# Earthquake Response Control of Double-Layer Truss Walls by means of Innovative Fuse Connections

Authors: Koichiro Ishikawa
Journal: Advances in Civil Engineering
 (2018)

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## Abstract

This study deals with partial cylindrical truss walls equipped with damper connections due to horizontal earthquake motions. The damper connection consists of an aluminum ball joint, an aluminum hub, and a steel bolt. A ductile elongation of the steel bolt due to a tensile stress is expected by avoiding the brittle collapse. The study proposes a fuse-type connection by means of yield of the steel bolt due to tension stress realized by the ductile failure collapse mechanism of the wall-type spatial structure. The proposed truss wall with the fuse-type connection can realize a deformation of nodes within the restriction for avoiding a nonstructural member damage. It is confirmed in the dynamic elastoplastic analysis that the control of the dynamic collapse mechanism such as the steel bolt elongation can avoid a brittle collapse mechanism such as a chain of member buckling. The evaluation method is also proposed by means of the limit displacement considering a ductility factor of the steel bolt within 2.0.


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## Body

## 1. Introduction

This study deals with the dynamic elastoplastic analysis considering a member buckling, and the fuse-type connection consists of an aluminum ball joint, an aluminum hub, and a steel bolt. A ductile elongation of the steel bolt due to a tensile stress is expected by avoiding the brittle collapse in our previous paper [1–3]. The study proposes a fuse-type connection by means of yield of the steel bolt due to tension stress realized by the ductile failure collapse mechanism of the wall-type spatial structure.The seismic response characteristics of spatial structures such as roof and wall types depend on their form and support conditions, and several reviews [4, 5] and guidelines [6–13] quoting many studies have been published depending on the performance of building structures. Several performance prediction methods have been developed for this purpose; however, the earthquake resistance capacity of spatial structures requires the variation of the form and the support condition, and it is very difficult to apply them to wall-type spatial structures. For the performance design, several prediction methods such as a pushover analysis and an adaptive capacity spectrum method have been developed for structures such as buildings and bridges [14–18].The control of the dynamic collapse mechanism is also proposed to improve the earthquake resistance capacity by a damper connection such as the steel bolt elongation.Effect of the member buckling and yield elongation of the steel bolt on the seismic response out of the plane is shown in comparison with the response of the wall structure subjected to the horizontal earthquake motions. The earthquake evaluation method is also proposed considering the dynamic collapse mechanism. A validity of the proposed method is shown by means of the accuracy between the analysis and the estimation.


## 2. Examples of Aluminum Truss Structures

Since earthquake resistance standards in Japan were improved, buildings which were designed on the basis of old seismic standards before 1981 need to be reinforced quickly on the basis of the exiting new ones.The aluminum braces are useful for seismic retrofitting of existing buildings because they achieve good workability in the erection site and reduce the seismic loading and additional loads on the foundations due to their lightweight and aluminum alloy members owing to their long-term corrosion resistance.Figure1 shows double-layer latticed walls and roofs made of an aluminum alloy truss system, and the walls resist in-plane shearing load in an earthquake. Figures 1(a) and 1(b) show the entrance canopy of the office and the atrium at the entrance of the railroad station, and they are L-shaped application of an aluminum truss wall. The truss walls achieve structural rigidity and strength on seismic loading, and the slender members with cladding prevent daylight. Figures 1(c) and 1(d) are CG images of seismic retrofit of RC school buildings using the aluminum truss walls.Figure 1
Aluminum truss walls and retrofit.
(a)
(b)
(c)
(d)


## 3. Connection Design of an Aluminum Truss Wall

We propose two types of connection systems: an aluminum ball-jointed truss wall and aluminum pin-connected braces. As described in more detail below, both systems have improved in their plastic deformability to resist excessive seismic loads. In our previous paper [1], the brittle collapse mechanism of the truss wall structure to resist lateral loads has been investigated to evaluate the earthquake resistance capacity.Figure2 illustrates the aluminum alloy ball-jointed truss connection used to retrofit; this nodal connection consists of aluminum parts and a steel bolt. All aluminum parts are extruded, and in heat-treated aluminum alloy 6061-T6, the end plug is welded at its edge to the strut by using a friction welding method. Friction welding, which is one of the various welding processes, is known for high joint efficiency and high reliability in comparison with MIG or TIG welding. The collar transfers the compression stress, and the steel bolt transfers the tension stress. The bolt is made of high-strength steel; the figure of the bolt is slimmed in the axle of the bolt as shown in Figure 2.Figure 2
Yielding bolt mechanism.The connection of the truss wall is designed by means of the condition such asNcr>NBu, where Ncr is a member buckling or an ultimate strength of the welded joint and NBu is an ultimate strength of the bolt. The bolts are able to extend by excessive tensile loading in a major earthquake; therefore, the truss wall structure achieves a good hysteretic curve as described in Figure 3. In our previous paper [2], it is investigated that the fuse-type connection realizes the tension yield of the steel bolt before the member buckling occurs.Figure 3
Hysteretic curve of the truss wall used to retrofit.


## 4. Truss Members including Joints and Modeling

The fuse connection consists of two hubs, two collars, two bolts, and a strut, as shown in Figure4. The steel bolt resists against the tension axial stress, and the collar resists against the compression axial stress, as far as the resistance mechanism of the axial stress between the hub and strut is concerned. Figures 5–7 show the numerical analysis model in this study.Figure 4
Truss system.Figure 5
Mechanism of stress transfer.Figure 6
Components of the member.Figure 7
Truss model of each element for analysis.


## 5. Hysteresis Models of the Truss Member

The present analysis adopts an assumption that struts buckle due to compression and yield under tension. Figure8 shows the hysteresis curves used for the slenderness ratio of a member. The maximum compressive stress σcr is determined using (1) which considers member crookedness and the residual stresses existing in the strut. Figure 9 shows the hysteresis curves of the steel bolt which yields under tension and slips under compression. The hub resists against the compression instead of the yielding bolt. The yield stress σy and Young’s modulus E are taken to be 210 MPa and 70 GPa, respectively. The maximum compressive stress σcr is calculated by (1), and the maximum tension stress of the weld fracture is taken to be 0.71σy due to a tension axial stress. The initial tension stress is not introduced in the steel bolt:(1)λΛ≤1.0:σcr=F1−0.5λ/Λ2,λΛ>1.0:σcr=F2λ/Λ2,Λ=π2E0.5F=37.17F=81.1.Figure 8
Hysteresis model of the aluminum strut.Figure 9
Hysteresis model of the steel bolt.


## 6. Time-History Analysis of the Truss Wall

Geometric and material nonlinearity is considered in the time-history analysis of the truss walls subjected to the horizontal earthquake motion of El Centro NS (PGA: 5.61 m/sec2). The Rayleigh damping matrix is used in this analysis. The damping factor h = 0.02 is used for first and second vibration modes in the damping matrix. The numerical integration method uses the Newmark method. β = 1/4 is used in this study because β = 1/4 will be unconditionally stable for the seismic response analysis.


### 6.1. Analysis Model of the Double-Layer Partial Cylindrical Truss Wall

The truss wall has a configuration as shown in Figure10. The length is 14 m with 7 grids, and the height is 7.2 m with 4 grids. The bottom nodes are constrained for all directions. The top nodes are free for the horizontal plane (X direction). They are restrained for the vertical direction (Y direction) and out of the plane (Z direction).Figure 10
Analysis model of the double-layer partial cylindrical truss wall.An aluminum alloy A6061-T6 is used in the strut, and a high tensile strength steel SCM435 with the yield strength of 649 N/mm2 is used in the connection steel bolt. A truss model is used in the analysis. The model is a lightweight structure made of an aluminum alloy. The structure can bear the dead load, which is confirmed as the static design.Table1 shows the member length L (mm), the slenderness ratio λ, the cross-sectional secondary radius i (mm), and the sectional area A (mm2). The member is determined by the earthquake-proof design using the base shear coefficient of 1.0. And the strength of pullout of the bolt such as the yield axial force is also shown in Table 1.Table 1
Member characteristics of the truss wall.
Wall depth: 1.0 m
Strut (mm)
Sectional area (mm2)
Cross-sectional secondary radius (mm)
Member length (mm)
Slenderness ratio/limit slenderness ratio
Chord member ofX direction
ϕ180 × t21
10489.8
56.7
1705
0.367
Chord member ofY direction
ϕ180 × t21
10489.8
56.7
1400
0.305
Web member
ϕ150 × t12
5202.5
49.0
1162
0.240
Bolt (mm)
Sectional area (mm2)
Member length (mm)
Minimum elongation (%)
Yield axial force (kN)
Chord member ofX direction
ϕ30.0
706.9
200
16
452.3
Chord member ofY direction
ϕ30.0
706.9
200
16
452.3
Web member
ϕ15.0
254.5
267
16
162.9
Wall depth: 0.4 m
Strut (mm)
Sectional area (mm2)
Cross-sectional secondary radius (mm)
Member length (mm)
Slenderness ratio/limit slenderness ratio
Chord member ofX direction
ϕ180 × t21
10189.8
56.7
1705
0.367
Chord member ofY direction
ϕ180 × t21
10189.8
56.7
1400
0.305
Web member
ϕ150 × t12
5202.5
49.0
994
0.240
Bolt (mm)
Sectional area (mm2)
Member length (mm)
Minimum elongation (%)
Yield axial orce (kN)
Chord member ofX direction
ϕ30.0
706.9
200
16
452.3
Chord member ofY direction
ϕ30.0
706.9
200
16
452.3
Web member
ϕ15.0
254.5
228
16
162.9


### 6.2. Vibration Characteristics and Seismic Responses of the Truss Wall

The natural period and the vibration mode of the two walls with the 1 m and 0.4 m wall depths are obtained by means of the eigenvalue analysis, respectively. The first and third natural periodsT1 and T3 are shown in Figure 11. The corresponding vibration modes are also shown in Figure 11, respectively. It is seen that the shear deformation mode of a wall appears in the first vibration mode of the two walls and the third mode of the wall with the 1 m depth. The out-of-plane shape in the third mode of the wall with the 0.4 m depth also appears due to the lower bending rigidity than in the wall with the 1 m depth. The study focuses on the out-of-plane deformation of the thin depth wall subjected to earthquake motions.Figure 11
The first and third vibration modes and natural periods. (a) Wall depth: 1.0 m. (b) Wall depth: 0.4 m.
(a)
(b)


### 6.3. Dynamic Response Behavior of the Truss Walls Subjected to Earthquake Motions

In the present study, the earthquake resistance capacity of the dome is evaluated by investigating the maximum horizontal displacementδmax at the top of the wall subjected to horizontal earthquake motions with the peak ground acceleration (PGA) multiplied by the PGA amplification factor λE. The damage limit artificial earthquake motion with a phase characteristic of the El Centro NS wave is used in the seismic response analysis. The PGA is taken to be 1.12 m/sec2. The relationship between λE and δmax of the two walls with different wall depths is shown in Figures 12 and 13. The location of the steel bolt yield is shown in Figure 14 at the beginning of the bolt yield and the member buckling, respectively. It is seen in the results that the bolt yield precedes the member buckling and the linear relationship between λE and δmax is kept within the plastic region from the beginning of the bolt yield to the beginning of the member buckling. This means that the response control can be feasible by means of the fuse-type connection such as the steel bolt yielding elongation.Figure 12
λ
E and δmax of the wall depth with 1 m.Figure 13
λ
E and δmax of the wall depth with 0.4 m.Figure 14
Location of the bolt yield of the wall depth with 1 m and 0.4 m. (a) Case ofλE = 7.4 (1 m depth). (b) Case of λE = 9.4 (1 m depth). (c) Case of λE = 7.6 (0.4 m depth).
(a)
(b)
(c)The time-history energy response of the restoring force of the member and the damping of the structure to the in-plane (X) and out-of-plane (Z) directions is shown in Figures 15 and 16, respectively. It is seen in the wall with depths that the structural damping almost absorbs the input energy due to the seismic response just before the member buckling occurs. The member buckling induces the absorbed energy in the case of the wall with 1 m depth subjected to earthquake motions with λE = 9.4. The out-of-plane also consumes energy greater due to member buckling as seen in Table 2. On the contrary, a sudden dynamic collapse of the wall with the 0.4 m depth occurs just after the member buckling because of the bending rigidity out of the plane with the less wall depth.Figure 15
Time-history energy response of the restoring force of the member and the damping of the structure to the in-plane (X) direction component. (a) 1 m wall depth (λE = 7.4). (b) 0.4 m wall depth (λE = 7.6). (c) 1 m wall depth (λE = 9.4). RE = restoring force energy; DE = damping energy.
(a)
(b)
(c)Figure 16
Time-history energy response to the out-of-plane (Z) direction component. (a) 1 m wall depth (λE = 7.4). (b) 0.4 m wall depth (λE = 7.6). (c) 1 m wall depth (λE = 9.4). RE = restoring force energy; DE = damping energy.
(a)
(b)
(c)Table 2
Ratio of the total energy in the out-of-plane (Z) direction to that in the in-plane (X) direction.
Failure type
Wall depth (m)
λ
E
Consumption energy in the in-plane directionEi (kN·m)
Consumption energy in the out-of-plane directionEo (kN·m)
E
o/(Ei + Eo) (%)
Steel bolt yield
1.0
7.4
1937.8
30.33
1.54
0.4
7.6
1814.7
137.83
7.06
Member buckling
1.0
9.4
5588.6
790.69
12.39The maximum strains of the steel connection bolt in both depths are 2 times less than the first yield strain as shown in Figure17. It is confirmed in the study that all members in both walls are also 2 times less than the first yield strain.Figure 17
Relationship between stress and strain of the web member. (a) 1 m wall depth before the member buckling (λE = 7.4). (b) 0.4 m wall depth before the collapse (λE = 7.6).
(a)
(b)


## 6.1. Analysis Model of the Double-Layer Partial Cylindrical Truss Wall

The truss wall has a configuration as shown in Figure10. The length is 14 m with 7 grids, and the height is 7.2 m with 4 grids. The bottom nodes are constrained for all directions. The top nodes are free for the horizontal plane (X direction). They are restrained for the vertical direction (Y direction) and out of the plane (Z direction).Figure 10
Analysis model of the double-layer partial cylindrical truss wall.An aluminum alloy A6061-T6 is used in the strut, and a high tensile strength steel SCM435 with the yield strength of 649 N/mm2 is used in the connection steel bolt. A truss model is used in the analysis. The model is a lightweight structure made of an aluminum alloy. The structure can bear the dead load, which is confirmed as the static design.Table1 shows the member length L (mm), the slenderness ratio λ, the cross-sectional secondary radius i (mm), and the sectional area A (mm2). The member is determined by the earthquake-proof design using the base shear coefficient of 1.0. And the strength of pullout of the bolt such as the yield axial force is also shown in Table 1.Table 1
Member characteristics of the truss wall.
Wall depth: 1.0 m
Strut (mm)
Sectional area (mm2)
Cross-sectional secondary radius (mm)
Member length (mm)
Slenderness ratio/limit slenderness ratio
Chord member ofX direction
ϕ180 × t21
10489.8
56.7
1705
0.367
Chord member ofY direction
ϕ180 × t21
10489.8
56.7
1400
0.305
Web member
ϕ150 × t12
5202.5
49.0
1162
0.240
Bolt (mm)
Sectional area (mm2)
Member length (mm)
Minimum elongation (%)
Yield axial force (kN)
Chord member ofX direction
ϕ30.0
706.9
200
16
452.3
Chord member ofY direction
ϕ30.0
706.9
200
16
452.3
Web member
ϕ15.0
254.5
267
16
162.9
Wall depth: 0.4 m
Strut (mm)
Sectional area (mm2)
Cross-sectional secondary radius (mm)
Member length (mm)
Slenderness ratio/limit slenderness ratio
Chord member ofX direction
ϕ180 × t21
10189.8
56.7
1705
0.367
Chord member ofY direction
ϕ180 × t21
10189.8
56.7
1400
0.305
Web member
ϕ150 × t12
5202.5
49.0
994
0.240
Bolt (mm)
Sectional area (mm2)
Member length (mm)
Minimum elongation (%)
Yield axial orce (kN)
Chord member ofX direction
ϕ30.0
706.9
200
16
452.3
Chord member ofY direction
ϕ30.0
706.9
200
16
452.3
Web member
ϕ15.0
254.5
228
16
162.9


## 6.2. Vibration Characteristics and Seismic Responses of the Truss Wall

The natural period and the vibration mode of the two walls with the 1 m and 0.4 m wall depths are obtained by means of the eigenvalue analysis, respectively. The first and third natural periodsT1 and T3 are shown in Figure 11. The corresponding vibration modes are also shown in Figure 11, respectively. It is seen that the shear deformation mode of a wall appears in the first vibration mode of the two walls and the third mode of the wall with the 1 m depth. The out-of-plane shape in the third mode of the wall with the 0.4 m depth also appears due to the lower bending rigidity than in the wall with the 1 m depth. The study focuses on the out-of-plane deformation of the thin depth wall subjected to earthquake motions.Figure 11
The first and third vibration modes and natural periods. (a) Wall depth: 1.0 m. (b) Wall depth: 0.4 m.
(a)
(b)


## 6.3. Dynamic Response Behavior of the Truss Walls Subjected to Earthquake Motions

In the present study, the earthquake resistance capacity of the dome is evaluated by investigating the maximum horizontal displacementδmax at the top of the wall subjected to horizontal earthquake motions with the peak ground acceleration (PGA) multiplied by the PGA amplification factor λE. The damage limit artificial earthquake motion with a phase characteristic of the El Centro NS wave is used in the seismic response analysis. The PGA is taken to be 1.12 m/sec2. The relationship between λE and δmax of the two walls with different wall depths is shown in Figures 12 and 13. The location of the steel bolt yield is shown in Figure 14 at the beginning of the bolt yield and the member buckling, respectively. It is seen in the results that the bolt yield precedes the member buckling and the linear relationship between λE and δmax is kept within the plastic region from the beginning of the bolt yield to the beginning of the member buckling. This means that the response control can be feasible by means of the fuse-type connection such as the steel bolt yielding elongation.Figure 12
λ
E and δmax of the wall depth with 1 m.Figure 13
λ
E and δmax of the wall depth with 0.4 m.Figure 14
Location of the bolt yield of the wall depth with 1 m and 0.4 m. (a) Case ofλE = 7.4 (1 m depth). (b) Case of λE = 9.4 (1 m depth). (c) Case of λE = 7.6 (0.4 m depth).
(a)
(b)
(c)The time-history energy response of the restoring force of the member and the damping of the structure to the in-plane (X) and out-of-plane (Z) directions is shown in Figures 15 and 16, respectively. It is seen in the wall with depths that the structural damping almost absorbs the input energy due to the seismic response just before the member buckling occurs. The member buckling induces the absorbed energy in the case of the wall with 1 m depth subjected to earthquake motions with λE = 9.4. The out-of-plane also consumes energy greater due to member buckling as seen in Table 2. On the contrary, a sudden dynamic collapse of the wall with the 0.4 m depth occurs just after the member buckling because of the bending rigidity out of the plane with the less wall depth.Figure 15
Time-history energy response of the restoring force of the member and the damping of the structure to the in-plane (X) direction component. (a) 1 m wall depth (λE = 7.4). (b) 0.4 m wall depth (λE = 7.6). (c) 1 m wall depth (λE = 9.4). RE = restoring force energy; DE = damping energy.
(a)
(b)
(c)Figure 16
Time-history energy response to the out-of-plane (Z) direction component. (a) 1 m wall depth (λE = 7.4). (b) 0.4 m wall depth (λE = 7.6). (c) 1 m wall depth (λE = 9.4). RE = restoring force energy; DE = damping energy.
(a)
(b)
(c)Table 2
Ratio of the total energy in the out-of-plane (Z) direction to that in the in-plane (X) direction.
Failure type
Wall depth (m)
λ
E
Consumption energy in the in-plane directionEi (kN·m)
Consumption energy in the out-of-plane directionEo (kN·m)
E
o/(Ei + Eo) (%)
Steel bolt yield
1.0
7.4
1937.8
30.33
1.54
0.4
7.6
1814.7
137.83
7.06
Member buckling
1.0
9.4
5588.6
790.69
12.39The maximum strains of the steel connection bolt in both depths are 2 times less than the first yield strain as shown in Figure17. It is confirmed in the study that all members in both walls are also 2 times less than the first yield strain.Figure 17
Relationship between stress and strain of the web member. (a) 1 m wall depth before the member buckling (λE = 7.4). (b) 0.4 m wall depth before the collapse (λE = 7.6).
(a)
(b)


## 7. Evaluation Method of the Response Estimation by means of the Limit Displacement

The comparison between the PGA amplification factorλE of the input earthquake motion and the maximum displacement δmax to the horizontal in-plane (X) direction at the top of the wall with the 1 m and 0.4 m wall depths is shown in Figure 18 by means of the dynamic analysis. And the proposed estimation method uses the limit displacement. The limit displacement δud is defined in the study as 1.2δy1 in the red line in Figure 18. The structural yield displacement δy1 is the horizontal in-plane displacement δ at the top of the wall just on the first occurrence of the steel bolt yield. It is also noticed that a ductility factor of the steel bolt is taken to be within 2.0 at the limit displacement δud. This is the reason that the limit displacement δud is taken to be 1.2δy1. The structural buckling displacement δy2 is the horizontal in-plane displacement δ at the top of the wall just on the first occurrence of the strut member buckling.Figure 18
Comparison between the limit displacement and the analysis. (a) 1 m wall depth. (b) 0.4 m wall depth.
(a)
(b)The evaluation method of the response estimation by means of the limit displacement is the first to calculate theδmax using the linear relationship between λE and δmax. It can be evaluated for engineers that the dynamic collapse occurs in the case of δmax larger than δud. The estimation value λEU is practically calculated by the proposed method using the response analysis. The proposed method can be applied to the wall with an aspect ratio of the shear-dominant deformation type.


## 8. Conclusions

This study deals with the partial cylindrical truss wall with the damper joint connection due to horizontal earthquake motions. It is confirmed in the dynamic elastoplastic analysis that the control of the dynamic collapse mechanism such as the steel bolt elongation can avoid a brittle collapse mechanism such as a chain of member buckling. Effect of the member buckling and yield elongation of the steel bolt on the seismic response out of the plane is also shown in comparison with the response of the wall structure subjected to the horizontal earthquake motions.The evaluation method is also proposed by means of the limit displacement considering a ductility factor of the steel bolt within 2.0. This means that the response control can be feasible by the damper connection such as the steel bolt elongation due to tension stress.



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*Source: 1425672-2018-08-15.xml*