TWM606173U - Stress energy dissipation support device - Google Patents

Abstract

A stress energy dissipation support device, comprising a force receiving member, a plurality of positioning members, a plurality of enclosing wing plates, and a plurality of enclosing webs. The force receiving member has an energy dissipating part, and both sides sequentially extend the conversion part and the connecting part to form The receiving part, the positioning parts are respectively combined with the corresponding surfaces of the confining wing plate, any side part of the confining wing plate is combined with the joint part, and the positioning part and the receiving part form a displacement and deformation distance; the side wing parts of the confining web are respectively combined with the surrounding part Corresponding surface of the beam wing plate, the abutment part abuts on both sides of the thickness direction of the force member; when the force member is deformed by external force, the beam web resists and eliminates the stress in the thickness direction, and the beam wing plate and the positioning member resist and eliminate The width direction stress, and the spacing buffers the stress of the deformation of the force member, and there is a gap between the bundle web and the force member, which can be used for non-destructive inspection operations after the earthquake.

Description

Stress energy dissipation support device

This creation is related to a stress energy dissipation support device, especially a stress energy dissipation support device with multi-directional stress energy dissipation, space for inspection after earthquake, simple assembly and material saving.

my country is located on the rim of the Pacific Ocean seismic belt. The number of earthquakes is quite frequent, and there are often strong earthquakes. According to the observational data of the Central Meteorological Bureau from 1994 to 2013, there are about 23,000 earthquakes in Taiwan every year, including about 1,000 felt earthquakes. According to statistical analysis of disastrous earthquake data, there are 101 earthquakes since 1901. Disastrous earthquakes, several large-scale earthquakes in the past, such as the Qingshui Earthquake, the Shirakawa Earthquake, the 921 Chichi Earthquake, etc. The main cause of casualties was the collapse of buildings that could not bear the violent vibrations. In order to increase the strength of the tough support, the building will add diagonally supporting member devices between the beam and the column.

For example, the Republic of China Patent Announcement No. I369434 "Steel side brace buckling beam system" includes independent axial members and confining members. The axial members are one or two long steel plates, and the end section is relatively central The section of the part is large, and the enclosing member is composed of a long steel plate with bolt holes on both sides along the length direction and welded with a long steel member with a special shape section. The axial force members are placed in two independent sets of enclosures. However, the above-mentioned patents still have defects that need to be improved: whether long steel members are type,> type, or type, both ends of the opening are welded to the long steel plate. When the axial force is generated by the external force During elastic deformation, the force of the deformation will be dispersed to the elongated steel member and transmitted along the welding points at the two ends of the opening of the elongated steel member. The force will eventually concentrate on the apex of the elongated steel member. When the external force disappears or weakens, the The overall strength of the shaped steel member will form a reaction force and be released towards the ends of the opening, which will easily cause the long steel member and the long steel plate to separate from the weld.

Another example is the Republic of China Patent Announcement No. I245828 "Energy Dissipation Support Device", the patent specification records: "Mutualize the main part (20) and the fixed parts (30) on both sides to maintain a proper accommodating gap (42), and Machining makes the accommodating gap (41) slightly larger than the accommodating gap (42), and then place it in parallel on a clamping piece (40), and then the other clamping piece (40) is placed on the main body (20), side The upper surface of the fixing piece (30) is then welded or bolted to form a connection and fixation between the clamping piece (40) and the outer side of the side fixing piece (30), so that the main body (20) can be connected to the side fixing piece ( The gap of 30) and the gap of the clamping piece (40) provide the allowable movement area of the main body (20) for shock absorption and energy dissipation; the two ends (21) of the main body (20) must have perforations (25) to borrow the perforations (25) ) Is locked between the beam and the column". From the above, it can be seen that after the fixed pieces on both sides are combined with the two clamping pieces (to simplify the description, the structure of the combination of the fixed pieces on both sides and the two clamping pieces is hereinafter referred to as the assembly ), the main part is in a floating state, that is, the clamping part can drive the side fixed part to move in the accommodating gap.

Define the main part and the side fixing part. The cross-section of the main part has two symmetrical long sides and short sides. If the two long sides are perpendicular to the ground, it is used in a vertical state; if the two short sides are perpendicular to the ground, it is used in a horizontal state. The position of the fixing piece is on the short side of the main body, and the position of the clamping piece is on the long side of the main piece; when the main piece is used vertically, the side fixing piece above the short side is affected by gravity. It will directly abut on the short side of the main body, and only the side fixing part under the short side has an accommodation gap with the main body; when the main body is used horizontally, the clamping piece above the long side is affected by gravity , Will directly abut against the long side of the main body. Therefore, when the main body is deformed by external force, whether it is vertical or horizontal, the space available for deformation is only on the square and both sides. Or the weight of the clamping piece is against, and there is no room for deformation; and the assembly is in a floating state, when the main body is deformed and restored by external force, the assembly will not return to the original position, and because the main body and the assembly The accommodating gap relationship between the main part and the assembly is not in a parallel state, but has an angular difference. When the main part is deformed by an external force again, the main part will hit the assembly, although the distance of the accommodating gap Very short, but because it is combined with a steel-frame structure, the force of micro-deformation is quite large, resulting in a decrease in the service life of the main body and the assembly; at the same time, although the patent can be used to supplement the side sticks to strengthen the structure, It also increases the manufacturing cost, and also increases the overall volume and weight.

In view of the above-mentioned shortcomings of traditional use, the creators researched and improved ways to address the above-mentioned shortcomings, and finally got the original creation.

The main purpose of this creation is to provide a stress energy dissipation support device with multi-directional energy dissipation.

The secondary purpose of this creation is to provide a stress energy dissipation support device with a post-earthquake viewing space.

Another purpose of this creation is to provide a stress energy dissipation support device that is easy to assemble and save materials.

In order to achieve the above objectives and effects, the technical means adopted by the present invention include: a force-receiving member, a plurality of positioning members, a plurality of bundling wings, and a plurality of bundling webs, of which:

The force-receiving member has an energy dissipating part, a conversion part and a coupling part extend in sequence on both sides, the cross-sectional area of the coupling part is larger than the cross-sectional area of the energy dissipating part, so that two adjacent conversion parts and the energy dissipation part form a In the receiving part, each joint part is provided with a plurality of joint holes.

Each positioning member has a joining end surface on one side, and a stopping end surface corresponding to the aforementioned receiving portion structure on the other side.

There is a corresponding surface between each bundle wing plate, the side has a corresponding side edge, and the other two sides have a side edge. The surface is combined with the corresponding joint end surface of the aforementioned positioning member, and the side The combination is on the top surface and the bottom surface corresponding to the aforementioned joint portion. as well as,

The middle section of each encircling web has an abutting portion, and a side wing portion extends on both sides respectively, and the abutting portion abuts on both sides of the force receiving member, and each side wing portion is respectively combined with the side edge portion of the enclosing wing plate.

Each positioning piece is combined with the corresponding surface of the bundle wing plate, and each bundle wing plate is combined with the top and bottom surfaces of the corresponding joint, then the positioning piece and the receiving part form a displacement and deformation distance; the side wing parts of each bundle web are respectively In combination with the side edges of the aforementioned confining wing plate, the abutting parts are pressed against both sides of the force receiving member, whereby when the force receiving member is deformed by the external force, the confining web resists and eliminates the stress in the thickness direction, and the confining wing The plate and the positioning member resist and eliminate the stress in the width direction, and the spacing buffers the stress of the deformation of the force receiving member, achieving a structure with multi-directional stress energy dissipation, simple combination and material saving.

According to the above structure, the enclosing web can be arc, arch, arch, >, <,], or [shape, or bridging structure, and the length of the enclosing web is equal to or less than that of the enclosing wing The length of the board.

According to the above structure, the force-receiving member can be any one-sided joint part on the left or right side which is joined with the corresponding side edge part of the surrounding wing plate.

According to the above structure, the abutting portion of the enclosing web is a plate structure parallel to the aforementioned force member.

According to the above structure, a baffle is provided on both sides of the confining wing plate, and the side wing part is combined between the baffle and the confining wing plate to achieve a structure that resists and eliminates the stress of the side wing part and prevents falling off.

According to the above structure, the bundle wing plate and the side baffles on both sides can be channel steel structure or welded structure.

According to the above structure, the force-receiving member is provided with a plurality of energy dissipating parts, the two ends of each energy dissipating part respectively extend the aforementioned conversion part, a connecting part is formed between two adjacent conversion parts, and the conversion parts on the two sides are respectively Connecting the aforementioned coupling parts forms a plurality of aforementioned receiving parts between each energy dissipating part and adjacent conversion parts.

According to the above structure, the number of the positioning members corresponds to the aforementioned receiving portion.

According to the above structure, the cross-sectional area of the connecting portion is equal to the cross-sectional area of the aforementioned coupling portion.

According to the above structure, the top surface and the bottom surface of the connecting portion are respectively combined with the corresponding surfaces of the bundling wings.

In order to obtain a more detailed understanding of the above-mentioned purposes, effects and features of this creation, the descriptions are as follows according to the drawings:

Please refer to Figure 1 and Figure 2. It can be seen that the structure of this creation mainly includes: a force member 1, a plurality of positioning members 2, a plurality of binding wings 3, and a plurality of binding webs 4, of which:

The force receiving member 1 has an energy dissipating part 11, the two ends of the energy dissipating part 11 respectively extend a conversion part 12 and a joining part 13 in sequence, and a receiving part is formed between two adjacent conversion parts 12 and the energy dissipating part 11 14, and the cross-sectional area of the coupling portion 13 is greater than the cross-sectional area of the energy dissipation portion 11, and each coupling portion 13 is provided with a plurality of coupling holes 131.

Each positioning member 2 has a coupling end surface 21 on one side, and a stop end surface 22 corresponding to the structure of the receiving portion 14 on the other side.

Each confining wing plate 3 has a surface 31, the side has a corresponding side edge 32, and the other two sides have a side edge 33 respectively, and the surface 31 of each confining wing plate 3 is corresponding.

The middle section of each encircling web 4 has an abutting portion 41, and a side wing 42 extends on both sides. In this embodiment, the encircling web 4 is represented by an arc structure, but it is not limited to the encircling web 4 It is an arc-shaped structure, for example, a structure in which the middle section has the abutment portion 41 and the side wing portions 42 are extended on both sides, such as arc, arch, arch, >, <, ], or [shape, bridge structure, etc., They should all belong to the scope of this creation.

Please refer to Figures 3 to 5 for assistance. When the above-mentioned structures are combined, the bonding end faces 21 of each positioning member 2 are combined on the surface 31 of the bundling wing plate 3. It should be noted that the "combination" can be welding, riveting, or The screw and nut are locked. In order to simplify the drawing and facilitate the description, the present embodiment is represented by welding technical means, and the welding points in each figure are indicated by the component number 5. The subsequent description will not explain the welding points 5 one by one.

After the binding wing plate 3 is combined with the positioning member 2, the side part 32 of each binding wing plate 3 is combined to the upper and lower ends of the joint 13, for example, the upper and lower ends of the joint 13 are welded to the side part 32. It should be noted that the force-receiving member 1 combined with the bundle wing plate 3 can be the top surface and the bottom surface of any one-sided joint 13 on the left or right side, respectively combined to the side of the corresponding bundle wing plate 3. In this embodiment, the joint 13 on the left side of the force-receiving member 1 is combined with the side portion 32 on the left side of the upper and lower bundling wing panels 3 respectively. On the contrary, the force-receiving member 1 can also be a joint on the right. The portion 13 is combined with the side portion 32 on the right side of the enclosing wing plate 3; at this time, each positioning member 2 is located in the receiving portion 14 of the force receiving member 1, and between the stopping end surface 22 of the positioning member 2 and the receiving portion 14 A gap 15 is formed. At this time, the force-bearing member 1 and the upper and lower beam wings 3 can be regarded as an H-shaped structure. The left and right sides of the force-bearing member 1 form a semi-open space S which can be used by relevant personnel. Non-destructive testing. Then, each enclosing web 4 is placed into the semi-open space S left and right, and the abutting portion 41 of the middle section of the enclosing web 4 abuts on both sides of the force receiving member 1 (it should be noted that, Taking the force member 1 as the reference, the joint 13 and the side edge 32 of the bundling wing plate 3 are combined, that is, the upper and lower ends. Therefore, the joint 13 of the force member 1 is between the upper and lower ends The sidewalls of the surrounding bundle web 4 are defined as "both sides"), and each side wing portion 42 of the surrounding bundle web 4 is connected to the edge portion 33 of the corresponding surface 31 of the bundle wing board 3 (both ends of the bundle web 4 are side wing portions 42, and "the edge portion 33 of the surface 31", that is, the long sides of the bundling wings 3 between the side portions 32 at both ends).

Please refer to Figures 6 to 8 for assistance. The joints 13 at both ends of the force-receiving member 1 are combined with the steel frame 6 respectively. When the force-receiving member 1 is deformed by an external force, it is guided by the encircling web 4 to resist and eliminate the force-receiving member 1 The stress in the thickness direction, the enclosing wing plate 3 and the positioning member 2 resist and eliminate the stress in the width direction of the force receiving member 1, and the space 15 buffers the stress of the deformation of the force member 1 to achieve multi-directional stress energy dissipation, Check the space after the earthquake, and the structure is easy to assemble and save materials.

Referring to FIG. 9, the feature of this embodiment compared with the previous embodiments is that the abutting portion 41 of the encircling web 4 is a plate-like or sheet-like structure and is parallel to the energy dissipation portion 11 of the force receiving member 1. A structure that increases the force receiving area between the abutting portion 41 and the energy dissipation portion 11 is achieved.

Please refer to FIG. 10, the feature of this embodiment compared to the previous embodiments is that a baffle 34 is provided on both sides of the bundling wing plate 3, and the side wing portion 42 of the bundling web 4 is combined with the baffle 34 and the baffle. Between the wing plates 3, a structure to eliminate the stress of the side wing portion 42 and prevent falling off is achieved. It should be noted that the confining wing plate 3 and the baffles 34 on both sides can be channel steel structure or welded structure.

Referring to FIG. 11, the feature of this embodiment compared with the previous embodiment is that the force receiving member 1 is provided with at least one or more energy dissipation parts 11, and both ends of each energy dissipation part 11 extend the aforementioned conversion parts 12, two A connecting portion 16 is formed between the adjacent conversion portions 12, and the conversion portions 12 on the two sides are respectively connected to the aforementioned coupling portion 13, and the cross-sectional area of the coupling portion 16 is equal to the cross-sectional area of the aforementioned coupling portion 13; When the force member 1 is combined with the aforementioned binding wing plate 3, in addition to the combination of the top surface and bottom surface of the aforementioned one-side or two-side joining portion 13 respectively to the surface 31 of the binding wing plate 3 on the corresponding side, it can further be both sides 32 are not combined with the upper and lower ends of the connecting portion 13, but instead are combined with the upper and lower ends of the connecting portion 14 of the force receiving member 1 with the corresponding surface 31 of the bundle wing plate 3; A plurality of receiving parts 14 are formed, and the number of positioning elements 2 corresponds to the number of receiving parts 15, so that not only the length of use can be increased, but also the combination of multiple sets of receiving parts 14 and positioning elements 2 can be used to achieve multi-stage stress energy dissipation Structure.

In summary, the new stress energy dissipation support device of the present invention is indeed a novel and progressive creation, and Yan has applied for a new patent according to law; however, the content of the above description is only a description of the preferred embodiment of this creation. Any changes, modifications, alterations or equivalent replacements extended by the technical means and scope of this creation should also fall within the scope of the patent application for this creation.

1: Force parts 11: Energy Dissipation Department 12: Conversion Department 13: Joint 131: Combination hole 14: Containment Department 15: spacing 16: connection part 2: positioning parts 21: Combine the end face 22: Stop end face 3: Bundle wing board 31: Surface 32: side 33: Side edge 34: bezel 4: Encircling web 41: abutment 42: Flanking 5: Welding 6: Steel structure S: Semi-open space

[Figure 1] is a three-dimensional view of a preferred embodiment of this creation. [Figure 2] is a three-dimensional exploded view of the preferred embodiment of this creation. [Figure 3] is the first three-dimensional combination diagram of the preferred embodiment of this creation. [Figure 4] is the second three-dimensional combination diagram of the preferred embodiment of this creation. [Figure 5] is the three-dimensional combination diagram of the preferred embodiment of this creation. [Figure 6] is a reference diagram of the use state of the preferred embodiment of this creation. [Figure 7] is a cross-sectional view of part A-A` in [Figure 6]. [Figure 8] is a sectional view of part B-B` in [Figure 6]. [Figure 9] is a cross-sectional view of part C-C` in [Figure 6]. [Figure 10] is another preferred embodiment of the encircling web created by this invention. [Figure 11] is a diagram of another preferred embodiment of the binding wing panel of this creation. [Figure 12] is a diagram of another preferred embodiment of the force-receiving member and positioning member of this creation.

1: Force parts

13: Joint

131: Combination hole

3: Bundle wing board

32: side

33: Side edge

4: Encircling web

41: abutment

42: Flanking

5: Welding

Claims (10)

A stress energy dissipation support device, which at least includes: a force receiving member, a plurality of positioning members, a plurality of enclosing wing plates, and a plurality of enclosing webs, wherein: the force receiving member has an energy dissipation part, The two ends respectively extend a conversion part and a coupling part in sequence. The cross-sectional area of the coupling part is larger than the cross-sectional area of the energy dissipation part, so that a receiving part is formed between the conversion part and the energy dissipation part, and each coupling part is provided with a plurality of coupling holes. One side of each positioning member has a joining end surface, and the other side has a stop end surface corresponding to the aforementioned receiving portion structure; there is a corresponding surface between the surrounding beam wings, and the surface side has a The side part has a side edge part on the other two sides, the surface is combined with the joint end surface corresponding to the aforementioned positioning member, and the side part is combined on the top surface and bottom surface corresponding to the aforementioned joint part; and, the middle section of each bundle web There is an abutment portion, one side wing portion extends on both sides respectively, the abutment portion abuts on both sides of the aforementioned force member, and each side wing portion is respectively combined with the side edge portion of the aforementioned bundling wing plate; the combined end surface of each positioning member Combine on the corresponding surface of each of the aforementioned confining wing panels, and the top and bottom surfaces of the single-sided joint part are combined to the side part of the confining wing panel on the corresponding side, then the positioning member is located in the aforementioned receiving part and is connected to the positioning member The stop end surface of each enclosing web forms a distance; and, the side wing portions of each enclosing web are respectively combined with the side edge portions of the aforementioned enclosing wing plate, so that the abutting portion abuts on both sides of the force receiving member, whereby the force receiving member is When the external force deforms, the enclosing web guides and resists and eliminates the stress in the thickness direction, while the enclosing wing plate and the positioning member resist and eliminate the stress in the width direction, and use the spacing to buffer the stress of the deformation of the force member. The directional stress dissipates energy, and the combination is simple and material-saving structure. The stress energy dissipation support device according to claim 1, wherein the enclosing web can be arc, arch, arch,> shape, <shape,] shape, or [shape, or bridging structure, and the enclosure The length of the web is equal to or less than the length of the bundle wing. The stress energy dissipating support device according to claim 1, wherein the force receiving member can be any one-sided joint part on the left or right side which is joined with the side part of the corresponding side of the bundle wing panel. The stress energy dissipation support device according to claim 1, wherein the abutting portion of the enclosing web is a plate structure parallel to the aforementioned force member. The stress energy dissipation support device according to claim 1, wherein a baffle is provided on the side edge of the confining wing plate, and the side wing part is combined between the baffle and the confining wing plate to achieve resistance and eliminate the side wing Structure to prevent stress and prevent falling off. The stress energy dissipation support device according to claim 5, wherein the confining wing plate and the baffles on both sides can be channel steel structure or welded structure. The stress energy dissipating support device according to claim 1, wherein the force receiving member has a plurality of energy dissipating parts, the two ends of each energy dissipating part respectively extend the aforementioned conversion part, and a connecting part is formed between two adjacent conversion parts, The conversion parts on the two sides are respectively connected to the aforementioned coupling parts, and a plurality of the aforementioned receiving parts are formed between each energy dissipation part and the adjacent conversion parts. The stress energy dissipation support device according to claim 7, wherein the number of the positioning members corresponds to the number of the aforementioned receiving parts. The stress energy dissipation support device according to claim 7, wherein the cross-sectional area of the connecting portion is equal to the cross-sectional area of the aforementioned coupling portion. The stress energy dissipation support device according to claim 7, wherein the top surface and the bottom surface of the connecting portion are respectively combined with the corresponding surfaces of the bundling wing panels.

Images