FRP Composite Spiral Stirrup Confined Concrete Column And Compression Design Method Thereof

Abstract

The present disclosure discloses a Fiber Reinforced Polymer/Plastic (FRP) composite spiral stirrup confined concrete column and a compression design method. The FRP composite spiral stirrup includes an internal FRP spiral stirrup and an external FRP square stirrup. In the form of the FRP composite spiral stirrup, effective transverse stress transfer is established by effectively binding stirrups, which can give full play to the mechanical properties of the FRP bars, provide “dual confinement” for core concrete, and greatly improve the peak stress of the core concrete. Confining mechanisms of the FRP composite spiral stirrup to the concrete in different areas are analyzed, a confinement model and a bearing capacity calculation method for the FRP composite spiral stirrup confined concrete column are proposed, and a design method for the FRP composite spiral stirrup confined concrete column is proposed after an accurate calculation method for the bearing capacity is obtained.

Claims

1. A Fiber Reinforced Polymer/Plastic (FRP) composite spiral stirrup confined concrete column, comprising: an FRP composite spiral stirrup (1), longitudinal bars (2), and concrete (3), wherein the longitudinal bars (2) comprise a central longitudinal bar (2-1) and corner longitudinal bars (2-2); the central longitudinal bar (2-1) is bound with the FRP composite spiral stirrup (1), and the corner longitudinal bars (2-2) are bound with a square stirrup to form a reinforcement skeleton; the reinforcement skeleton is arranged in the concrete (3); the FRP composite spiral stirrup (1) comprises an internal FRP spiral stirrup (1-1) and an external FRP square stirrup (1-2); the diameter of the internal FRP spiral stirrup (1-1) is equal to the side length of the external FRP square stirrup (1-2); each circle of FRP spiral stirrup is bound with an FRP square stirrup; and the longitudinal bars are also evenly distributed at the corners of the FRP square stirrup.

2. The FRP composite spiral stirrup confined concrete column according to claim 1, wherein the FRP square stirrup and the FRP spiral stirrup use one or more of Glass Fiber Reinforced Polymer/Plastic (GFRP) bars, Carbon Fiber Reinforced Polymer/Plastic (CFRP) bars, Basalt Fiber Reinforced Polymer/Plastic (BFRP) bars, and Aramid Fiber Reinforced Polymer/Plastic (AFRP) bars.

3. The FRP composite spiral stirrup confined concrete column according to claim 1, wherein the longitudinal bars use one of steel bars, the GFRP bars, the CFRP bars, the BFRP bars, and the AFRP bars, or mixed bars of the steel bars and FRP bars.

4. A compression design method for the FRP composite spiral stirrup confined concrete column according to claim 1, comprising the following steps: step one: applying the column to a marine environment, so as to determine the environment type of an area where the column is located and the action grade thereof, and perform a durability design on members under different design service lives and corresponding limit states; step two: working out an overall scheme and a structural form according to design requirements, and preliminarily determining sectional dimensions of the FRP composite spiral stirrup confined concrete column with reference to the existing design and relevant data; step three: calculating the maximum design bearing capacity of a control cross section of the column under the design service life and the limit state according to the worked outbuilding scale of a building structure, the position where the column is located, and a set load feature; step four: preliminarily working out the configurations of longitudinal bars and stirrups according to the preliminarily worked out sectional dimensions, the maximum design bearing capacity under the limit state, and the reinforcement requirements in a specification; step five: determining effective lateral confinement stresses of the internal FRP spiral stirrup and the external FRP square stirrup; and step six: making a composite spiral stirrup confinement model, and calculating the limit bearing capacity of the FRP composite spiral stirrup confined concrete column.

5. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 4, wherein in step five, a formula for calculating the effective lateral confinement stress of the FRP spiral stirrup is as follows: $f_1{}^{\text{'}}=k_e\frac{2f_{\text{fb}}{A}_{\text{f}}}{S{d}_{\text{s}}}$ in the formula, $f_{fb}$ is a smaller value of the bending strength of the spiral stirrup and 0.004E .sub.ft .sup., and E .sub.ft is the tensile modulus of elasticity of a reinforcement material; A.sub.f is the sectional area of the spiral stirrup; S is the spacing between stirrups; $d_s$ is the diameter between the middle lines of the spiral stirrups; k.sub.e is an effective confinement coefficient; a formula for calculating the effective confinement coefficient k.sub.e of the FRP spiral stirrup is as follows: $k_e=\frac{A_e}{A_{cc}}=\frac{1-\frac{S^{\text{'}}}{2d_s}}{1-{\rho }_{cc}}$ in the formula, .sup.Acc is the area of the concrete enclosed by the middle lines of the spiral stirrups and does not comprise the area of the longitudinal bars; A.sub.e is the effective confinement area of the effectively confined core concrete; S′ is the clear distance between stirrups; and p.sub.cc is the ratio of the area of the longitudinal bars to the sectional core area.

6. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 4, wherein in step five, for the FRP square stirrup, the lateral confinement stress generated by the same in a horizontal plane is unevenly distributed; a confining force reaches the maximum at the longitudinal bar; an arch-shaped “ineffective confinementarea” between two adjacent longitudinal bars is in a quadratic parabola shape; the area of the parabola is $2$ $w_i^2/6,$ wherein W.sub.i is the clear distance between the two adjacent longitudinal bars; the square stirrup also has an arch-shaped “ineffective confinement area” in the vertical direction; so, for the FRP square stirrup, a process for calculating the effective lateral confinement stress f.sub.2’ is as follows: ${{\displaystyle f}}_2^{\text{'}}=\frac{{{\displaystyle f}}_{1\text{x}}^{\text{'}}+{{\displaystyle f}}_{1\text{y}}^{\text{'}}}{2}$ wherein, ${{\displaystyle f}}_{1\text{x}}^{\text{'}}=k_{\text{e}}{\rho }_{\text{x}}{f}_{\text{fb}}=k_e\frac{A_{\text{sx}}}{S{d}_c}{f}_{\text{fb}}$ ${{\displaystyle f}}_{\text{ly}}^{\text{'}}=k_{\text{e}}{\rho }_{\text{y}}{f}_{\text{fb}}=k_e\frac{A_{\text{sy}}}{S{b}_c}{f}_{\text{fb}}$ in the formula, f.sub.lX’ is an effective lateral confinement stress in an x direction; f.sub.ly’ is an effective lateral confinement stress in a y direction; A.sub.sx is the total area of the stirrup in the x direction; A.sub.sy is the total area of the stirrup in the y direction; b.sub.c and d.sub.c, are distances of centerlines of the rectangular stirrup in two directions, respectively, where $b_c\ge d_c;$ a formula for calculating the effective confinement coefficient k.sub.e of the FRP square stirrup is as follows: $k_e=\frac{A_e}{A_{cc}}=\frac{(1-{\displaystyle \underset{i=1}{\overset{n}{.Math.}}\frac{w_i^2}{6b_c{d}_c}})(1-\frac{S^{\text{'}}}{2b_c})(1-\frac{S^{\text{'}}}{2d_c})}{\left(1-{\rho }_{cc}\right)}$ in the formula, n the number of the longitudinal bars.

7. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 4, wherein in step six, when the composite spiral stirrup confinement model is made, in order to accurately reflect the actual confining effect of each stirrup, a composite spiral stirrup confinement area is divided into a dual confinement area and a single confinement area to accurately reflect the actual confining effect of each stirrup, wherein the dual confinement area is an area inside the spiral stirrup, and the single confinement area is an area from the spiral stirrup to the square stirrup; a peak stress expression of the concrete in the dual confinement area is as follows: $f_{cc1}=f_{co}\left(1.0+3.897{(\frac{{{{\displaystyle f}}^{\text{'}}}_d}{f_{co}})}^{0.737}\right)$ in the formula, ƒ.sub.cc1 is the peak stress of the concrete in the dual confinement area; ƒ.sub.co is the strength of confined concrete; ƒ.sub.d’ is the sum of the effective lateral confinement stresses of the spiral stirrup and the rectangular stirrup; a peak stress expression of the concrete in the single confinement area is as follows: $f_{cc2}=f_{co}\left(2.254\sqrt{1+\frac{7.94f_2\text{'}}{f_{co}}-}2\frac{f_2\text{'}}{f_{co}}-1.254\right)$ in the formula, ƒ.sub.cc2 is the peak stress of the concrete in the single confinement area; ƒ.sub.co is the strength of the confined concrete; ƒ.sub.2’ is an effective lateral confinement stress of the FRP rectangular stirrup; finally, a formula for calculating the bearing capacity of the FRP composite spiral stirrup confined concrete column is as follows: $P_0=f_{cc1}\left(A_1-n_{1}A{}_{bar}\right)+f_{cc2}(A_2-n_2{A}_{bar})+n{\epsilon }_{bar}{E}_{bar}{A}_{bar}$ in the formula, P.sub.0 is the bearing capacity of the FRP composite spiral stirrup confined concrete column; fcc1 is the peak stress of the concrete in the dual confinement area; A.sub.1 is the area of the dual confinement area; n.sub.1 is the number of the longitudinal bars of the dual confinement area; ƒ.sub.cc2 is the peak stress of the con concrete in the single confinement area; A.sub.2 is the area of the single confinement area; n.sub.2 is the number of the longitudinal bars in the single confinement area; A.sub.bar is the sectional area of a single longitudinal bar; n is the total number of the longitudinal bars; ε.sub.bar is the limit compressive strain of the FRP bar; and E.sub.bar is the modulus of elasticity of the FRP bar.

8. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 7, wherein the values of the limit compressive strains E.sub.bar of the FRP bar are taken as 1.3%, 1.2%, and 0.7% according to the slenderness ratios of 6, 10, and 15, and the values of other slenderness ratios are taken according to interpolation.

9. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 4, wherein the FRP square stirrup and the FRP spiral stirrup use one or more of Glass Fiber Reinforced Polymer/Plastic (GFRP) bars, Carbon Fiber Reinforced Polymer/Plastic (CFRP) bars, Basalt Fiber Reinforced Polymer/Plastic (BFRP) bars, and Aramid Fiber Reinforced Polymer/Plastic (AFRP) bars.

10. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 4, wherein the longitudinal bars use one of steel bars, the GFRP bars, the CFRP bars, the BFRP bars, and the AFRP bars, or mixed bars of the steel bars and FRP bars.

11. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 9, wherein in step five, a formula for calculating the effective lateral confinement stress of the FRP spiral stirrup is as follows: $f_1{}^{\text{'}}=k_e\frac{2f_{\text{fb}}{A}_{\text{f}}}{S{d}_{\text{s}}}$ in the formula, f .sub.fb is a smaller value of the bending strength of the spiral stirrup and 0.004E .sub.ft .sup., and E .sub.ft is the tensile modulus of elasticity of a reinforcement material; A.sub.f is the sectional area of the spiral stirrup; S is the spacing between stirrups; d.sub.c, is the diameter between the middle lines of the spiral stirrups; k.sub.e is an effective confinement coefficient; a formula for calculating the effective confinement coefficient k.sub.e of the FRP spiral stirrup is as follows: $k_e=\frac{A_e}{A_{cc}}=\frac{1-\frac{S^{\text{'}}}{2d_s}}{1-{\rho }_{cc}}$ in the formula, A.sub.cc is the area of the concrete enclosed by the middle lines of the spiral stirrups and does not comprise the area of the longitudinal bars; A.sub.e is the effective confinement area of the effectively confined core concrete; S′ is the clear distance between stirrups; and P.sub.cc is the ratio of the area of the longitudinal bars to the sectional core area.

12. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 10, wherein in step five, a formula for calculating the effective lateral confinement stress of the FRP spiral stirrup is as follows: $f_1{}^{\text{'}}=k_e\frac{2f_{\text{fb}}{A}_{\text{f}}}{S{d}_{\text{s}}}$ in the formula, f.sub.fb is a smaller value of the bending strength of the spiral stirrup and 0.004E .sub.ft .sup., and E .sub.ft is the tensile modulus of elasticity of a reinforcement material; A.sub.f is the sectional area of the spiral stirrup; S is the spacing between stirrups; d.sub.s, is the diameter between the middle lines of the spiral stirrups; k.sub.e is an effective confinement coefficient; a formula for calculating the effective confinement coefficient k.sub.e of the FRP spiral stirrup is as follows: $k_e=\frac{A_e}{A_{cc}}=\frac{1-\frac{S^{\text{'}}}{2d_s}}{1-{\rho }_{cc}}$ in the formula, A.sub.cc is the area of the concrete enclosed by the middle lines of the spiral stirrups and does not comprise the area of the longitudinal bars; A.sub.e is the effective confinement area of the effectively confined core concrete; S′ is the clear distance between stirrups; and p.sub.cc is the ratio of the area of the longitudinal bars to the sectional core area.

13. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 9, wherein in step five, for the FRP square stirrup, the lateral confinement stress generated by the same in a horizontal plane is unevenly distributed; a confining force reaches the maximum at the longitudinal bar; an arch-shaped “ineffective confinementarea” between two adjacent longitudinal bars is in a quadratic parabola shape; the area of the parabola is $w_i^2/6,$ wi′16, wherein W.sub.i is the clear distance between the two adjacent longitudinal bars; the square stirrup also has an arch-shaped “ineffective confinement area” in the vertical direction; so, for the FRP square stirrup, a process for calculating the effective lateral confinement stress f.sub.2’ is as follows: ${{\displaystyle f}}_2^{\text{'}}=\frac{{{\displaystyle f}}_{1\text{x}}^{\text{'}}+{{\displaystyle f}}_{1\text{y}}^{\text{'}}}{2}$ wherein, $f_{1\text{x}}^{{}^1}=k_{\text{e}}{\rho }_{\text{x}}{f}_{\text{fb}}=k_{\text{e}}\frac{A_{\text{sx}}}{S{d}_{\text{c}}}{f}_{\text{fb}}$ $f_{\text{ly}}^{\text{'}}=k_{\text{e}}{\rho }_{\text{x}}{f}_{\text{fb}}=k_{\text{e}}\frac{A_{\text{sy}}}{S{d}_{\text{c}}}{f}_{\text{fb}}$ in the formula, f.sub.lx’ is an effective lateral confinement stress in an x direction; f.sub.ly’ is an effective lateral confinement stress in a y direction; A.sub.sx is the total area of the stirrup in the x direction; A.sub.sy is the total area of the stirrup in the y direction; b.sub.c and d.sub.c, are distances of centerlines of the rectangular stirrup in two directions, respectively, where b.sub.c ≥d.sub.c; a formula for calculating the effective confinement coefficient k.sub.e of the FRP square stirrup is as follows: $k_{\text{e}}=\frac{A_{\text{e}}}{A_{\text{cc}}}=\frac{\left(1-{\displaystyle \underset{i=1}{\overset{n}{.Math.}}\frac{w_i^2}{6b_{\text{c}}{d}_{\text{c}}}}\right)\left(1-\frac{S^{{}^1}}{2b_{\text{c}}}\right)\left(1-\frac{S^{{}^1}}{2d_{\text{c}}}\right)}{\left(1-{\rho }_{\text{cc}}\right)}$ in the formula, n the number of the longitudinal bars.

14. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 10, wherein in step five, for the FRP square stirrup, the lateral confinement stress generated by the same in a horizontal plane is unevenly distributed; a confining force reaches the maximum at the longitudinal bar; an arch-shaped “ineffective confinementarea” between two adjacent longitudinal bars is in a quadratic parabola shape; the area of the parabola is $w_i^2/6,$ wi′16, wherein W.sub.i is the clear distance between the two adjacent longitudinal bars; the square stirrup also has an arch-shaped “ineffective confinement area” in the vertical direction; so, for the FRP square stirrup, a process for calculating the effective lateral confinement stress f.sub.2’ is as follows: $f_2^1=\frac{f_{\text{lx}}^1+f_{\text{ly}}^1}{2}$ wherein, $f_{1\text{x}}^{{}^1}=k_{\text{e}}{\rho }_{\text{x}}{f}_{\text{fb}}=k_{\text{e}}\frac{A_{\text{sx}}}{S{d}_{\text{c}}}{f}_{\text{fb}}$ $f_{1\text{x}}^{{}^1}=k_{\text{e}}{\rho }_{\text{x}}{f}_{\text{fb}}=k_{\text{e}}\frac{A_{\text{sx}}}{S{d}_{\text{c}}}{f}_{\text{fb}}$ in the formula, f.sub.lx’ is an effective lateral confinement stress in an x direction; f.sub.ly’ is an effective lateral confinement stress in a y direction; A.sub.sx is the total area of the stirrup in the x direction; Asy is the total area of the stirrup in the y direction; b.sub.c and d.sub.c, are distances of centerlines of the rectangular stirrup in two directions, respectively, where b.sub.c ≥ d.sub.c; a formula for calculating the effective confinement coefficient k.sub.e of the FRP square stirrup is as follows: $k_{\text{e}}=\frac{A_{\text{e}}}{A_{\text{cc}}}=\frac{\left(1-{\displaystyle \underset{i=1}{\overset{n}{.Math.}}\frac{w_i^2}{6b_{\text{c}}{d}_{\text{c}}}}\right)\left(1-\frac{S^{{}^1}}{2b_{\text{c}}}\right)\left(1-\frac{S^{{}^1}}{2d_{\text{c}}}\right)}{\left(1-{\rho }_{\text{cc}}\right)}$ in the formula, n the number of the longitudinal bars.

15. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 9, wherein in step six, when the composite spiral stirrup confinement model is made, in order to accurately reflect the actual confining effect of each stirrup, a composite spiral stirrup confinement area is divided into a dual confinement area and a single confinement area to accurately reflect the actual confining effect of each stirrup, wherein the dual confinement area is an area inside the spiral stirrup, and the single confinement area is an area from the spiral stirrup to the square stirrup; a peak stress expression of the concrete in the dual confinement area is as follows: $f_{cc1}=f_{co}\left(1.0+3.897{\left(\frac{f_d^{{}^1}}{f_{co}}\right)}^{0.737}\right)$ in the formula, f.sub.ccl is the peak stress of the concrete in the dual confinement area; f.sub.co is the strength of confined concrete; f.sub.d’ is the sum of the effective lateral confinement stresses of the spiral stirrup and the rectangular stirrup; a peak stress expression of the concrete in the single confinement area is as follows: $f_{cc2}=f_{co}\left(2.254\sqrt{1+\frac{7.94f_2\text{'}}{f_{co}}}-2\frac{f_2\text{'}}{f_{co}}-1.254\right)$ in the formula, f.sub.cc2 is the peak stress of the concrete in the single confinement area; f.sub.co is the strength of the confined concrete; f.sub.2’ is an effective lateral confinement stress of the FRP rectangular stirrup; finally, a formula for calculating the bearing capacity of the FRP composite spiral stirrup confined concrete column is as follows: $P_0=f_{cc1}\left(A_1-n_1{A}_{bar}\right)+f_{cc2}\left(A_2-n_2{A}_{bar}\right)+n{\epsilon }_{bar}{E}_{bar}{A}_{bar}$ in the formula, P.sub.0 is the bearing capacity of the FRP composite spiral stirrup confined concrete column; fcc1 is the peak stress of the concrete in the dual confinement area; A.sub.1 is the area of the dual confinement area; n.sub.1 is the number of the longitudinal bars of the dual confinement area; f.sub.cc2 is the peak stress of the con concrete in the single confinement area; A.sub.2 is the area of the single confinement area; n.sub.2 is the number of the longitudinal bars in the single confinement area; A.sub.bar is the sectional area of a single longitudinal bar; n is the total number of the longitudinal bars; E.sub.bar is the limit compressive strain of the FRP bar; and E.sub.bar is the modulus of elasticity of the FRP bar.

16. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 10, wherein in step six, when the composite spiral stirrup confinement model is made, in order to accurately reflect the actual confining effect of each stirrup, a composite spiral stirrup confinement area is divided into a dual confinement area and a single confinement area to accurately reflect the actual confining effect of each stirrup, wherein the dual confinement area is an area inside the spiral stirrup, and the single confinement area is an area from the spiral stirrup to the square stirrup; a peak stress expression of the concrete in the dual confinement area is as follows: $f_{cc1}=f_{co}\left(1.0+3.897{\left(\frac{f_d^{{}^1}}{f_{co}}\right)}^{0.737}\right)$ in the formula, ƒ.sub.cc1 is the peak stress of the concrete in the dual confinement area; f.sub.co is the strength of confined concrete; f.sub.d’ is the sum of the effective lateral confinement stresses of the spiral stirrup and the rectangular stirrup; a peak stress expression of the concrete in the single confinement area is as follows: $f_{cc2}=f_{co}\left(2.254\sqrt{1+\frac{7.94f_2\text{'}}{f_{co}}}-2\frac{f_2\text{'}}{f_{co}}-1.254\right)$ in the formula, f.sub.cc2 is the peak stress of the concrete in the single confinement area; f.sub.co is the strength of the confined concrete; f.sub.2’ is an effective lateral confinement stress of the FRP rectangular stirrup; finally, a formula for calculating the bearing capacity of the FRP composite spiral stirrup confined concrete column is as follows: $P_0=f_{cc1}\left(A_1-n_1{A}_{bar}\right)+f_{cc2}\left(A_2-n_2{A}_{bar}\right)+n{\epsilon }_{bar}{E}_{bar}{A}_{bar}$ in the formula, P.sub.0 is the bearing capacity of the FRP composite spiral stirrup confined concrete column; fccl is the peak stress of the concrete in the dual confinement area; A.sub.1 is the area of the dual confinement area; n.sub.1 is the number of the longitudinal bars of the dual confinement area; f.sub.cc2 is the peak stress of the con concrete in the single confinement area; A.sub.2 is the area of the single confinement area; n.sub.2 is the number of the longitudinal bars in the single confinement area; A.sub.bar is the sectional area of a single longitudinal bar; n is the total number of the longitudinal bars; E.sub.bar is the limit compressive strain of the FRP bar; and E.sub.bar is the modulus of elasticity of the FRP bar.

17. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 15, wherein the values of the limit compressive strains E.sub.bar of the FRP bar are taken as 1.3%, 1.2%, and 0.7% according to the slenderness ratios of 6, 10, and 15, and the values of other slenderness ratios are taken according to interpolation.

18. The compression design method for the FRP composite spiral stirrup confined concrete column according to claim 16, wherein the values of the limit compressive strains E.sub.bar of the FRP bar are taken as 1.3%, 1.2%, and 0.7% according to the slenderness ratios of 6, 10, and 15, and the values of other slenderness ratios are taken according to interpolation.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0067] FIG. 1 is a schematic structural diagram of the present disclosure;

[0068] FIG. 2 is a sectional view of an A-A directional plane in FIG. 1;

[0069] FIG. 3 is a transverse sectional view of an effective lateral confinement stress of an FRP spiral stirrup in the present disclosure;

[0070] FIG. 4 is a longitudinal partial sectional view of the effective longitudinal confinement stress of the FRP spiral stirrup in the present disclosure;

[0071] FIG. 5 is a transverse sectional view of the effective lateral confinement stress of an FRP square stirrup in the present disclosure;

[0072] FIG. 6 is a longitudinal partial sectional view of an effective longitudinal confinement stress of the FRP square stirrup in the present disclosure; and

[0073] FIG. 7 is a schematic diagram of a confinement area of the composite spiral stirrup in the present disclosure.

DETAILED DESCRIPTION OF THE EMBODIMENTS

[0074] Implementation modes of the present disclosure are described below through particular and specific embodiments. Other advantages and effects of the present disclosure can be easily understood by those skilled in the art from the content disclosed in the present specification.

[0075] The present disclosure provides an FRP composite spiral stirrup confined concrete column and a compression design method thereof, as shown in FIG. 1 to FIG. 7.

[0076] An FRP composite spiral stirrup confined concrete column includes an FRP composite spiral stirrup 1, longitudinal bars 2, and concrete 3. The longitudinal bars 2 include a central longitudinal bar 2-1 and corner longitudinal bars 2-2. The central longitudinal bar 2-1 is bound with the FRP composite spiral stirrup 1, and the corner longitudinal bars 2-1 are bound with a square stirrup to form a reinforcement skeleton. The reinforcement skeleton is arranged in the concrete 3. The FRP composite spiral stirrup 1 includes an internal FRP spiral stirrup 1-1 and an external FRP square stirrup 1-2. The diameter of the internal FRP spiral stirrup 1-1 is equal to the side length of the external FRP square stirrup 1-2. Each circle of FRP spiral stirrup is bound with an FRP square stirrup. Circumferential lateral confining force is provided by using the internal spiral stirrup, and a square stirrup is arranged externally, which can not only change the cross section into a square to enlarge the application range of the column, but also work together with the internal spiral stirrup to realize “dual confinement”.

[0077] The FRP square stirrup 1-1 and the FRP spiral stirrup 1-2 use one or more of Glass Fiber Reinforced Polymer/Plastic (GFRP) bars, Carbon Fiber Reinforced Polymer/Plastic (CFRP) bars, Basalt Fiber Reinforced Polymer/Plastic (BFRP) bars, and Aramid Fiber Reinforced Polymer/Plastic (AFRP) bars. The longitudinal bars use steel bars, the GFRP bars, the CFRP bars, the BFRP bars, and the AFRP bars, or mixed reinforcing bars of the steel bars and the FRP bars. According to the corrosive environment conditions of the working conditions from ordinary to severe, the steel bars, mixed reinforcing bars of the steel bars and the FRP, and full FRP longitudinal bars are selected in sequence, so as to meet the requirement of durability, and reduce the structural cost.

[0078] A compression design method for the FRP composite spiral stirrup confined concrete column includes the following steps.

[0079] Step one: the column is applied to a marine environment, so as to determine the environment type of an area where the column is located and the action grade thereof, and perform a durability design on members under different design service lives and corresponding limit states.

[0080] Step two: an overall scheme and a structural form are worked out according to design requirements, and sectional dimensions of the FRP composite spiral stirrup confined concrete column are determined preliminarily with reference to the existing design and relevant data.

[0081] Step three: the maximum design bearing capacity of a control cross section of the column under the design service life and the limit state is calculated according to the worked outbuilding scale of a building structure, the position where the column is located, and a set load feature.

[0082] Step four: the configurations of longitudinal bars and stirrups are worked out preliminarily according to the preliminarily worked out sectional dimensions, the maximum design bearing capacity under the limit state, and the reinforcement requirements in a specification.

[0083] Step five: effective lateral confinement stresses of the internal FRP spiral stirrup and the external FRP square stirrup are determined.

[0084] Step six: a composite spiral stirrup confinement model is made, and the limit bearing capacity of the FRP composite spiral stirrup confined concrete column is calculated.

[0085] In step five, the effective lateral confinement stresses of the internal FRP spiral stirrup and the external FRP square stirrup are calculated. In order to express the confining effect of the stirrup more accurately, the effective lateral confinement stresses of the two stirrups are respectively calculated according to the situation that both the spiral stirrup confined concrete and the square stirrup confined concrete have an effective confinement area, as shown in FIG. 3.

[0086] Firstly, for the effective lateral confinement stress of the FRP spiral stirrup, the radial pressure generated by the FRP spiral stirrup in the horizontal plane is evenly distributed, and the FRP spiral stirrup has an arch-shaped “ineffective confinement area” in the vertical direction, and the boundary of the ineffective confinement area is in a quadratic parabola shape. Therefore, a formula for calculating the effective lateral confinement stress fl′ of the FRP spiral stirrup is as follows:

[00010]$f_1^{\text{'}}=k_{\text{e}}\frac{2f_{\text{fb}}{A}_{\text{f}}}{S{d}_{\text{s}}}$

[0087] In the formula, f.sub.fb is a smaller value of the bending strength of the spiral stirrup and 0.004E.sub.ft; [0088] A.sub.f is the sectional area of the spiral stirrup; [0089] S is the spacing between stirrups; [0090] d.sub.s is the diameter between the middle lines of the spiral stirrups; [0091] k.sub.e is an effective confinement coefficient;a formula for calculating the effective confinement coefficient k.sub.e of the FRP spiral stirrup is as follows:

[00011]$k_{\text{e}}=\frac{A_{\text{e}}}{A_{\text{cc}}}=\frac{\text{1-}\frac{S^{\text{'}}}{2d_{\text{s}}}}{1-{\rho }_{\text{cc}}}$

[0092] In the formula, A.sub.cc is the area of the concrete enclosed by the middle lines of the spiral stirrups and does not include the area of the longitudinal bars; [0093] A.sub.e is the area of the effectively confined core concrete; [0094] S′ is the clear distance between stirrups; and [0095] p.sub.cc is the ratio of the area of the longitudinal bars to the sectional core area.

[0096] Secondly, for the FRP square stirrup, the lateral confinement stress generated by the same in a horizontal plane is unevenly distributed; a confining force reaches the maximum at the longitudinal bar; an arch-shaped “ineffective confinement area” between two adjacent longitudinal bars is in a quadratic parabola shape; the area of the parabola is w.sub.i.sup.2/6, where w.sub.i is the clear distance between the two adjacent longitudinal bars; and a rectangular stirrup also has an arch-shaped “ineffective confinement area” in the vertical direction.

[0097] So, for the FRP square stirrup, the effective lateral confinement stress f.sub.2’ of the FRP square stirrup can be calculated according to the following formula::

[00012]$f_2^{\text{'}}=\frac{f_{\text{1}\text{}\text{x}}^{\text{'}}+f_{\text{1}\text{}\text{y}}^{\text{'}}}{2}$

where,

[00013]$f_{1\text{}\text{x}}^{\text{'}}=k_{\text{e}}{\rho }_{\text{x}}{f}_{\text{fb}}=k_{\text{e}}\frac{A_{\text{sx}}}{S{d}_{\text{c}}}{f}_{\text{fb}}$

[00014]$f_{1\text{}\text{y}}^{\text{'}}=k_{\text{e}}{\rho }_{\text{y}}{f}_{\text{fb}}=k_{\text{e}}\frac{A_{\text{sy}}}{S{b}_{\text{c}}}{f}_{\text{fb}}$

[0098] In the formula, f.sub.lx’ is an effective lateral confinement stress in an x direction; [0099] f.sub.ly’ is an effective lateral confinement stress in a y direction; [0100] A.sub.sx is the total area of the stirrup in the x direction; [0101] A.sub.sy is the total area of the stirrup in the y direction; [0102] b.sub.c and d.sub.c are distances of centerlines of the rectangular stirrup in two directions, respectively, where b.sub.c ≥ d.sub.c;a formula for calculating the effective confinement coefficient k.sub.e of the FRP square stirrup is as follows:

[00015]$k_{\text{e}}=\frac{A_{\text{e}}}{A_{\text{cc}}}=\frac{\left(1-{\displaystyle \underset{i=1}{\overset{n}{.Math.}}\frac{w_i^2}{6b_{\text{c}}{d}_{\text{c}}}}\right)\left(1-\frac{S^{\text{'}}}{2b_{\text{c}}}\right)\left(1-\frac{S^{\text{'}}}{2d_{\text{c}}}\right)}{\left(1\text{-}{\rho }_{\text{cc}}\right)}$

[0103] In the formula, n is the number of the longitudinal bars.

[0104] In step six, when the composite spiral stirrup confinement model is made, confining mechanisms of the two types of stirrups to the concrete in different areas are analyzed, and a method for calculating the bearing capacity of the composite spiral stirrup confined column is proposed.

[0105] The composite spiral stirrup confinement model: a composite stirrup confinement area is innovatively divided into a dual confinement area (i.e., an area inside a spiral stirrup, an area 14 as shown in FIG. 4) and a single confinement area (i.e., an area from the spiral stirrup to the rectangular stirrup, an area 13 as shown in FIG. 4), such that an actual confining effect of each stirrup can be reflected accurately. By the confinement model as shown in FIG. 4, the contribution of different confinement areas to the bearing capacity of the column is calculated separately.

[0106] For the peak stress of the concrete in the dual confinement area, the ratio f.sub.cc / f.sub.co of the peak stress of the confined concrete to the peak stress of the unconfined concrete has a strong nonlinear correlation with the confining ratio f.sub.l′/ f.sub.co. Fitting is performed according to test data, so as to obtain a peak stress expression of the FRP stirrup confined concrete strength model:

[00016]$f_{cc1}=f_{co}\left(1.0+3.897{\left(\frac{f_d^{\text{'}}}{f_{\text{co}}}\right)}^{0.737}\right)$

[0107] In the formula, f.sub.cc1 is the peak stress of the concrete in the dual confinement area; [0108] f.sub.co is the strength of unconfined concrete; and [0109] f.sub.d’ is the sum of the effective lateral confinement stresses of the spiral stirrup and the rectangular stirrup.

[0110] For the peak stress of concrete in the single confinement area: in the single confinement area, the concrete is only confined by the rectangular stirrup; the effective lateral confinement stresses in two directions of a cross section are the same; and a formula for calculating the peak stress of the stirrup confined concrete is as follows:

[00017]$f_{cc2}=f_{co}\left(2.254\sqrt{1+\frac{7.94f_2\text{'}}{f_{co}}}-2\frac{f_2\text{'}}{f_{co}}-1.254\right)$

[0111] In the formula, f.sub.cc2 is the peak stress of the concrete in the single confinement area; [0112] f.sub.co is the strength of unconfined concrete; and [0113] f.sub.2’ is an effective lateral confinement stress of the FRP rectangular stirrup.

[0114] Finally, the bearing capacity of the composite spiral stirrup confined column considers the contribution of three pieces of concrete with different confining effects and longitudinal bars. A formula for calculating the bearing capacity P.sub.0 of the FRP composite spiral stirrup confined concrete column is as follows:

[00018]$P_0=f_{cc1}\left(A_1-n_1{A}_{bar}\right)+f_{cc2}\left(A_2-n_2{A}_{bar}\right)+n{\epsilon }_{bar}{E}_{bar}{A}_{bar}$

[0115] In the formula, P.sub.0 is the bearing capacity of the FRP composite spiral stirrup confined concrete column; [0116] f.sub.cc1 is the peak stress of the concrete in the dual confinement area; [0117] A.sub.1 is the area of the dual confinement area; [0118] n.sub.1 is the number of the longitudinal bars of the dual confinement area; [0119] f.sub.cc2 is the peak stress of the con concrete in the single confinement area; [0120] A.sub.2 is the area of the single confinement area; [0121] n.sub.2 is the number of the longitudinal bars in the single confinement area; [0122] A.sub.bar is the sectional area of a single longitudinal bar; [0123] n is the total number of the longitudinal bars; [0124] ε.sub.bar is the limit compressive strain of the FRP bar; and [0125] E.sub.bar is the modulus of elasticity of the FRP bar.

[0126] Where, ε.sub.bar is the limit compressive strain of the FRP bar. The values of the limit compressive strains are 1.3%, 1.2%, and 0.7% according to the slenderness ratios of 6, 10, and 15, and the values of other slenderness ratios are taken according to interpolation. E.sub.bar is the modulus of elasticity of the FRP bar, and the value thereof is 46.3 GPa.

[0127] A method for pouring the FRP composite spiral stirrup confined concrete column is as follows:

[0128] First, the FRP spiral stirrup (1-1) is bound to the central longitudinal bar (2-1), and simultaneously, the spacing between the FRP spiral stirrups is adjusted according to a design requirement. Then, the FRP square stirrup (1-2) is bounded, and finally, the corner longitudinal bars (2-2) are bound to the corners of the FRP square stirrup (1-2). Therefore, reinforcement skeleton with the confinement of the FRP composite spiral stirrups is obtained.

[0129] In the present embodiment, in order to ensure that the concrete between the FRP spiral stirrup (1-1) and the FRP square stirrup (1-2) is also effectively confined. The FRP square stirrup is a closed stirrup, and is formed by lapping two ends. A lap joint is located at a right angle of the square stirrup. The four bending angles are all 90°. The lapping length needs to be 12 times greater than the diameter of the stirrup, so as to meet the effective lapping length, and ensure that the FRP square stirrup 2 can provide effective confinement under a high stress.

[0130] High-strength concrete (3) is the concrete with the compressive strength of C60, and in order to support a framework for the bound reinforcement skeleton, the set thickness of a protective layer reserved at an edge is 25 mm. The high-strength concrete 3 may be poured in a vertical or horizontal mode.

[0131] The FRP bars are selected from GFRP bars, which have the characteristics of light weight, high strength, corrosion resistance, fatigue resistance, and higher cost performance relative to other FRP bars.

[0132] According to the actual design requirements, proper diameter of the FRP bar and dimensions of the spiral stirrup and the square stirrup are selected, and the diameter of the FRP spiral stirrup is equal to the side length of the FRP square stirrup (±5 mm), which can ensure accurate binding of the two types of stirrups, thereby providing “dual confinement” for the core concrete, and improving the bearing capacity and the ductility of the concrete column.

[0133] The accuracy of the method for calculating the bearing capacity the FRP composite spiral stirrup confined concrete column proposed by the present disclosure is further proved below by design examples.

[0134] In order to avoid the eccentric pressure of a column body caused by a long column, the dimensions of column to be designed is 300 mm×300 mm×900 mm, the thickness of the protective layer is 25 mm, the longitudinal bars are eight GFRP bars with the diameter of 16 mm; the diameter of the GFRP stirrup is 8 mm; and the spacing between the stirrups is 50, 100, and 150 mm. The form of a composite spiral stirrup (internal spiral stirrups and external rectangular spiral stirrups) is used. The concrete strength grade is C60.

[0135] Now, two traditional calculation methods for calculating a spiral stirrup column and the calculation method proposed by the present disclosure are used for comparative analysis, and the accuracy is verified by corresponding test data:

[0136] First, a formula for overall calculation of the bearing capacity of the column and a calculation result without considering a confinement area are as follows:

[00019]$P_0=0.85{f^{\prime }}_c\left(A_g-A_s\right)+0.02E_f{A}_s$

[0137] In the formula, f.sub.c’ is the effective lateral confinement stress of the spiral stirrup and the rectangular stirrup; A.sub.g is the sectional area; A.sub.s is the sectional area of a longitudinal bar; and E.sub.f is a modulus of elasticity of the GFRP longitudinal bar.

[0138] It is calculated that the bearing capacity of the column is 3241KN under the three stirrup spacings of 50 mm, 100 mm, and 150 mm.

[0139] Second, a calculation formula and a result obtained by using the effective confinement model of the spiral stirrup without distinguishing the dual confinement area and the single confinement area are as follows:

[00020]$P_0=f_{cc1}\left(A_1-n{A}_{bar}\right)+n{\epsilon }_{bar}{E}_{bar}{A}_{bar}$

[0140] f.sub.cc1 In the formula, f.sub.cc1 is to perform even summation on the effective lateral confinement stresses of a simple spiral stirrup and the rectangular stirrup.

[0141] It is calculated that the bearing capacity of the column is 5296KN, 4383KN, and 4136KN respectively under the three stirrup spacings of 50 mm, 100 mm, and 150 mm.

[0142] Third, a formula and a calculation result obtained by using the composite spiral stirrup confinement model proposed by the present disclosure and distinguishing the actual confining effects of different areas are as follows:

[00021]$P_0=f_{cc1}\left(A_1-n_1{A}_{bar}\right)+f_{cc2}\left(A_2-n_2{A}_{bar}\right)+n{\epsilon }_{bar}{E}_{bar}{A}_{bar}$

[0143] It is calculated that the bearing capacity of the column is 4926KN, 4006KN, and 3843KN respectively under the three stirrup spacings of 50 mm, 100 mm, and 150 mm.

[0144] It is calculated that the bearing capacity of the column is 5016KN, 4083KN, and 3943KN respectively under the three stirrup spacings of 50 mm, 100 mm, and 150 mm.

[0145] It can be known from the comparison with the test data that the average errors of the three calculation methods under different stirrup spacings are respectively 75.39%, 106.5%, and 97.93%. Therefore, the bearing capacity calculated by using the composite spiral stirrup confinement model proposed by the present disclosure is the most accurate, and a smaller value is beneficial to retaining the bearing allowance for the practical engineering.

[0146] Finally, it is to be noted that the above embodiments are merely used to illustrate the technical solutions of the present disclosure, and are not intended to limit the present disclosure. Although the present disclosure has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that the technical solutions described in the foregoing embodiments are modified, or some technical features are equivalently replaced. However, these modifications and replacements do not make the essence of the corresponding technical solutions depart from the spirit and scope of the technical solutions of various embodiments of the present disclosure.

[0147] In the descriptions of the present disclosure, it is to be understood that an orientation or positional relationship indicated by the terms “front”, “back”, “left”, “right”, “center”, and the like is an orientation or positional relationship shown in the drawings, and is merely for the convenience of describing the present disclosure and simplifying the description, rather than indicating or implying that the device or elements referred to have a particular orientation, and configure and operate for the particular orientation. Thus, it cannot be construed as limiting the scope of protection of the present disclosure.