A portion of the disclosure of this patent document contains material, which is subject to copyright protection. The copyright owner has no objection to the facsimile reproduction by anyone of the patent document or the patent disclosure, as it appears in the Patent and Trademark Office patent file or records, but otherwise reserves all copyright rights whatsoever.
The present application claims priority to CN Patent Application No. 202310035365.7 filed Jan. 10, 2023; the disclosure of which is incorporated herein by reference in its entirety.
The present invention relates to the technical field of wind-resistant and seismic-resistant building structures, particularly to a damage-free engagement device for enhanced wind-resistance of base-isolated structures.
Seismic isolation technology is an effective way to reduce the damage caused by earthquakes to building structures, and to provide full protection on human life and property. In recent years, it has been widely used in construction. The basic principle of seismic isolation technology is to install isolation bearings with lower horizontal stiffness in the seismic isolation layer, which prolongs the natural vibration period of the structure, and reduces the seismic response of the super-structure. Therefore, theoretically, an isolation layer with a lower horizontal stiffness would yield a better isolation effect.
In the design of seismic isolation, the horizontal stiffness of the seismic isolation layer should be minimized to fully utilize the isolation performance of the seismic isolators, provided that the relevant codes and standards are met. However, when the seismic isolation structure needs to withstand large wind loads (such as in areas with high wind loads, high-rise buildings or wind-sensitive structures), excessively low stiffness of the seismic isolation layer may lead to excessive floor acceleration response under wind load, resulting in discomfort issues during wind loading.
In order to meet the wind-comfort requirements of the seismic isolation structures, the conventional technology generally resort to an increased horizontal stiffness of the seismic isolation layer. This method to some extent reduces the functional advantages of the seismic isolation structure and cannot achieve the maximum “horizontal earthquake isolation” function, thereby reducing the seismic isolation efficiency of the structure.
In order to address the conflict between the flexibility demand for seismic isolation and the stiffness demand for wind-induced vibration-resistance in seismic isolation structures, it is necessary to add wind resistance units in the seismic isolation layer to: 1) provide additional stiffness under wind load, 2) withdraw from operation under medium and large earthquakes and ensure the complete release of the flexibility of the seismic isolation layer. To date, the wind resistance devices added to existing seismic isolators have various defects, such as the non-adjustable additional stiffness, the complex structural configuration which is difficult to maintain, the inability to switch automatically from a “wind-resistance locked” to a “seismic isolation unlocked” state, and the possible plastic damages of components under large earthquake actions.
The purpose of the present invention is to provide a damage-free engagement device for enhanced wind-resistance of base-isolated structures to overcome the defects in the prior arts.
The purpose of the present invention can be achieved by the following technical solution:
The technical solution of the present invention is to provide a damage-free engagement device for enhanced wind-resistance of base-isolated structures, which includes:
A rubber seismic isolation support is placed between the super-structure and the sub-structure of a seismic isolation layer. The support has an upper and a lower surface, each equipped with a connecting plate that links the super-structure and the sub-structure of the seismic isolation layer.
A group of wind-resistance stiffness adjusters are disposed between the upper connecting plate and the lower connecting plate. These wind-resistance stiffness adjusters surround the rubber seismic isolation support. The wind-resistance stiffness adjuster includes a horizontal sliding bearing plate fixed on the upper connecting plate, a vertical guide groove disposed on the lower connecting plate, and components arranged within the vertical guide groove. The components in the vertical guide groove include a bird beak plate and a disc spring group in sequence from top to bottom. The bird beak plate is able to slide up and down along the vertical guide groove, and an upper hook structure of the bird beak plate fits and hooks with the horizontal sliding bearing plate.
In which the seismic isolation support is a commercially available product commonly used for building seismic isolation.
In a further embodiment, the bird beak plate has a comma-shaped structure, and comprises a circular structure and an upper hook structure integrated with the circular structure, and the horizontal sliding bearing plate has an L-shaped structure, and comprises a horizontal bar and protrusions located at an end of the horizontal bar, and the upper hook structure of the bird beak plate engages with and hooks onto the protrusions of the horizontal sliding bearing plate.
In a further embodiment, when the upper hook structure of the bird beak plate engages and hooks onto the protrusions of the horizontal sliding bearing plate, an interface between them forms an inclined slope surface.
In a further embodiment, wherein a central part of the circular structure of the bird beak plate has a hole through which a horizontal connecting rod passes to connect the plurality sets of wind-resistance stiffness adjusters set side by side.
In a further embodiment, two side walls of the vertical guide groove are non-equal in length and comprise a longer side wall and a shorter side wall, and the highest point of the longer side wall is lower than the lowest point of the horizontal sliding bearing plate.
In a further embodiment, the longer side wall further fits slidingly with the upper hook structure of the bird beak plate, and the shorter side wall fits slidingly with the circular structure of the bird beak plate.
In a further embodiment, upper and lower surfaces of the disc spring group disposed with an upper steel washer and a lower steel washer, the upper steel washer is in contact with a bottom of the bird beak plate, and the lower steel washer is equipped with a stiffness adjustment bolt to adjust a compression state of the disc spring group.
In a further embodiment, the stiffness adjustment bolt comprises a bolt end plate positioned on the vertical guide groove, a bolt fixed to the bolt end plate, and a washer and a nut threaded sequentially through the bolt from top to bottom.
In a further embodiment, a center of the lower steel washer has a hole, allowing the bolt to pass through the lower steel washer.
In a further embodiment, when the bolt passes through the lower steel washer to secure the stiffness adjustment bolt to the disc spring group, the washer further fits against the lower steel washer, and the bolt end plate fits against the bottom of the vertical guide groove.
Compared with the prior art, the present invention has the following beneficial effects:
The labels in the figure are as follows:
The following detailed description of the present invention is provided in conjunction with the accompanying drawings and specific embodiments.
In the following embodiments, unless otherwise specified, functional components or structures not specifically mentioned are considered to be conventional components or structures commonly used in the field for achieving their respective functions.
As shown in
The bird beak plate 6 shown in
The principle of operation of the present invention is as follows: The compressive characteristics of the disc spring assembly 10 and the horizontal resistance generated by the engagement and hooking between the bird beak plate 6 and the horizontal sliding bearing plate 3 provide horizontal stiffness to resist the bending moment and horizontal shear load borne by the seismic isolation layer under wind load. This effectively solves the wind resistance issue in isolation structures. Under certain seismic actions, the bird beak plate 6 is subjected to horizontal thrust, which compresses the disc spring assembly 10 in the vertical guide groove 7 and disengages from the horizontal sliding bearing plate 3. Consequently, the wind stiffness adjuster is disengaged and no longer restrains the horizontal displacement of the seismic isolation layer. The rubber seismic isolation support 4 begins to function. The initial stiffness of the wind stiffness adjuster does not affect the horizontal isolation effect of the rubber seismic isolation support 4, thus avoiding the issue of excessive horizontal stiffness in the isolation support caused by considering wind-induced vibration in existing designs. After an earthquake, the stiffness adjustment bolt 9 can be turned to release the pressure on the disc spring assembly 10. Then, the horizontal sliding bearing plate 3 is adjusted to re-engage and hook onto the bird beak plate 6, and finally, the stiffness adjustment bolt 9 is tightened to restore the working state of the wind stiffness adjuster quickly. This process ensures that no component replacement or plastic damage occurs throughout the entire process of the “wind lock-isolation unlock-wind lock” mechanism.
The installation method of the present invention device is as follows:
The description of the above embodiments is provided to enable those skilled in the art to understand and use the invention. It will be apparent to those skilled in the art that various modifications can be made to these embodiments and that the general principles described herein can be applied to other embodiments without departing from the inventive concept. Therefore, the present invention is not limited to the above embodiments, and any improvements and modifications made by those skilled in the art based on the disclosure of the present invention should be within the scope of the present invention.
Number | Date | Country | Kind |
---|---|---|---|
202310035365.7 | Jan 2023 | CN | national |
Number | Name | Date | Kind |
---|---|---|---|
4527365 | Yoshizawa | Jul 1985 | A |
4991366 | Teramura | Feb 1991 | A |
5125761 | Cullen | Jun 1992 | A |
8641282 | Chuang | Feb 2014 | B2 |
8789319 | Li | Jul 2014 | B2 |
9856670 | Kraft | Jan 2018 | B1 |
11339849 | Zhou | May 2022 | B2 |
20130148917 | Chuang | Jun 2013 | A1 |
20140041320 | Li | Feb 2014 | A1 |
20210301900 | Zhou | Sep 2021 | A1 |
20220290457 | Yang | Sep 2022 | A1 |