position has been drawn to set The floor above box all-wing aircraft is set, tower crane is fixed temporarily on steel part to steel construction draws close at a slow speed.
CN201710167360.4A 2017-03-20 2017-03-20 A kind of construction method of the high wing articulated structure drifted by wind of curtain wall construction Active CN106968371B (en)

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108060731A (en) * 2017-11-17 2018-05-22 江河创建集团股份有限公司 Overhang big all-wing aircraft type unitized curtain wall system and its installation method
CN112942795B (en) * 2021-02-04 2022-01-04 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 (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009215781A (en) * 2008-03-11 2009-09-24 Shin Nikkei Co Ltd Curtain wall structure
CN102619340A (en) * 2011-03-08 2012-08-01 青光绪 Mounting method for unitary glass curtain wall
CN204212294U (en) * 2014-10-14 2015-03-18 中建三局装饰有限公司 The modular self-supporting flying-wing device of a kind of Super High
CN205242770U (en) * 2015-12-24 2016-05-18 广州江河幕墙系统工程有限公司 Buckle formula glass wing device and in fixed all -wing aircraft glass's aluminum alloy glass cell body thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009215781A (en) * 2008-03-11 2009-09-24 Shin Nikkei Co Ltd Curtain wall structure
CN102619340A (en) * 2011-03-08 2012-08-01 青光绪 Mounting method for unitary glass curtain wall
CN204212294U (en) * 2014-10-14 2015-03-18 中建三局装饰有限公司 The modular self-supporting flying-wing device of a kind of Super High
CN205242770U (en) * 2015-12-24 2016-05-18 广州江河幕墙系统工程有限公司 Buckle formula glass wing device and in fixed all -wing aircraft glass's aluminum alloy glass cell body thereof

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