CN107989277B - Novel aluminum alloy structure wide goose plate - Google Patents
Novel aluminum alloy structure wide goose plate Download PDFInfo
- Publication number
- CN107989277B CN107989277B CN201711485203.4A CN201711485203A CN107989277B CN 107989277 B CN107989277 B CN 107989277B CN 201711485203 A CN201711485203 A CN 201711485203A CN 107989277 B CN107989277 B CN 107989277B
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- China
- Prior art keywords
- aluminum alloy
- plate
- plates
- wing
- tail connecting
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- 241000272814 Anser sp. Species 0.000 title claims abstract description 43
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 41
- 238000003756 stirring Methods 0.000 claims abstract description 23
- 238000003466 welding Methods 0.000 claims abstract description 19
- 239000000463 material Substances 0.000 claims description 8
- 230000000295 complement effect Effects 0.000 claims description 2
- 238000010276 construction Methods 0.000 abstract description 5
- 230000007547 defect Effects 0.000 abstract description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 3
- 238000001125 extrusion Methods 0.000 description 10
- 239000000956 alloy Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 206010057040 Temperature intolerance Diseases 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000004040 coloring Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000008543 heat sensitivity Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 238000004078 waterproofing Methods 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04D—ROOF COVERINGS; SKY-LIGHTS; GUTTERS; ROOF-WORKING TOOLS
- E04D3/00—Roof covering by making use of flat or curved slabs or stiff sheets
- E04D3/24—Roof covering by making use of flat or curved slabs or stiff sheets with special cross-section, e.g. with corrugations on both sides, with ribs, flanges, or the like
- E04D3/30—Roof covering by making use of flat or curved slabs or stiff sheets with special cross-section, e.g. with corrugations on both sides, with ribs, flanges, or the like of metal
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Joining Of Building Structures In Genera (AREA)
- Roof Covering Using Slabs Or Stiff Sheets (AREA)
Abstract
The invention discloses a novel wild goose plate with an aluminum alloy structure, which comprises an upper two symmetrically inclined wing plates, a lower beam, a top horizontal wing tail connecting plate and honeycomb aluminum alloy sections. The single plate is in a wild goose shape, and the thickness of the single plate is gradually thinned from the root to the tail. The inclined wing plate consists of 3 variable cross-section plates, and the lower beam and the top horizontal wing tail connecting plate are all integrally extruded cross sections. The parts constituting the wild goose plate are connected by friction stir welding. The horizontal wing tail connecting plate at the top is symmetrical in shape except at the junction; the cross sections of the junctions are fastened with each other, so that reliable connection between two wild goose plates can be ensured, and the problem of water resistance of the wild goose plate roof can be solved. The invention not only overcomes the defects of the traditional roof truss, but also meets the building functions and realizes the green construction and high assembly targets.
Description
Technical Field
The invention relates to a novel wild goose plate with an aluminum alloy structure, and belongs to the technical field of building structures.
Background
At present, most of the commonly used structural forms in various industrial plants, warehouses and large-space public buildings are traditional roof trusses. However, the traditional roof truss is very heavy in dead weight, increases the construction measure cost of transportation, hoisting and the like, greatly increases the foundation cost of the structure, has poor corrosion resistance, and has no integrated design with the structure due to the functions of roof waterproofing and the like.
The aluminum alloy material has the characteristics of light weight, high strength-quality ratio, good corrosion resistance, basically no maintenance, easy extrusion molding, high material recycling rate, green construction and the like, so that the aluminum alloy material is widely applied to structural engineering. In view of the characteristics of the aluminum alloy materials, the defect problem of the traditional roof truss is exactly solved, and the assembly rate of the building engineering is improved.
With the deep research of aluminum alloy materials, the appearance of novel hard aluminum, super hard aluminum and other materials, and the maturity of a novel welding process-friction stir welding technology specially researched for the aluminum alloy materials, the feasibility of the implementation of the wide goose plate with the aluminum alloy structure is technically ensured.
Disclosure of Invention
The invention aims to overcome the defects of the traditional roof truss and provides a novel wild goose plate with an aluminum alloy structure.
The invention is realized by the following technical scheme:
the novel wide goose plate with the aluminum alloy structure comprises two symmetrical inclined wing plates at the upper part, a lower beam and a top horizontal wing tail connecting plate, wherein the inclined wing plates, the lower beam and the horizontal wing tail connecting plate are all honeycomb-shaped aluminum alloy sections;
the inclined wing plates, the lower beam and the horizontal wing tail connecting plates are connected through friction stir welding;
after the wild goose plate with the aluminum alloy structure is mutually overlapped with the other wild goose plate with the aluminum alloy structure, the waterproof problem of the roof can be solved;
the cross section of the wild goose plate with the aluminum alloy structure is in a wild goose shape, the included angle between the two symmetrical inclined wing plates and the horizontal direction is 20 degrees (plus 0-10 degrees), the thickness of the two symmetrical inclined wing plates is gradually thinned from the root part to the tail part, the root part is 100mm, the tail part of the inclined wing plates is reduced to 50mm, the height of the lower beam is 325mm, and the width of the lower beam is 200mm;
the thickness of the rib plate with the honeycomb aluminum alloy section and the upper and lower flange plates except the junction are that
4.0-5.0 mm, and the rest is 2.0-3.0 mm; the transverse width of the wide goose plate with the aluminum alloy structure is generally 3-4 meters, and the longitudinal span of the wide goose plate can be spanned by 9-30 meters.
The variable cross-section treatment mode not only meets the requirements of the structure on strength, deformation and stability, but also can save materials and improve economic benefits.
The symmetrical inclined wing plates are formed by combining 3 honeycomb aluminum alloy sections with variable cross sections, the lower beam is a honeycomb aluminum alloy section formed by integral extrusion, and the top horizontal wing tail connecting plate is also a honeycomb aluminum alloy section formed by integral extrusion;
the top horizontal wing tail connecting plate needs to be extruded into a folded plate, so that smooth realization of friction stir welding is guaranteed.
The 3 variable cross-section honeycomb aluminum alloy sections of the upper symmetrical inclined wing plates, the root parts of the inclined wing plates and the lower beam, and the tail parts of the root parts of the inclined wing plates and the top horizontal wing tail connecting plates are connected through friction stir welding.
The top horizontal wing tail connecting plate is symmetrical in shape except at the joint; the cross section form of the junction of the top horizontal wing tail connecting plates is complementary and is a mutually fastened form, so that the aim of ensuring the reliability of connection between two wild goose plates is fulfilled, and meanwhile, the problem of water resistance of the wild goose plate roof is solved.
The assembly of the wild goose plate structure can not influence the construction progress of the working procedures such as equipment installation below the roof of the building main body. The parts constituting the wild goose plate are connected by friction stir welding. The horizontal wing tail connecting plate at the top is symmetrical in shape except at the junction; the cross sections of the junctions are fastened with each other, so that reliable connection between two wild goose plates can be ensured, and the problem of water resistance of the wild goose plate roof can be solved. The invention not only overcomes the defects of the traditional roof truss, but also meets the building functions and realizes the green construction and high assembly targets.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present invention;
FIG. 2 is a schematic view of the structure of the lower beam;
FIG. 3 is a schematic view of the structure of two symmetrical inclined wing plate roots;
FIG. 4 is a schematic view of the structure of the middle of two symmetrical inclined flanges;
FIG. 5 is a schematic view of the structure of the tail of two symmetrical inclined wings;
FIG. 6 is a schematic view of the structure of the top horizontal tail web first;
FIG. 7 is a schematic view of the structure of a top horizontal tail connection plate II;
FIG. 8 is a schematic view of horizontal movement during the process of connecting two complete wild goose plates;
FIG. 9 is a schematic view of vertical movement during the process of joining two complete wild goose plates;
fig. 10 is a schematic diagram of two complete wild goose plates after connection is completed.
Reference numerals illustrate: the first horizontal wing tail connecting plate, the second horizontal wing tail connecting plate, the tail part of the 3-inclined wing plate, the middle part of the 4-inclined wing plate, the root part of the 5-inclined wing plate and the lower beam.
Detailed Description
The invention is further described below with reference to the drawings and examples, which are not intended to be limiting in any way.
As shown in figures 1-10, the novel aluminum alloy structure wild goose plate comprises two symmetrical inclined wing plates at the upper part, a lower beam 6 and a horizontal wing tail connecting plate at the top, wherein each part is a honeycomb aluminum alloy section. The upper two symmetrical inclined wing plates are divided into a root 5, a middle part 4, a tail 3, a lower beam 6, a horizontal wing tail connecting plate 1 and a horizontal wing tail connecting plate 2 at the top. These parts are all aluminum alloy honeycomb sections extruded at one time in the factory. Extrusion processes require the use of extrusion front equipment, extruders, extrusion back equipment, extrusion tooling including basic tools and dies, with the dies being the most important extrusion tools. Anodic oxidation and coloring are also needed to be carried out on the component after extrusion molding so as to achieve the optimal corrosion resistance and durability of the aluminum alloy.
After the members are extruded, the members are fixed by a supporting device according to the external dimensions and angles shown in fig. 1, and friction stir welding is performed at the contact positions of the members. The friction stir welding is to utilize the stirring head with special shape of hard stirring finger stick to insert the welded head and to generate heat with the welded metal in a friction stir, and simultaneously combine the extrusion of the stirring head to the weld joint metal to make the joint metal in a plastic state, and the stirring finger stick moves forward along the welding direction while rotating to form compact intermetallic combination under the combined action of heat and machine to realize the connection of materials. The stirring head consists of a stirring finger rod with a special shape and a shaft shoulder. The length of the stirring finger rod is equal to the plate thickness, but in general, the length of the stirring finger rod is slightly shorter than the thickness of the base material; and the diameter of the shaft shoulder is larger than that of the stirring finger rod. The friction stir welding does not need a filler wire and inert gas protection in the welding process; the groove and special treatment on the surface of the material are not needed before welding, and the defects of air holes, cracks and the like are not generated during welding. The materials such as hard aluminum, super hard aluminum and the like with strong heat sensitivity can be reliably connected by friction stir welding, so that the joint strength of the aluminum alloy structure is improved, and the problem of reduced joint strength of the aluminum alloy material caused by fusion welding is solved.
After all the components are connected into an integral wild goose plate through friction stir welding, the wild goose plate is transported to a factory for hoisting. Because the design considers that the horizontal wing tail connecting plates at the top are mutually fastened and considers the dimensional relationship between the horizontal direction and the vertical direction, when the wild goose plates are hoisted, only one wild goose plate is hoisted in place, and the other wild goose plate moves horizontally to the in-place wild goose plate and then moves vertically upwards, so that the lap joint of the two wild goose plates can be completed. The lapped wild goose plate roof not only realizes structural connection, but also solves the waterproof problem of the roof.
Therefore, the novel aluminum alloy structure wild goose plate with light weight, high strength, corrosion resistance, no maintenance and strong durability is formed.
The above is only a specific application example of the present invention, and other embodiments of the present invention are also possible, and all the technical solutions formed by equivalent substitution or equivalent transformation fall within the scope of protection claimed by the present invention.
Claims (4)
1. Novel aluminum alloy structure wide goose board, its characterized in that: the wing plate comprises two symmetrical inclined wing plates at the upper part, a lower beam and a top horizontal wing tail connecting plate, wherein the inclined wing plates, the lower beam and the horizontal wing tail connecting plate are all honeycomb-shaped aluminum alloy sections; the inclined wing plates, the lower beam and the horizontal wing tail connecting plates are connected through friction stir welding; after the two wide goose plates with the aluminum alloy structures are mutually overlapped, the waterproof problem of the roof can be solved; the cross section of the wide goose plate with the aluminum alloy structure is in a wide goose shape; the top horizontal wing tail connecting plate is symmetrical in shape except at the joint; the cross section forms of the joints of the top horizontal wing tail connecting plates are complementary and are mutually fastened; the included angle between the two symmetrical inclined wing plates and the horizontal direction is 20 degrees, the thickness of the two symmetrical inclined wing plates gradually becomes thinner from the root part to the tail part, the root part is 100mm, and the tail part of the inclined wing plates is reduced to 50mm; the symmetrical inclined wing plates are formed by combining 3 honeycomb aluminum alloy sections with variable cross sections, the lower beam is an integrally extruded honeycomb aluminum alloy section, and the top horizontal wing tail connecting plate is also an integrally extruded honeycomb aluminum alloy section.
2. The novel wild goose plate with the aluminum alloy structure according to claim 1, wherein the variable cross section processing mode not only meets the requirements of the structure on strength, deformation and stability, but also can save materials and improve economic benefit.
3. The novel aluminum alloy structured wild goose plate as claimed in claim 1, wherein: the top horizontal wing tail connecting plate is extruded into a folding plate.
4. The novel aluminum alloy structured wild goose plate as claimed in claim 1, wherein: the 3 variable cross-section honeycomb aluminum alloy sections forming the upper symmetrical inclined wing plates, the root parts of the inclined wing plates and the lower beam, and the tail parts of the inclined wing plates and the top horizontal wing tail connecting plates are connected through friction stir welding.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201711485203.4A CN107989277B (en) | 2017-12-30 | 2017-12-30 | Novel aluminum alloy structure wide goose plate |
Applications Claiming Priority (1)
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CN201711485203.4A CN107989277B (en) | 2017-12-30 | 2017-12-30 | Novel aluminum alloy structure wide goose plate |
Publications (2)
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CN107989277A CN107989277A (en) | 2018-05-04 |
CN107989277B true CN107989277B (en) | 2024-01-23 |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH09324492A (en) * | 1996-06-06 | 1997-12-16 | Nippon Light Metal Co Ltd | Building structure member and roof support structure member using the building structure member |
CN2580001Y (en) * | 2002-11-20 | 2003-10-15 | 程渝 | Prestress concrete wild goose shape plate |
CN1877186A (en) * | 1996-03-19 | 2006-12-13 | 株式会社日立制作所 | Friction stir welding method and structure body formed |
CN206174238U (en) * | 2016-09-12 | 2017-05-17 | 上海通正铝业(昆山)航空科技有限公司 | Aluminum alloy structural engineering's roof structure |
CN106801489A (en) * | 2017-03-24 | 2017-06-06 | 广东铝遊家科技有限公司 | Aluminum alloy roof board combining structure |
CN208168175U (en) * | 2017-12-30 | 2018-11-30 | 贵阳铝镁设计研究院有限公司 | A kind of aluminium alloy structure wide goose plate |
-
2017
- 2017-12-30 CN CN201711485203.4A patent/CN107989277B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1877186A (en) * | 1996-03-19 | 2006-12-13 | 株式会社日立制作所 | Friction stir welding method and structure body formed |
JPH09324492A (en) * | 1996-06-06 | 1997-12-16 | Nippon Light Metal Co Ltd | Building structure member and roof support structure member using the building structure member |
CN2580001Y (en) * | 2002-11-20 | 2003-10-15 | 程渝 | Prestress concrete wild goose shape plate |
CN206174238U (en) * | 2016-09-12 | 2017-05-17 | 上海通正铝业(昆山)航空科技有限公司 | Aluminum alloy structural engineering's roof structure |
CN106801489A (en) * | 2017-03-24 | 2017-06-06 | 广东铝遊家科技有限公司 | Aluminum alloy roof board combining structure |
CN208168175U (en) * | 2017-12-30 | 2018-11-30 | 贵阳铝镁设计研究院有限公司 | A kind of aluminium alloy structure wide goose plate |
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CN107989277A (en) | 2018-05-04 |
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