CN204212294U - The modular self-supporting flying-wing device of a kind of Super High - Google Patents
The modular self-supporting flying-wing device of a kind of Super High Download PDFInfo
- Publication number
- CN204212294U CN204212294U CN201420591638.2U CN201420591638U CN204212294U CN 204212294 U CN204212294 U CN 204212294U CN 201420591638 U CN201420591638 U CN 201420591638U CN 204212294 U CN204212294 U CN 204212294U
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- China
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- aluminum alloy
- alloy frame
- main body
- building main
- wing aircraft
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Abstract
The utility model relates to the modular self-supporting flying-wing device of a kind of Super High, comprise building main body, described building main body is connected with all-wing aircraft unit of encorbelmenting, described all-wing aircraft unit of encorbelmenting comprises the bearing unit plate be arranged on structure trunk and the aluminum alloy frame being arranged at bearing unit plate both sides, described aluminum alloy frame is enclosed by horizontal frame and munnion and forms, the inside of described aluminum alloy frame is provided with shaped steel, is provided with sunk screw between described aluminum alloy frame and shaped steel; The horizontal frame of described aluminum alloy frame is provided with adaptor, described adaptor is provided with steel suspension member, described adaptor is mounted by steel suspension member and building main body, also connecting bolt is provided with between described steel suspension member and building main body, the all-wing aircraft part of encorbelmenting in outside meets the load bearing system of force request by self syndeton, formation, while the moulding of formation all-wing aircraft, there is load-carrying members advantages of simple, stable connection, and there is the beneficial effect of easy accessibility.
Description
Technical field
The utility model relates to a kind of Super High modular self-supporting all-wing aircraft system, be particularly useful for more than 100 meters building without load-carrying members position unit type curtain wall install time technology apply.
Background technology
At present, state's Curtain Wall is due to the needs of Appearance of Architecture, the complex space moulding of some uniquenesses is needed to be applied to building appearance, super highrise building also adopts type unitized curtain wall system more and more widely, when whole building form compare is regular, normal cells formula curtain wall is processed in suitability for industrialized production, guarantee that installation accuracy and water resistance aspect all have obvious advantage, in super highrise building Curtain Wall Design process, local location gives prominence to the all-wing aircraft system ubiquity of large of curtain wall, and this position is general without agent structure, common type unitized curtain wall system is the all-wing aircraft moulding realizing these uniquenesses, on the one hand, connector of encorbelmenting in a large number need be set up when structure design, strengthen frame section sectional dimension anyhow, cause unit plate processing technology complicated, the safety of system and practicality are difficult to be taken into account, on the other hand, all-wing aircraft plate mounts in process, installation accuracy cannot be controlled effectively, increase difficulty of construction equally, final installation quality and appearance effect must be had influence on.
Utility model content
Goal of the invention of the present utility model is: for prior art Problems existing, provide a kind of construction and installation easy, form the modular self-supporting flying-wing device of the Super High meeting force request by the structure of self.
To achieve these goals, the technical solution adopted in the utility model is:
The modular self-supporting flying-wing device of a kind of Super High, comprise building main body, described building main body is connected with all-wing aircraft unit of encorbelmenting, described all-wing aircraft unit of encorbelmenting comprises the bearing unit plate be arranged on structure trunk and the aluminum alloy frame being arranged at bearing unit plate both sides, described aluminum alloy frame is enclosed by horizontal frame and munnion and forms, the inside of described aluminum alloy frame is provided with shaped steel, is provided with sunk screw between described aluminum alloy frame and shaped steel; The horizontal frame of described aluminum alloy frame is provided with adaptor, described adaptor is provided with steel suspension member, described adaptor is mounted by steel suspension member and building main body, is also provided with connecting bolt between described steel suspension member and building main body.
Preferably, weldable steel square tube is provided with between described shaped steel and aluminum alloy frame.Adopt such structure, have that syndeton is more stable, the better beneficial effect of rigidity.
In sum, owing to have employed technique scheme, the beneficial effects of the utility model are: by being connected to form an overall all-wing aircraft unit by without the plate (i.e. aluminum alloy frame) of load-carrying members position and adjacent two without the building main body bearing unit plate between the plate of load-carrying members position, and reinforced by the mode increasing shaped steel in aluminum alloy frame, aluminum alloy frame and shaped steel transport to scene in advance after processing factory completes, only need by the adaptor on horizontal frame and steel suspension member, by also fixing in unit plate mounting and building main body, make all-wing aircraft part that it is encorbelmented in outside by self syndeton, form the load bearing system meeting force request, while the moulding of formation all-wing aircraft, there is load-carrying members advantages of simple, stable connection, and there is the beneficial effect of easy accessibility.
Accompanying drawing explanation
Fig. 1 is side elevation structural representation of the present utility model;
Fig. 2 is profile in plan of the present utility model;
Fig. 3 is the detailed construction schematic diagram of Fig. 1;
Mark in figure: aluminum alloy frame-1; Weldable steel square tube-2; Sunk screw-3; Bolt-4; Steel suspension member-5; Adaptor-6; Shaped steel-7; Building main body-8; Hollow tempered glass-9; Gripper shoe-10; Glass block-11.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in detail.
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
As shown in Figure 1 to Figure 3, the modular self-supporting flying-wing device of the present embodiment Super High, comprise building main body 8, building main body 8 is connected with all-wing aircraft unit of encorbelmenting, in the present embodiment, the height of all-wing aircraft unit of encorbelmenting is more than or equal to 100m, all-wing aircraft unit of encorbelmenting comprises the bearing unit plate be arranged on structure trunk, and be arranged at the aluminum alloy frame 1 of bearing unit plate both sides, aluminum alloy frame 1 frame is enclosed by horizontal frame and munnion and forms, the inside of aluminum alloy frame 1 is provided with shaped steel 7, weldable steel square tube 2 is provided with between shaped steel 7 and aluminum alloy frame 1, the rectangular square tube that weldable steel square tube in the present embodiment and both sides are welded respectively at shaped steel 7 and aluminum alloy frame, sunk screw 3 is provided with between aluminum alloy frame 1 and shaped steel 7, the bottom of shaped steel 7 extends to form the gripper shoe 10 for carrying hollow tempered glass 9 to the outside of structure trunk 8, the top of described gripper shoe 10 is provided with glass block 11, and the top of described glass block 11 is provided with hollow tempered glass 9.The horizontal frame of aluminum alloy frame 1 is provided with adaptor 6, adaptor 6 in the present embodiment is in tabular, one end of adaptor 6 is fixedly connected with the horizontal frame of aluminum alloy frame 1, the other end upwards extends, adaptor 6 is provided with steel suspension member 5, adaptor 6 is mounted by steel suspension member 5 and building main body 8, connecting bolt 4 is also provided with between steel suspension member 5 and building main body 8, adopt such structure, there is syndeton more stable, the better beneficial effect of rigidity, the present embodiment is by being connected to form an overall all-wing aircraft unit by without the plate (i.e. aluminum alloy frame 1) of load-carrying members position and adjacent two without the building main body 8 bearing unit plate between the plate of load-carrying members position, and reinforced by the mode increasing shaped steel 7 in aluminum alloy frame 1, aluminum alloy frame 1 and shaped steel 7 transport to scene in advance after processing factory completes, only need by the adaptor 6 on horizontal frame and steel suspension member 5, by also fixing in unit plate mounting and building main body 8, make all-wing aircraft part that it is encorbelmented in outside by self syndeton, form the load bearing system meeting force request, while the moulding of formation all-wing aircraft, there is load-carrying members advantages of simple, stable connection, and there is the beneficial effect of easy accessibility.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (2)
1. the modular self-supporting flying-wing device of Super High, comprise building main body, described building main body is connected with all-wing aircraft unit of encorbelmenting, it is characterized in that: described in all-wing aircraft unit of encorbelmenting comprise the bearing unit plate be arranged on structure trunk and the aluminum alloy frame being arranged at bearing unit plate both sides, described aluminum alloy frame is enclosed by horizontal frame and munnion and forms, the inside of described aluminum alloy frame is provided with shaped steel, is provided with sunk screw between described aluminum alloy frame and shaped steel; The horizontal frame of described aluminum alloy frame is provided with adaptor, described adaptor is provided with steel suspension member, described adaptor is mounted by steel suspension member and building main body, is also provided with connecting bolt between described steel suspension member and building main body.
2. the modular self-supporting flying-wing device of Super High according to claim 1, is characterized in that: be provided with weldable steel square tube between described shaped steel and aluminum alloy frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420591638.2U CN204212294U (en) | 2014-10-14 | 2014-10-14 | The modular self-supporting flying-wing device of a kind of Super High |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420591638.2U CN204212294U (en) | 2014-10-14 | 2014-10-14 | The modular self-supporting flying-wing device of a kind of Super High |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204212294U true CN204212294U (en) | 2015-03-18 |
Family
ID=52980980
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420591638.2U Expired - Fee Related CN204212294U (en) | 2014-10-14 | 2014-10-14 | The modular self-supporting flying-wing device of a kind of Super High |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204212294U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN108442588A (en) * | 2018-04-02 | 2018-08-24 | 武汉凌云建筑装饰工程有限公司 | The design method of irregular stereo polygonal element curtain wall |
-
2014
- 2014-10-14 CN CN201420591638.2U patent/CN204212294U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN106968371B (en) * | 2017-03-20 | 2018-09-04 | 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 |
| CN108442588A (en) * | 2018-04-02 | 2018-08-24 | 武汉凌云建筑装饰工程有限公司 | The design method of irregular stereo polygonal element curtain wall |
| CN108442588B (en) * | 2018-04-02 | 2020-11-10 | 武汉凌云建筑装饰工程有限公司 | Method for designing special-shaped three-dimensional polygonal unit curtain wall |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150318 Termination date: 20151014 |
|
| EXPY | Termination of patent right or utility model |