CN212642286U

CN212642286U - Stress energy dissipation support device

Info

Publication number: CN212642286U
Application number: CN202022093122.3U
Authority: CN
Inventors: 吴郁宣; 廖秀敏
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-09-22
Filing date: 2020-09-22
Publication date: 2021-03-02
Anticipated expiration: 2030-09-22

Abstract

The utility model discloses a stress energy dissipation support device, which comprises a stress part, a plurality of positioning parts, a plurality of surrounding beam wing plates and a plurality of surrounding beam web plates, wherein the stress part is provided with an energy dissipation part, two sides of the stress part sequentially extend a conversion part and a combination part to form an accommodating part, the positioning parts respectively combine the corresponding surfaces of the surrounding beam wing plates, any side part of the surrounding beam wing plates is combined with the combination part, and a displacement and deformation interval is formed between the positioning part and the accommodating part; the side wing parts of the girding web plates are respectively combined with the corresponding surfaces of the girding wing plates, and the abutting parts abut against the two sides of the stressed part in the thickness direction; when the stress piece is deformed by an external force, the enclosure beam web resists and eliminates the stress in the thickness direction, the enclosure beam wing plate and the positioning piece resist and eliminates the stress in the width direction, the deformation stress of the stress piece is buffered at intervals, and a gap is reserved between the enclosure beam web and the stress piece, so that nondestructive detection operation can be performed after an earthquake.

Description

Stress energy dissipation support device

Technical Field

The utility model relates to a stress energy dissipation supporter especially indicates a stress energy dissipation supporter device that has multi-direction stress energy dissipation, possesses and shakes the back and look at the space, and the combination is simple and convenient, save material.

Background

On the pacific earthquake zone around gulf position of China, the earthquake occurs quite frequently and often occurs strongly. The observation data of the taiwan meteorological office from 1994 to 2013 of 20 years shows that 23,000 earthquakes occur in the taiwan area per year on average, wherein the number of the sensitive earthquakes is about 1,000; in terms of the statistical analysis of the disastrous earthquake data, 101 times of disastrous earthquakes are counted from 1901, the main casualties caused by the large-scale earthquakes in the past, such as the clean water earthquake and the great earthquake in the white river, 921 concentrated on the great earthquake, are caused by the fact that the building cannot bear violent vibration and collapses, and therefore, the building can be provided with the structural material device which can increase the toughness supporting strength and can increase the inclined support between the beam and the column.

For example, taiwan patent publication No. I369434, "steel side bracing buckling restraining member", includes independent axial force members and confining members, the axial force members are one or two long steel plates, the cross section of the end portion of each of the axial force members is larger than that of the central portion of each of the axial force members, the confining members are formed by welding a long steel plate having bolt holes along the longitudinal direction on both sides thereof and a long steel member having a cross section of a special shape, and the axial force members are placed between two independent confining members; however, the above patents still have disadvantages to be improved: the long steel member is of a type, a shape or a shape, two open ends are welded on the long steel plate, when the axial force member is subjected to external force to generate elastic deformation, the deformation force is dispersed to the long steel member and is transmitted along welding points at the two open ends of the long steel member, the force is finally concentrated at the top point of the long steel member, when the external force disappears or is weakened, the overall force of the long steel member forms a reaction force and is released towards the two open ends, and the long steel member and the long steel plate are easily separated from the welding position.

For another example, taiwan patent publication No. I2457828 "energy dissipation support device", the patent specification: mutually arranging the main body piece (20) and the two side fixing pieces (30) to keep a proper accommodating gap (42), processing to enable the accommodating gap (41) to be slightly larger than the accommodating gap (42), then parallelly arranging the main body piece and the side fixing pieces on one clamping piece (40), correspondingly arranging the other clamping piece (40) on the main body piece (20) and the side fixing pieces (30), and then cooperatively welding or using bolts to connect and fix the clamping pieces (40) and the side fixing pieces (30) to form a connection and fixation, so that the main body piece (20) can provide a shock-absorbing and energy-dissipating allowable moving area for the main body piece (20) in the gap between the main body piece and the side fixing pieces (30) and the gap between the main body piece and the clamping pieces (40); the two ends (21) of the main body (20) are provided with through holes (25) to be locked between the beam and the column through the through holes (25). As can be seen from the above, after the two side fixing members and the two clamping members are combined (for the sake of simplifying the description, the structure of the combination of the two side fixing members and the two clamping members, hereinafter referred to as an assembly), the main body is in a floating state, that is, the clamping members can drive the side fixing members to move in the accommodating gaps.

Defining a main body part and a side fixing part, wherein the cross section of the main body part is provided with two symmetrical long sides and short sides, and the two long sides are vertical to the ground and are in a vertical use state; the two short sides are vertical to the ground and are in a horizontal use state, the side fixing piece is positioned on the side surface of the short side of the main body piece, and the clamping piece is positioned on the side surface of the long side of the main body piece; when the main body piece is used vertically, the side fixing piece above the short side surface is influenced by gravity and can directly abut against the short side surface of the main body piece, and only the side fixing piece below the short side surface has an accommodating gap with the main body piece; when the main body piece is horizontally used, the clamping piece above the long side surface is influenced by gravity and can directly abut against the long side surface of the main body piece, so that when the main body piece is deformed by external force, no matter in a vertical or horizontal state, only the space for deformation is left on the left side and the left side, and the space above the main body piece is abutted by the weight of the side fixing piece or the clamping piece without the space for deformation; the assembly is in a floating state, when the main body part is deformed by external force and is recovered, the assembly cannot return to the original position, and because of the containing clearance relationship between the main body part and the assembly, the main body part and the assembly cannot be in a parallel state and have an angle difference, when the main body part is deformed by the external force again, the main body part can impact the assembly, although the containing clearance distance is extremely short, the micro-deformation force is quite large because the main body part is combined on a building with a steel skeleton structure, and the service life of the main body part and the assembly is reduced; meanwhile, although the patent can use the side attachment piece reinforcing structure in an auxiliary way, the manufacturing cost is increased, and the whole volume and weight are also increased.

In view of the above disadvantages, the present invention provides a new and improved method for improving the performance of a medical device.

SUMMERY OF THE UTILITY MODEL

The utility model discloses main aim at provides a stress energy dissipation eyelidretractor device with multi-direction ability dissipation.

The utility model discloses secondary aim at provides an utensil shakes the stress energy dissipation eyelidretractor device of back inspection space.

Another object of the present invention is to provide a combined simple and energy-saving stress energy-dissipating support device.

To achieve the above objects and effects, the present invention provides a method comprising: a atress piece, plural setting element, plural enclose and restraint the pterygoid lamina, enclose and restraint the web with plural number, wherein:

the stress piece is provided with an energy dissipation part, a conversion part and a combination part sequentially extend from two sides of the stress piece, the sectional area of the combination part is larger than that of the energy dissipation part, a containing part is formed between two adjacent conversion parts and the energy dissipation part, and each combination part is provided with a plurality of combination holes.

One side of each positioning piece is provided with a combination end surface, and the other side is provided with a stop end surface corresponding to the accommodating part structure.

The surrounding wing plates are provided with a corresponding surface, the side edges are provided with a corresponding side edge part, the other two side edges are provided with a side edge part, the surface is combined with the corresponding combination end surface of the positioning piece, and the side edge parts are combined on the corresponding top surface and the bottom surface of the combination part. And the number of the first and second groups,

the middle section of each enclosure web plate is provided with a leaning part, two sides of the leaning part extend to form a wing part respectively, the leaning part is propped against two sides of the stress piece, and each wing part is combined with the side edge part of the enclosure web plate respectively.

Each positioning piece is respectively combined with the corresponding surface of the surrounding beam wing plate, and each surrounding beam wing plate is combined with the top surface and the bottom surface of the corresponding combining part, so that a displacement and deformation space is formed between each positioning piece and the accommodating part; the lateral wing part of each enclosure web plate is respectively combined with the lateral edge part of the enclosure beam wing plate, so that the abutting parts abut against the two sides of the stress piece, therefore, when the stress piece deforms under an external force, the enclosure beam web plates resist and eliminate the stress in the thickness direction, the enclosure beam wing plates and the positioning pieces resist and eliminate the stress in the width direction, and the stress of the deformation of the stress piece is buffered at intervals, so that the structure with multidirectional stress energy dissipation, simple and convenient combination and material saving is achieved.

Preferably, the containment web may be arcuate, arched, arcuate, > shaped, < shaped, ] shaped, or [ shaped, or bridge shaped, and the length of the containment web is equal to or less than the length of the containment flaps.

Preferably, the force-bearing part can be formed by combining any one of the left-side or right-side combining parts with the corresponding side part of the girding wing plate.

Preferably, the abutting part of the enclosing web is a plate structure parallel to the force bearing part.

Preferably, the two sides of the enclosure wing plate are respectively provided with a baffle plate, and the side wing parts are combined between the baffle plates and the enclosure wing plate, so that a structure for resisting and eliminating the stress of the side wing parts and preventing the side wing parts from falling off is achieved.

Preferably, the beam enclosing wing plate and the side baffles on the two sides can be of a channel steel structure or a welding structure.

Preferably, the force receiving member has a plurality of energy dissipation parts, two ends of each energy dissipation part extend to the conversion parts, a connection part is formed between two adjacent conversion parts, and the conversion parts at the two most sides are connected to the connection parts, so that a plurality of accommodating parts are formed between each energy dissipation part and the adjacent conversion parts.

Preferably, the number of the positioning pieces corresponds to the number of the accommodating parts.

Preferably, the cross-sectional area of the connecting portion is equal to the cross-sectional area of the connecting portion.

Preferably, the top surface and the bottom surface of the connecting part are respectively combined with the corresponding surfaces of the enclosing wing plates.

Advantageous effects

Compared with the prior art, the beneficial effects of the utility model are that: displacement and deformation intervals are formed between the positioning piece and the accommodating part; when the stress piece is deformed by an external force, the enclosure beam web resists and eliminates the stress in the thickness direction, the enclosure beam wing plate and the positioning piece resist and eliminates the stress in the width direction, the deformation stress of the stress piece is buffered at intervals, and a gap is reserved between the enclosure beam web and the stress piece, so that nondestructive detection operation can be performed after an earthquake.

Drawings

Fig. 1 is a perspective view of the preferred embodiment of the present invention.

Fig. 2 is an exploded perspective view of the preferred embodiment of the present invention.

Fig. 3 is a first perspective assembly view of the preferred embodiment of the present invention.

Fig. 4 is a second perspective assembly view of the preferred embodiment of the present invention.

Fig. 5 is a three-dimensional assembly view of the preferred embodiment of the present invention.

Fig. 6 is a reference diagram of the usage status of the preferred embodiment of the present invention.

FIG. 7 is a partial sectional view of A-A' of FIG. 6.

FIG. 8 is a partial sectional view of B-B' in FIG. 6.

FIG. 9 is a partial sectional view of C-C' of FIG. 6.

Fig. 10 is a view of yet another preferred embodiment of the girth web of the present invention.

Fig. 11 is a view of another preferred embodiment of the containment flaps of the present invention.

Fig. 12 is a diagram of another preferred embodiment of the force-bearing member and the positioning member of the present invention.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

Referring to fig. 1 and 2, it can be seen that the structure of the present invention mainly includes: a atress spare 1, a plurality of setting element 2, a plurality of enclose restraint pterygoid lamina 3, a plurality of enclose restraint web 4, wherein:

the stress member 1 has an energy dissipation part 11, two ends of the energy dissipation part 11 respectively extend a conversion part 12 and a connection part 13 in sequence, a receiving part 14 is formed between two adjacent conversion parts 12 and the energy dissipation part 11, the cross-sectional area of the connection part 13 is larger than that of the energy dissipation part 11, and each connection part 13 is provided with a plurality of connection holes 131.

Each positioning element 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 containment flap 3 has a surface 31, a side edge having a corresponding side edge portion 32, and two side edges having a side edge portion 33, and the surfaces 31 of the containment flaps 3 correspond to each other.

In the present embodiment, the central section of each enclosure web 4 has an abutting portion 41, and two sides of the enclosure web 4 extend to a wing portion 42, but the enclosure web 4 is represented by an arc structure, but the enclosure web 4 is not limited to be only an arc structure, and the central section has the abutting portion 41, and two sides of the enclosure web 4 extend to the wing portion 42, such as an arc, an arch, a shape < shape >, or a [ shape, bridge structure, etc., all of which belong to the scope of the present invention.

Referring to fig. 3 to 5, in the above structure combination, the combination end surface 21 of each positioning element 2 is respectively combined with the surface 31 of the surrounding beam wing plate 3, it should be noted that "combination" may be welding, riveting, or screw and nut locking, for simplifying the drawing and facilitating the description, the embodiment is represented by a welding technique, the welding position in each figure is represented by an element number 5, and the welding position 5 will not be explained in detail in the following description.

After the binding wing plates 3 are combined with the positioning member 2, the side edge portions 32 of the binding wing plates 3 are combined with the upper and lower ends of the combining portion 13, for example, the upper and lower ends of the combining portion 13 are welded with the side edge portions 32, it should be noted that the stress member 1 is combined with the binding wing plates 3, and the top surface and the bottom surface of any one-side combining portion 13 on the left side or the right side can be respectively combined with the side edge portions 32 of the corresponding binding wing plates 3; in the present embodiment, the coupling portion 13 on the left side of the force receiving member 1 is combined with the side edge portion 32 on the left side of the upper and lower girding flanges 3; conversely, the force receiving member 1 may be formed by combining the right-side connecting portion 13 with the right-side edge portion 32 of the containment flaps 3; at this time, each positioning member 2 is located in the receiving portion 14 of the force receiving member 1, and a space 15 is formed between the stop end surface 22 of the positioning member 2 and the receiving portion 14, at this time, the force receiving member 1 and the upper and lower confining wing plates 3 can be regarded as an H-shaped structure, a semi-open space S is formed on the left and right sides of the force receiving member 1, and can be used for nondestructive detection by relevant personnel, then, each confining wing plate 4 is respectively placed in the semi-open space S on the left and right sides, the abutting portion 41 in the middle section of the confining wing plate 4 abuts against the two sides of the force receiving member 1 (it should be noted that, with the force receiving member 1 as a reference, the combining portion 13 and the side edge portion 32 of the confining wing plate 3 are combined, i.e. the upper and lower ends, so that the side wall between the upper and lower ends of the combining portion 13 of the force receiving member 1, i.e. the wing portion is defined as "two sides"), and each side wing portion 42 of the confining web plate 4 is respectively combined with the edge portion 33 of the corresponding surface 31, and "edge 33 of surface 31", i.e., the long side of containment flaps 3 between both end side portions 32).

Referring to fig. 6 to 8, the joints 13 at the two ends of the stressed member 1 are respectively combined with the steel skeleton structure 6, when the stressed member 1 is deformed by an external force, the stress in the thickness direction of the stressed member 1 is guided and resisted and eliminated by the encircling web plate 4, the stress in the width direction of the stressed member 1 is resisted and eliminated by the encircling web plate 3 and the positioning member 2, and the deformed stress of the stressed member 1 is buffered by the space 15, so that the structure with multidirectional stress energy dissipation, post-earthquake inspection space, simple and convenient combination and material saving is achieved.

Referring to fig. 9, the feature of this embodiment compared to the previous embodiment is that the abutting portion 41 of the girth web 4 is a plate-shaped or sheet-shaped structure and is parallel to the energy dissipation portion 11 of the force receiving member 1, so as to achieve a structure of increasing the force receiving area between the abutting portion 41 and the energy dissipation portion 11.

Referring to fig. 10, the present embodiment is characterized in that two sides of the containment strake 3 are respectively provided with a baffle 34, and the side wing 42 of the containment strake 4 is combined between the baffle 34 and the containment strake 3 to achieve a structure of eliminating stress of the side wing 42 and preventing falling off, and it should be noted that the containment strake 3 and the baffles 34 at two sides can be a channel steel structure or a welded structure.

Referring to fig. 11, the characteristics of this embodiment compared to the previous embodiments are that the force receiving member 1 has at least one or more energy dissipation parts 11, two ends of each energy dissipation part 11 respectively extend to the conversion parts 12, a connection part 16 is formed between two adjacent conversion parts 12, the conversion parts 12 at the two sides are respectively connected to the connection part 13, and the cross-sectional area of the connection part 16 is equal to the cross-sectional area of the connection part 13; it should be noted that, when the force-bearing member 1 is combined with the aforementioned encircling wing plate 3, besides the top surface and the bottom surface of the aforementioned one-side or two-side combining portion 13 are respectively combined to the surface 31 of the encircling wing plate 3 on the corresponding side, further, the two-side edge portions 32 are not combined with the upper and lower ends of the combining portion 13, but the upper and lower ends of the connecting portion 14 of the force-bearing member 1 are respectively combined with the corresponding surface 31 of the encircling wing plate 3; a plurality of receiving parts 14 are formed between the adjacent converting parts, and the number of the positioning pieces 2 corresponds to that of the receiving parts 15, so that the length of use can be increased, and a multi-stage stress energy dissipating structure can be achieved by combining a plurality of groups of receiving parts 14 and positioning pieces 2.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims

1. Stress energy dissipation eyelidretractor device, its characterized in that: it includes a atress piece, plural setting element, plural enclose and restraint the pterygoid lamina, enclose and restraint the web with plural number at least, wherein:

the stress piece is provided with an energy dissipation part, two ends of the stress piece respectively extend a conversion part and a combination part in sequence, the sectional area of the combination part is larger than that of the energy dissipation part, so that an accommodating part is formed between the conversion part and the energy dissipation part, and each combination part is respectively provided with a plurality of combination holes;

one side of each positioning piece is provided with a combination end surface, and the other side of each positioning piece is provided with a stop end surface corresponding to the accommodating part structure;

a corresponding surface is arranged between the surrounding and restraining wing plates, the side edge of the surface is provided with a side edge part, the other two sides are provided with a side edge part, the surface is combined with the corresponding combination end surface of the positioning piece, and the side edge parts are combined on the corresponding top surface and the bottom surface of the combination part; and the number of the first and second groups,

each middle section of the enclosure web plate is provided with a leaning part, two sides of the middle section of the enclosure web plate extend to form a wing part respectively, the leaning parts lean against two sides of the stress piece, and each side wing part is combined with the side edge part of the enclosure web plate respectively;

the combination end surfaces of the positioning pieces are combined on the corresponding surfaces of the enclosure wing plates, the top surfaces and the bottom surfaces of the single-side combination parts are respectively combined on the side edge parts of the enclosure wing plates on the corresponding sides, and the positioning pieces are arranged in the accommodating parts and form a distance with the stopping end surfaces of the positioning pieces; and the side wing part of each encircling web plate is respectively combined with the side edge part of the encircling web plate, so that the abutting part abuts against two sides of the stress piece, therefore, when the stress piece deforms under the external force, the stress in the thickness direction is guided and resisted and eliminated through the encircling web plate, the stress in the width direction is resisted and eliminated through the encircling web plate and the positioning piece, and the stress of the deformation of the stress piece is buffered by means of the distance, so that the structure with multidirectional stress energy elimination is achieved.

2. A stress-dissipating support device according to claim 1, in which: the confining web is in an arc shape, an arch shape, a > shape, < shape, <shape, a shape, or a [ shape, or a bridging structure, and the length of the confining web is equal to or less than that of the confining wing plates.

3. A stress-dissipating support device according to claim 1, in which: the stressed part is formed by combining a single-side combining part on the left side or the right side with a side edge part on the corresponding side of the girding wing plate.

4. A stress-dissipating support device according to claim 1, in which: the abutting part of the enclosing web is a plate structure parallel to the force bearing part.

5. A stress-dissipating support device according to claim 1, in which: the side edge parts of the enclosing wing plates are respectively provided with a baffle plate, and the side wing parts are combined between the baffle plates and the enclosing wing plates, so that the structure for resisting and eliminating the stress of the side wing parts and preventing the side wing parts from falling off is achieved.

6. A stress-dissipating support device according to claim 5, in which: the enclosure wing plate and the baffles on the two sides are of channel steel structures or welded structures.

7. A stress-dissipating support device according to claim 1, in which: the stress element is provided with a plurality of energy dissipation parts, two ends of each energy dissipation part respectively extend to the conversion parts, a connecting part is formed between two adjacent conversion parts, the conversion parts at the two most sides are respectively connected with the connecting part, and a plurality of accommodating parts are formed between each energy dissipation part and the adjacent conversion parts.

8. A stress-dissipating support device according to claim 7, in which: the number of the positioning pieces corresponds to the number of the accommodating parts.

9. A stress-dissipating support device according to claim 7, in which: the cross-sectional area of the connecting portion is equal to the cross-sectional area of the connecting portion.

10. A stress-dissipating support device according to claim 7, in which: the top surface and the bottom surface of the connecting part are respectively combined with the corresponding surfaces of the surrounding beam wing plates.