# Damage Identification of a Derrick Steel Structure Based on the HHT Marginal Spectrum Amplitude Curvature Difference

Authors: Dongying Han; Shimin Wei; Peiming Shi; Ying Zhang; Kai Gao; Nengyuan Tian
Journal: Shock and Vibration
 (2017)

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## Abstract

For the damage identification of derrick steel structures, traditional methods often require high-order vibration information of structures to identify damage accurately. However, the high-order vibration information of structures is difficult to acquire. Based on the technology of signal feature extraction, only using the low-order vibration information, taking the right front leg as an example, we analyzed the selection of HHT marginal spectrum amplitude and the calculation process of its curvature in practical application, designed the damage conditions of a derrick steel structure, used the index and intrinsic mode function (IMF) instantaneous energy curvature method to perform the damage simulation calculation and comparison, and verified the effect of identifying the damage location in a noisy environment. The results show that the index can accurately determine the location of the damage element and weak damage element and can be used to qualitatively analyze the damage degree of the element; under the impact load, the noise hardly affects the identification of the damage location. Finally, this method was applied to the ZJ70 derrick steel structure laboratory model and compared with the IMF instantaneous energy curvature method. We verified the feasibility of this method in the damage location simulation experiment.


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## Body

## 1. Introduction

Derrick steel structures play an important role in the oil and gas exploration and development [1, 2]. During long-term service, because of various factors such as disassembly and corrosion, damage inevitably occurs, which gradually reduces the safety performance and carrying capacity of the derrick steel structures and forms security risks [3–5]. In recent years, the damage detection method based on structural signal feature extraction [6, 7] has attracted the attention of many scholars; this method mainly uses the vibration signal from the vibration sensors to collect structural damage. Using signal-processing methods, the appropriate damage-sensitive indicators are analyzed, and further structural-damage identification or health monitoring is realized [8].Huang et al. proposed Hilbert-Huang transform (HHT) method, which is a new, self-adaptive frequency analysis method [9], and included the empirical mode decomposition (EMD) and Hilbert transform (HT); the core is the EMD. Chen et al. used the instantaneous frequency of IMFs (intrinsic mode functions) as the component damage index of structure damage detection [10–12]. Pines and Salvino combined the EMD with Hilbert transform to obtain the phase of the component signals and used the phase information of different degrees of freedom to identify the structure damage [13]. Li et al. [14] used the method of wavelet analysis to analyze the maximum energy of the intrinsic mode functions (IMFs) component, which includes the wavelet coefficients for damage identification. Cheraghi and Taheri  [15] analyzed the energy of the IMF component signal, selected the effective characteristic information as the damage sensitivity index, and applied it to identify the pipeline structure damage. Rezaei and Taheri [16, 17] used the energy of the first-order IMF component after the decomposition of the signal EMD as a damage sensitivity index to diagnose the damage of the pipeline structure. Chen et al. proposed to show the status of damage material wing box of the material of the feature vector-relative variation of the instantaneous frequency [18]. Cao et al. [19] proposed a structural-damage early-warning method based on the EMD, where the structure before and after damage in the component of the IMF’s energy distribution changes as the damage-sensitive index, and applied the method to model Health Monitoring Benchmark structure damage identification. Ren et al. [20] applied the improved HHT method to the damage identification of engineering structures and proposed the method to identify the damage location of the structure using the structural before and after the damage in the first-order response to a first-order IMF feature energy ratio. Wang et al. applied the method to the bridge structure. The HHT theory has not been used in complex structures, such as derrick steel structures, but it has been used in simple structures in the literature [21]. Li et al. applied the method to the crack identification of the rotor [22]. This paper realized the damage identification of the derrick steel structure based on the HHT marginal spectrum amplitude curvature difference and only used a low-level vibration information structure. The simulation calculated the damage identification of the derrick and compared it with the IMF instantaneous energy curvature difference. Finally, the feasibility of the method was verified with derrick damage location simulation experiments.


## 2. HHT Marginal Spectrum Amplitude Curvature

### 2.1. HHT Theory

The HHT method consists of two parts: EMD and HT. The original signalx(t) is decomposed into a series of IMFs and a residual function by EMD:(1)xt=∑i=1nci+rn.Hilbert transformation of the IMF component:(2)c^i=1π∫-∞+∞ciτt-τdτ.Based on this function, the analytic signal is established, and the instantaneous amplitude and phase function are obtained:(3)zi=ci+jc^i=aiejφi,ai=ci2+c^i2,φi=arctanc^ici.The instantaneous frequency is defined as the derivative of the instantaneous phase:(4)ωi=dφidt.Signalx(t) can be expressed as(5)xt=RE∑i=1naiejφi=RE∑i=1naiej∫ωidt.Here, we ignore the residual component of the original signalrn; RE denotes the real part. We call the above formula on the right part of the equal sign the Hilbert spectrum:(6)Hω,t=RE∑i=1naitej∫ωitdt.Hilbert marginal spectrum is obtained by integrating the above formula with time:(7)hω=∫0THω,tdt.


### 2.2. HHT Marginal Spectrum Amplitude Curvature

After the structure is applied to the vibrational excitation, the vibration response signal of different parts of the structure is extracted. After the signal is decomposed by the EMD, a series of IMF components is obtained, the main IMF component is selected, and the marginal spectrum amplitude is calculated. Then, the relative HHT marginal spectrum amplitude at different parts of the structure is(8)Ri=FiF0,where Fi is the HHT marginal spectrum of different parts of the structure and F0 is the HHT marginal spectrum of the structure reference position.The HHT marginal spectrum amplitude curvature of different parts of structures is approximately calculated by the central difference method:(9)Φi=Ri+1-2Ri+Ri-1l2,where Ri is calculated at the site of the relative HHT marginal spectrum amplitude, Ri+1 and Ri-1 are calculated at the sites adjacent to the relative HHT marginal spectrum amplitude, and l is the distance between adjacent parts.The difference in HHT marginal spectrum amplitude curvature is(10)ΔΦi=Φui-Φdi,where Φui is the HHT marginal spectrum amplitude curvature before structural damage.


## 2.1. HHT Theory

The HHT method consists of two parts: EMD and HT. The original signalx(t) is decomposed into a series of IMFs and a residual function by EMD:(1)xt=∑i=1nci+rn.Hilbert transformation of the IMF component:(2)c^i=1π∫-∞+∞ciτt-τdτ.Based on this function, the analytic signal is established, and the instantaneous amplitude and phase function are obtained:(3)zi=ci+jc^i=aiejφi,ai=ci2+c^i2,φi=arctanc^ici.The instantaneous frequency is defined as the derivative of the instantaneous phase:(4)ωi=dφidt.Signalx(t) can be expressed as(5)xt=RE∑i=1naiejφi=RE∑i=1naiej∫ωidt.Here, we ignore the residual component of the original signalrn; RE denotes the real part. We call the above formula on the right part of the equal sign the Hilbert spectrum:(6)Hω,t=RE∑i=1naitej∫ωitdt.Hilbert marginal spectrum is obtained by integrating the above formula with time:(7)hω=∫0THω,tdt.


## 2.2. HHT Marginal Spectrum Amplitude Curvature

After the structure is applied to the vibrational excitation, the vibration response signal of different parts of the structure is extracted. After the signal is decomposed by the EMD, a series of IMF components is obtained, the main IMF component is selected, and the marginal spectrum amplitude is calculated. Then, the relative HHT marginal spectrum amplitude at different parts of the structure is(8)Ri=FiF0,where Fi is the HHT marginal spectrum of different parts of the structure and F0 is the HHT marginal spectrum of the structure reference position.The HHT marginal spectrum amplitude curvature of different parts of structures is approximately calculated by the central difference method:(9)Φi=Ri+1-2Ri+Ri-1l2,where Ri is calculated at the site of the relative HHT marginal spectrum amplitude, Ri+1 and Ri-1 are calculated at the sites adjacent to the relative HHT marginal spectrum amplitude, and l is the distance between adjacent parts.The difference in HHT marginal spectrum amplitude curvature is(10)ΔΦi=Φui-Φdi,where Φui is the HHT marginal spectrum amplitude curvature before structural damage.


## 3. Extracting the Signal Characteristics of the Derrick Steel Structure

### 3.1. Establishment of the Simulation Model of the Derrick Steel Structure

The model of the derrick steel structure is 2.951 m high, and the maximum hook load is 13.9 kN. Its material is Q235 steel. The structure was divided into 274 elements and 142 nodes, and its finite-element model is shown in Figure1. The right front pillar nodes of the derrick steel structure were numbered 1–20 from the bottom. There was one element between every two nodes, and the elements were numbered 1–19 from the bottom to the top.Figure 1
Finite-element model of the derrick steel structure.


### 3.2. Derrick Steel Structure Model Analysis

The modal analysis of the model shows that the first three orders of the frequency were 17.53, 18.0, and 38.71 Hz. The first-order vibration mode was mainly the left-and-right first-order bending overall vibration; the second-order vibration mode was mainly the front-and-back first-order bending overall vibration; the third-order vibration mode was mainly torsional vibration.We used a random-noise acceleration load in the vibration model of the derrick steel structure; the sampling frequency of the random-noise acceleration loads was 1000 Hz; the amplitude was 1.2 m/s2; and the load acted on node 20 along the direction of y-axis for 2 s. We used the complete method to solve the transient dynamics, and the acceleration response of nodes 1–20 of the right front pillar of the derrick steel structure in the y direction was extracted.


### 3.3. Extracting the HHT Marginal Spectrum Amplitude Curvature

Our example structure has 15 nodes. The acceleration response of the Fourier spectral analysis in Figure2 shows that random loads can stimulate the first- and third-order frequencies (17.53 Hz and 38.71 Hz) in the derrick steel structure, and the first-order vibration is prioritized.Figure 2
Spectral analysis of the acceleration response of node 15 in the derrick steel structure.Considering the complexity of the derrick steel structure, the nodes in the lower part of the derrick steel structure cannot stimulate the third-order frequency under a random load. Therefore, we used the bandpass filter and HHT combination of methods to extract the first-order vibration information of the derrick steel structure and determine the cut-off frequency of 17 Hz and 18 Hz. We filtered the other frequency components using the EMD decomposition, as shown in Figure3.Figure 3
First-order vibration response of node 15 in the derrick steel structure and EMD.Figure3 shows that the main characteristic information of the signal is concentrated in the first-order IMF component; therefore, we only extracted the marginal spectrum amplitude of the first-order IMF component. The marginal spectrum of the first-order IMF component of node 15 is shown in Figure 4. We could extract the marginal spectrum amplitude of the derrick steel structure from its vibration in the first-order frequency. In the derrick, we selected node 1 as the reference point and calculated the HHT marginal spectrum amplitude curvature of nodes 1~20.Figure 4
First-order IMF component marginal spectrum of node 15 in the derrick steel structure.


## 3.1. Establishment of the Simulation Model of the Derrick Steel Structure

The model of the derrick steel structure is 2.951 m high, and the maximum hook load is 13.9 kN. Its material is Q235 steel. The structure was divided into 274 elements and 142 nodes, and its finite-element model is shown in Figure1. The right front pillar nodes of the derrick steel structure were numbered 1–20 from the bottom. There was one element between every two nodes, and the elements were numbered 1–19 from the bottom to the top.Figure 1
Finite-element model of the derrick steel structure.


## 3.2. Derrick Steel Structure Model Analysis

The modal analysis of the model shows that the first three orders of the frequency were 17.53, 18.0, and 38.71 Hz. The first-order vibration mode was mainly the left-and-right first-order bending overall vibration; the second-order vibration mode was mainly the front-and-back first-order bending overall vibration; the third-order vibration mode was mainly torsional vibration.We used a random-noise acceleration load in the vibration model of the derrick steel structure; the sampling frequency of the random-noise acceleration loads was 1000 Hz; the amplitude was 1.2 m/s2; and the load acted on node 20 along the direction of y-axis for 2 s. We used the complete method to solve the transient dynamics, and the acceleration response of nodes 1–20 of the right front pillar of the derrick steel structure in the y direction was extracted.


## 3.3. Extracting the HHT Marginal Spectrum Amplitude Curvature

Our example structure has 15 nodes. The acceleration response of the Fourier spectral analysis in Figure2 shows that random loads can stimulate the first- and third-order frequencies (17.53 Hz and 38.71 Hz) in the derrick steel structure, and the first-order vibration is prioritized.Figure 2
Spectral analysis of the acceleration response of node 15 in the derrick steel structure.Considering the complexity of the derrick steel structure, the nodes in the lower part of the derrick steel structure cannot stimulate the third-order frequency under a random load. Therefore, we used the bandpass filter and HHT combination of methods to extract the first-order vibration information of the derrick steel structure and determine the cut-off frequency of 17 Hz and 18 Hz. We filtered the other frequency components using the EMD decomposition, as shown in Figure3.Figure 3
First-order vibration response of node 15 in the derrick steel structure and EMD.Figure3 shows that the main characteristic information of the signal is concentrated in the first-order IMF component; therefore, we only extracted the marginal spectrum amplitude of the first-order IMF component. The marginal spectrum of the first-order IMF component of node 15 is shown in Figure 4. We could extract the marginal spectrum amplitude of the derrick steel structure from its vibration in the first-order frequency. In the derrick, we selected node 1 as the reference point and calculated the HHT marginal spectrum amplitude curvature of nodes 1~20.Figure 4
First-order IMF component marginal spectrum of node 15 in the derrick steel structure.


## 4. Simulation Analysis

### 4.1. Damage Condition Design

In the practical condition of the derrick steel structure, damage most likely occurs in the front pillar, so we selected the right front pillar of the derrick steel structure for the study. Damage was set up in two cases: single damage and double damage. Damage can be achieved by reducing the stiffness of the element, and the specific damage conditions are shown in Table1.Table 1
Damage condition of the derrick steel structure.
Condition
Damage degree
Damage type
Damage position
1
5%
Single damage
16
2
20%
10
3
30%
5
4
5%
Double damage
8, 14
5
10%
5, 13
6
5%, 10%
5, 13


### 4.2. Identifying Damage Location

The nonstationary signal can be decomposed into an intrinsic mode function (IMF) and a residual function by empirical modal decomposition. Each component of the IMF contains the local characteristics of different time scales in the original signal. The IMF instantaneous energy reflects the change over time of each component. To verify the effectiveness of this method, we used the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference to identify the damage location under six damage conditions. We calculated the derrick steel structure in good conditions and six damage conditions of the HHT marginal spectrum amplitude curvature and IMF instantaneous energy curvature of nodes 1~20. Then, we compared our results with the corresponding node of curvature difference before and after the derrick steel structure was damaged. The sensor is disturbed by external noise in practical conditions, so we verified the effect of identifying the damage location in a noisy environment.The above analysis is shown in Figure5. Figures 5(a)–5(d) show the single-damage conditions, where elements 16, 10, and 5 were clearly damaged. Figures 5(a) and 5(d) show the 5% damage condition of element 16. Figure 5(e) is the relation curve between the HHT marginal spectrum curvature difference and the node in 10% random noise of damaged element 5; Figures 5(f)–5(i) show the double-damage conditions. We can clearly identify the position of the upper and lower parts of the damaged element in the pillar. Figures 5(g) and 5(h) compare the same damage location with different degrees of damage, and the upper part of the damage element in the pillar of Figure 5(h) is easier to identify than that in Figure 5(g). Figure 5(j) is the relation curve between the HHT marginal spectrum curvature difference and the node in 10% random noise of damaged elements 5 and 13. The comparison shows that the noise under the impact load hardly affected the damage location identification of the derrick steel structure. Therefore, both methods can identify the damage location of the derrick, and the rule based on the HHT method is as follows. The HHT marginal spectrum amplitude curvature difference of the damaged element at two ends of the node mutates, and neighboring nodes have opposite signs. The absolute value of one curvature difference of the node is the maximum of nearby nodes, which can make the HHT marginal spectrum curvature difference of adjacent nodes increase. For the double-damaged places, the HHT marginal spectrum amplitude curvature difference is sensitive to the lower part of the damaged element of the pillar identification. When the damaged position is identical, with the increase in damage degree, it is easier to identify the position of the upper damaged element, and the position of the weakly damaged element can be correctly identified.Figure 5
Relationship between the difference of the HHT marginal spectrum curvature and the nodes.
(a)
Condition 1 (damage of unit 16; HHT method)
(b)
Condition 2 (damage of unit 10; HHT method)
(c)
Condition 3 (damage of unit 5; HHT method)
(d)
Condition 1 (damage of unit 16; IMF method)
(e)
10% random noise (damage of unit 5)
(f)
Condition 4 (damage of units 8 and 14; HHT method)
(g)
Condition 5 (damage of units 5 and 13; HHT method)
(h)
Condition 6 (damage of units 5 and 13; HHT method)
(i)
Condition 6 (damage of units 5 and 13; IMF method)
(j)
10% random noise (damage of units 5 and 13)


### 4.3. Damage Degree Identification

Supposing that the stiffness of element 13 of the right front pillar of the derrick steel structure successively was reduced by 5%, 10%, 15%, 20%, 25%, 30%, 35%, 40%, 45%, and 50%, we calculated the HHT marginal spectrum amplitude curvature difference of node 13 of element 13 at the corresponding damage degree. Figure6 shows the histogram of the relationship between the absolute value of the HHT marginal spectrum amplitude curvature difference and the damage degree.Figure 6
Relationship between the difference of the HHT marginal spectrum curvature and the damage degree.Figure6 shows that the absolute value of the HHT marginal spectrum amplitude curvature difference of node 13 increases with the increase in damage degree. Therefore, we can qualitatively analyze the damage degree of a derrick steel structure based on the HHT marginal spectrum amplitude curvature difference.


## 4.1. Damage Condition Design

In the practical condition of the derrick steel structure, damage most likely occurs in the front pillar, so we selected the right front pillar of the derrick steel structure for the study. Damage was set up in two cases: single damage and double damage. Damage can be achieved by reducing the stiffness of the element, and the specific damage conditions are shown in Table1.Table 1
Damage condition of the derrick steel structure.
Condition
Damage degree
Damage type
Damage position
1
5%
Single damage
16
2
20%
10
3
30%
5
4
5%
Double damage
8, 14
5
10%
5, 13
6
5%, 10%
5, 13


## 4.2. Identifying Damage Location

The nonstationary signal can be decomposed into an intrinsic mode function (IMF) and a residual function by empirical modal decomposition. Each component of the IMF contains the local characteristics of different time scales in the original signal. The IMF instantaneous energy reflects the change over time of each component. To verify the effectiveness of this method, we used the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference to identify the damage location under six damage conditions. We calculated the derrick steel structure in good conditions and six damage conditions of the HHT marginal spectrum amplitude curvature and IMF instantaneous energy curvature of nodes 1~20. Then, we compared our results with the corresponding node of curvature difference before and after the derrick steel structure was damaged. The sensor is disturbed by external noise in practical conditions, so we verified the effect of identifying the damage location in a noisy environment.The above analysis is shown in Figure5. Figures 5(a)–5(d) show the single-damage conditions, where elements 16, 10, and 5 were clearly damaged. Figures 5(a) and 5(d) show the 5% damage condition of element 16. Figure 5(e) is the relation curve between the HHT marginal spectrum curvature difference and the node in 10% random noise of damaged element 5; Figures 5(f)–5(i) show the double-damage conditions. We can clearly identify the position of the upper and lower parts of the damaged element in the pillar. Figures 5(g) and 5(h) compare the same damage location with different degrees of damage, and the upper part of the damage element in the pillar of Figure 5(h) is easier to identify than that in Figure 5(g). Figure 5(j) is the relation curve between the HHT marginal spectrum curvature difference and the node in 10% random noise of damaged elements 5 and 13. The comparison shows that the noise under the impact load hardly affected the damage location identification of the derrick steel structure. Therefore, both methods can identify the damage location of the derrick, and the rule based on the HHT method is as follows. The HHT marginal spectrum amplitude curvature difference of the damaged element at two ends of the node mutates, and neighboring nodes have opposite signs. The absolute value of one curvature difference of the node is the maximum of nearby nodes, which can make the HHT marginal spectrum curvature difference of adjacent nodes increase. For the double-damaged places, the HHT marginal spectrum amplitude curvature difference is sensitive to the lower part of the damaged element of the pillar identification. When the damaged position is identical, with the increase in damage degree, it is easier to identify the position of the upper damaged element, and the position of the weakly damaged element can be correctly identified.Figure 5
Relationship between the difference of the HHT marginal spectrum curvature and the nodes.
(a)
Condition 1 (damage of unit 16; HHT method)
(b)
Condition 2 (damage of unit 10; HHT method)
(c)
Condition 3 (damage of unit 5; HHT method)
(d)
Condition 1 (damage of unit 16; IMF method)
(e)
10% random noise (damage of unit 5)
(f)
Condition 4 (damage of units 8 and 14; HHT method)
(g)
Condition 5 (damage of units 5 and 13; HHT method)
(h)
Condition 6 (damage of units 5 and 13; HHT method)
(i)
Condition 6 (damage of units 5 and 13; IMF method)
(j)
10% random noise (damage of units 5 and 13)


## 4.3. Damage Degree Identification

Supposing that the stiffness of element 13 of the right front pillar of the derrick steel structure successively was reduced by 5%, 10%, 15%, 20%, 25%, 30%, 35%, 40%, 45%, and 50%, we calculated the HHT marginal spectrum amplitude curvature difference of node 13 of element 13 at the corresponding damage degree. Figure6 shows the histogram of the relationship between the absolute value of the HHT marginal spectrum amplitude curvature difference and the damage degree.Figure 6
Relationship between the difference of the HHT marginal spectrum curvature and the damage degree.Figure6 shows that the absolute value of the HHT marginal spectrum amplitude curvature difference of node 13 increases with the increase in damage degree. Therefore, we can qualitatively analyze the damage degree of a derrick steel structure based on the HHT marginal spectrum amplitude curvature difference.


## 5. Experimental Analysis

### 5.1. Damage Location Simulation and Sensor Layout

The ZJ70-type derrick steel structure laboratory model was made according to the prototype equipment of a 7000 m drilling rig with a proportion of 1 : 18. The model is a front-opening model with beam pillars and is divided into four segments. The upper part is the overall structure of the closed segment; the other three segments have a front-opening shape of “∩.” The components of the main body are connected with pins, and its physical model is shown in Figure 7.Figure 7
Laboratory model of the ZJ70-type derrick steel structure.We numbered the segments of the derrick steel structure number as 1–4 from top to bottom. Because of the limited conditions, the experiment of the derrick steel structure was based on one of the two front-opening pillars as the object of study, and the damage forms are simulated by loosening the pin between two segments. We simulated 3 damage conditions. The specific damage conditions are shown in Table2.Table 2
Damage experimental conditions of the derrick steel structure.
Condition
Damage form
Damage type
Damage position
1
Pin loose
Single damage
The place between second segment and third segment
2
Single damage
The place between third segment and forth segment
3
Double damage
Integrating the first two kinds of damage locationIn the experiment, 12 acceleration sensors were used to collect the vibration signals of different parts of the derrick steel structure. The sensors were numbered 1–12 from top to bottom. Conditions 1 and 2 simulated the damage between sensors 6 and 7; Condition 3 simulates the damage between sensors 3 and 4 and the damage between sensors 9 and 10. Figure8 shows the measured distance between adjacent acceleration sensors under three damage conditions. When we calculated the HHT marginal spectrum amplitude curvature, we selected sensor 1 as the reference point.Figure 8
Damage location simulation and sensor layout.
(a)
Single damage
(b)
Double damage


### 5.2. Experimental Signal Acquisition

The vibration excitation mode in the experiments was marked to ensure that the vibration position was identical before and after the simulation of the derrick steel structure. The 12 sensors simultaneously collected the vibration signal of the derrick steel structure; the interface shows the time-domain signal window in real time and 12 channels. To easily observe the signal collected by each sensor, Figure9 is based on Condition 1 as an example, and we intercepted the time-domain signal of sensors 1–12 of the derrick steel structure before it became damaged.Figure 9
Time-domain signal of sensors 1–12 before and after the damage of the derrick steel structure under Condition 1.
(a)
Before being damaged
(b)
After being damaged


### 5.3. Analysis of Experimental Results

We calculated the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference of the derrick steel structure in three conditions and show its relationship with sensors 1–12 in Figure10.Figure 10
Relationship between the HHT marginal spectrum curvature difference or IMF instantaneous energy curvature difference and the sensors.
(a)
Condition 1 (Sensors 6 and 7; HHT method)
(b)
Condition 1 (Sensors 6 and 7; IMF method)
(c)
Condition 2 (Sensors 6 and 7; HHT method)
(d)
Condition 2 (Sensors 6 and 7; IMF method)
(e)
Condition 3 (Sensors 3, 4, 9, and 10; HHT method)
(f)
Condition 3 (Sensors 3, 4, 9, and 10; IMF method)In conditions 1 and 2, the derrick steel structure was simulated with single damage. Figures10(a) and 10(b) show the significant mutations of the damage sensitivity index of sensors 6 and 7, which is consistent with the presupposition of damage position. Therefore, the single damage of the derrick steel structure can be accurately identified based on the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference. Condition 3 simulates the double damage of the derrick steel structure. Figure 10(c) clearly shows that the damage-sensitive index of sensors 3 and 4 mutated and significantly changed. Sensors 9 and 10 had the largest amplitude of variation of the damage-sensitive index with the adjacent value, which is also consistent with the preset double-damage position. Therefore, the double-damage position of the derrick steel structure can also be identified by the damage sensitivity index.


## 5.1. Damage Location Simulation and Sensor Layout

The ZJ70-type derrick steel structure laboratory model was made according to the prototype equipment of a 7000 m drilling rig with a proportion of 1 : 18. The model is a front-opening model with beam pillars and is divided into four segments. The upper part is the overall structure of the closed segment; the other three segments have a front-opening shape of “∩.” The components of the main body are connected with pins, and its physical model is shown in Figure 7.Figure 7
Laboratory model of the ZJ70-type derrick steel structure.We numbered the segments of the derrick steel structure number as 1–4 from top to bottom. Because of the limited conditions, the experiment of the derrick steel structure was based on one of the two front-opening pillars as the object of study, and the damage forms are simulated by loosening the pin between two segments. We simulated 3 damage conditions. The specific damage conditions are shown in Table2.Table 2
Damage experimental conditions of the derrick steel structure.
Condition
Damage form
Damage type
Damage position
1
Pin loose
Single damage
The place between second segment and third segment
2
Single damage
The place between third segment and forth segment
3
Double damage
Integrating the first two kinds of damage locationIn the experiment, 12 acceleration sensors were used to collect the vibration signals of different parts of the derrick steel structure. The sensors were numbered 1–12 from top to bottom. Conditions 1 and 2 simulated the damage between sensors 6 and 7; Condition 3 simulates the damage between sensors 3 and 4 and the damage between sensors 9 and 10. Figure8 shows the measured distance between adjacent acceleration sensors under three damage conditions. When we calculated the HHT marginal spectrum amplitude curvature, we selected sensor 1 as the reference point.Figure 8
Damage location simulation and sensor layout.
(a)
Single damage
(b)
Double damage


## 5.2. Experimental Signal Acquisition

The vibration excitation mode in the experiments was marked to ensure that the vibration position was identical before and after the simulation of the derrick steel structure. The 12 sensors simultaneously collected the vibration signal of the derrick steel structure; the interface shows the time-domain signal window in real time and 12 channels. To easily observe the signal collected by each sensor, Figure9 is based on Condition 1 as an example, and we intercepted the time-domain signal of sensors 1–12 of the derrick steel structure before it became damaged.Figure 9
Time-domain signal of sensors 1–12 before and after the damage of the derrick steel structure under Condition 1.
(a)
Before being damaged
(b)
After being damaged


## 5.3. Analysis of Experimental Results

We calculated the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference of the derrick steel structure in three conditions and show its relationship with sensors 1–12 in Figure10.Figure 10
Relationship between the HHT marginal spectrum curvature difference or IMF instantaneous energy curvature difference and the sensors.
(a)
Condition 1 (Sensors 6 and 7; HHT method)
(b)
Condition 1 (Sensors 6 and 7; IMF method)
(c)
Condition 2 (Sensors 6 and 7; HHT method)
(d)
Condition 2 (Sensors 6 and 7; IMF method)
(e)
Condition 3 (Sensors 3, 4, 9, and 10; HHT method)
(f)
Condition 3 (Sensors 3, 4, 9, and 10; IMF method)In conditions 1 and 2, the derrick steel structure was simulated with single damage. Figures10(a) and 10(b) show the significant mutations of the damage sensitivity index of sensors 6 and 7, which is consistent with the presupposition of damage position. Therefore, the single damage of the derrick steel structure can be accurately identified based on the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference. Condition 3 simulates the double damage of the derrick steel structure. Figure 10(c) clearly shows that the damage-sensitive index of sensors 3 and 4 mutated and significantly changed. Sensors 9 and 10 had the largest amplitude of variation of the damage-sensitive index with the adjacent value, which is also consistent with the preset double-damage position. Therefore, the double-damage position of the derrick steel structure can also be identified by the damage sensitivity index.


## 6. Conclusions

Vibration sensors have been widely studied and applied to collect vibration signals to detect the structural state of damage in health-monitoring technology. We only used the low-level vibration information of the derrick steel structure to propose a damage identification method for derrick steel structures based on the HHT marginal spectrum amplitude curvature difference.(1) The HHT marginal spectrum amplitude curvature difference is related to the position of damaged elements. From the comparison with IMF instantaneous energy curvature difference, the position of damaged elements and the weak damage of the derrick steel structure can be accurately identified based on the HHT marginal spectrum amplitude curvature difference.(2) The HHT marginal spectrum amplitude curvature difference can qualitatively analyze the damage degree of the elements, and the larger absolute value of the HHT marginal spectrum amplitude curvature difference between two ends of the damaged element increases with the increase in damage degree of the element.(3) The simulation experiment of the damage location of the derrick steel structure shows that the damage identification method for derrick steel structures based on the HHT marginal spectrum amplitude curvature difference and IMF instantaneous energy curvature difference can extract the low-level vibration information. Thus, we can correctly identify the location of damaged elements and easily obtain the low-level vibration information of derrick steel structures in practice, which indicates that the method is reliable and easy to operate.



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*Source: 1062949-2017-09-17.xml*