Sheng Shen1,2, Yao Wang3, Sheng-Lan Ma4, Di Huang5, Zhi-Hong Wu6, Xiao Guo7. 1. Department of Civil Engineering, Fuzhou University, Fuzhou 350108, China. s_shen@fzu.edu.cn. 2. Hebei Province Key Laboratory of Evolution and Control of Mechanical Behavior in Traffic Engineering Structure, Shijiazhuang Tiedao University, Shijiazhuang 050043, China. s_shen@fzu.edu.cn. 3. CSCEC Strait Construction and Development Co., LTD, Fuzhou 350015, China. yao.wang@tom.com. 4. Fujian Provincial Key Laboratory of Advanced Technology and Informatization in Civil Engineering, Fujian University of Technology, Fuzhou 350118, China. mashenglan@fjut.edu.cn. 5. Department of Civil Engineering, Fuzhou University, Fuzhou 350108, China. N160527015@fzu.edu.cn. 6. CSCEC Strait Construction and Development Co., LTD, Fuzhou 350015, China. francois@seu.edu.cn. 7. CSCEC Strait Construction and Development Co., LTD, Fuzhou 350015, China. Xiao_Guo@tom.com.
Abstract
Prestress loss evaluation in prestressed strands is essential for prestressed structures. However, the sensors installed outside the duct can only measure the total prestress loss. The sensors attached on strands inside the duct also have several problems, such as inadequate durability in an aggressive environment and vulnerability to damage during tensioning. This paper proposes a new installation method for long-gauge fiber Bragg grating (LFBG) sensors to prevent accidental damage. Then the itemized prestress losses were determined in each stage of the pre-tensioning and post-tensioning according to the LFBG measurements. We verified the applicability of the LFBG sensors for prestress monitoring and the accuracy of the proposed prestress loss calculation method during pre-tensioning and post-tensioning. In the pre-tensioning case, the calculated prestress losses had less deviation from the true losses than those obtained from foil-strain gauges, and the durability of the LFBG sensors was better than foil-strain gauges, whereas in post-tensioning case, the calculated prestress losses were close to those derived from theoretical predictions. Finally, we monitored prestress variation in the strand for 90 days. The itemized prestress losses at each stages of post-tensioning were obtained by the proposed calculation method to show the prospect of the LFBG sensors in practical evaluation.
Prestress loss evaluation in prestressed strands is essential for prestressed structures. However, the sensors installed outside the duct can only measure the total prestress loss. The sensors attached on strands inside the duct also have several problems, such as inadequate durability in an aggressive environment and vulnerability to damage during tensioning. This paper proposes a new installation method for long-gauge fiber Bragg grating (LFBG) sensors to prevent accidental damage. Then the itemized prestress losses were determined in each stage of the pre-tensioning and post-tensioning according to the LFBG measurements. We verified the applicability of the LFBG sensors for prestress monitoring and the accuracy of the proposed prestress loss calculation method during pre-tensioning and post-tensioning. In the pre-tensioning case, the calculated prestress losses had less deviation from the true losses than those obtained from foil-strain gauges, and the durability of the LFBG sensors was better than foil-strain gauges, whereas in post-tensioning case, the calculated prestress losses were close to those derived from theoretical predictions. Finally, we monitored prestress variation in the strand for 90 days. The itemized prestress losses at each stages of post-tensioning were obtained by the proposed calculation method to show the prospect of the LFBG sensors in practical evaluation.
Prestressing of steel strands provides reversal stress to counteract in-service stress partially or entirely, improve the crack resistance, and reduce the deflection of prestressed structures. Thus, the tensile stress in steel strands can be maintained over time. However, the applied prestress may decrease gradually due to various reasons, such as the stress relaxation in the steel strands, concrete creep and shrinkage, friction between the strand and duct, and deformation of anchoring devices [1]. Moreover, long-term factors including aggressive environment, pitting, stress corrosion, and hydrogen embrittlement can decrease prestressing further and trigger a fracture of the strand that gives rise to accidents, causing the degradation of the nuclear containment vessel [2], the decrease in seismic performance of the concrete frame [3], and the collapse of a bridge [4]. Therefore, measuring and evaluating prestress loss of steel strand is imperative for maintenance and accurate assessment of prestressed structures.Current sensing techniques for prestress loss measurement can be grouped into two categories: global measurements and local measurements. The global measurements are performed via elastomagnetic sensors [5,6,7], stress waves [8,9], Anchorage-Measurement-Access system [10,11], frequency [12,13], and modal parameters [14]. A common characteristic of the global measurement techniques is that the sensors are usually placed outside anchoring devices to obtain a “global” prestress of the strand. However, this approach has critical drawbacks. First, the “global” value fails to reflect the itemized prestress losses distributing along the strand. Moreover, most global measurements are indirect, complicated in data processing, and disturbed easily by electromagnetic interference. Last, the global measurement does not provide enough sensitivity to detect stress variations that may be quite small compared to the total stress of a prestressed strand due to micro cracks.To overcome these disadvantages, researchers have focused on the local measurement that place the sensor on the surface of the strand to directly monitor prestresses at some pre-designated points. The local measurement is applied based on some electric sensors, such as strain gauges [15,16], piezoelectric transducer actuator [17] and so on. However, local measurement is more challenging to perform than global measurement due to the following three reasons. First, if the duct has a curved profile between the ends, the sensor or connecting line may be dislocated and damaged by the friction between the strand and duct during tensioning. Second, the interspace is small between the strand and duct. Some sensors, such as the elastomagnetic sensors, cannot be installed into the duct due to their size. The third reason is that grout used to fill the duct after tensioning may trigger a short circuit to the electric sensor without resin isolation.The above challenges could be overcome using a fiber Bragg grating (FBG) sensor that is more suitable for long-term prestress monitoring than an electric sensor due to its small size, light weight, high stability, and durability. In recent years, FBG sensors have been widely used for dynamic strain-stress and vibration measurements in bridges [18,19,20], scour monitoring [21,22], reinforcement corrosion [23,24], and leakages in concrete structures and pipelines [25,26,27,28]. Two kinds of FBG sensors have been proposed for prestress monitoring. The first type is named as “smart strand” consisting of six helical wires and a core wire embedded an FBG sensor [29,30,31,32,33]. Although the FBG sensor can accurately measure prestress in the core wire, the “smart strand” also has two drawbacks in practice. First, for cost reduction, the position of each FBG sensor in a “smart strand” is predetermined in the production stage, and the distance between adjacent sensors is usually identical. However, these predetermined positions and distances may not match the required positions and distances in practical construction. Second, because the core wire is surrounded closely by six helical wires, it is difficult to connect the embedded FBG sensor in the core wire to the optical cable used to transmit the optical signal.An improved “smart strand” type sensor has been proposed for monitoring prestress distribution by combining the Brillouin optical time domain analysis/refectory (BOTDA/R) sensor and the FBG sensor along a single optical fiber to solve this problem [34,35]. However, the measurement error of the BOTDA/R sensor was at least dozens of micro-strain, reducing the accuracy of the monitoring data. The results of Zhang’s experiments showed that the strain measurement error of AQ8603 (produced by Ando Electric Co. Ltd., Tokyo, Japan) based on the BOTDR technique was ±130 με (1.96 σ,σ = ±65 με) [36], which is larger than the AQ8603’s nominal precision of ±50 με. The measurement error of the NBX-6000 (produced by Neubrex Co. Ltd., Kobe, Japan) based on pulse-prepump Brillouin Optical Time Domain Analysis (PPP-BOTDA) was about ±80 με (2σ, σ = ±40 με), which is larger than the NBX-6000’s nominal precision of ±25 με [37]. The second type of FBG sensor comprises a grating packaged with a metal capillary [38,39]. Then the capillary-encapsulated FBG sensors are bonded on the surface of the strand by epoxy resin to measure the elongation. The shortcomings of this type of FBG sensors also exist. First, the elastic modulus of steel is far greater than that of resin, and the mechanical strength of most epoxy resins is limited. Thus, mechanical creep may occur in epoxy, when the epoxy is stressed to beyond 50% of its tensile strength [40], and the bonding may fail if the transmitting stress reaches 80% of the ultimate tensile strength of resin [41]. Second, the sensor is proposed to install in the space between two adjacent steel wires [39]. This installation method may lead to accidental damage to the sensor caused by the dislocation of adjacent wires during strand tensioning. Finally, because the strain distributed in each wire is not identical, the measurements from the sensor for a single wire may have a remarkable difference from the true strain of the strand.We propose that the long-gauge fiber Bragg grating (LFBG) sensor [42] could overcome the abovementioned limitations. The LFBG sensor has a sensing gauge ranging from 0.1 to 1 m suggesting that the measured strain can represent the average elongation of all wires in the gauge length. Meanwhile, the LFBG sensor is packaged by epoxy-soaked fiber reinforced polymer (FRP) material because the elastic modulus of the epoxy-soaked FRP material is less than that of steel so that the bonding can safely transmit the strain from the strand to the sensor. Moreover, the durability of the LFBG sensor has been verified by the fatigue experiment and long-term durability tests in acidic, alkaline, and salt environments [43]. The applicability of the LFBG sensor was also confirmed in practical monitoring for measuring dynamic strain [44] and dynamic displacement [45], and observing the change in the neutral axis position [46]. However, little is known on the monitoring and calculation of prestress losses based on the LFBG sensor.This paper is organized as follows: Section 2 introduces the structure and design of an LFBG sensor for prestress monitoring in a strand and proposes the installation procedure in practical operation. Based on the strain measurements from the installed LFBG sensors, Section 3 proposes a method to calculate the itemized prestress losses in both pre-tensioning and post-tensioning. Section 4 and Section 5 demonstrate the application of the proposed method experimentally and via in-site monitoring, respectively.
2. The Design and Installation of LFBG Sensors
2.1. Introduction of the LFBG Strain Sensor
The structure of an LFBG sensor proposed by Li [42] is illustrated in Figure 1. A notable feature of this sensor is the use of an embedded and hollow polytetrafluoroethylene tube, inside which an FBG is sleeved and fixed at both ends, and the gauge length of the sensing part can be predetermined.
Figure 1
The structural design of the packaged LFBG sensor proposed by Li [42].
Moreover, the specific design is advantageous for numerous reasons: (i) The hollow tube used to encapsulate the FBG inside can ensure the strain at each point of the fiber optic is identical, and the measurement from the FBG equals the average strain over the gauge length directly. (ii) A special epoxy resin used to recoat the FBG can effectively prevent the slippage between the bare fiber optic and the epoxy resin. Meanwhile, the strain compatibility can be achieved between the FBG and epoxy resin until the measurement attains the breaking strain. This point is important for high stress-strain measurement in practical prestress monitoring. (iii) The bonding capability of the FRP material with structural materials, such as steel and concrete, is excellent. The FRP also has an excellent long-term durability and stability to prevent degradation due to corrosion and extreme environments.
2.2. Length Design of LFBG Sensor Installed on the Strand
As shown in Figure 2, the strand is composed of a linear core wire and six helical wires. Because the gauge lengths are no longer than several centimeters, most traditional strain sensors, such as the electric resistance strain gauge and the short-gauge FBG sensor, can obtain only the strain of one wire in the strand. However, this measurement cannot represent the true elongation of the strand. Therefore, the sensing part of the LFBG sensor needs to have a length that can touch all the six helical wires in a spiral. For example, the gauge length of an LFBG sensor is about 20–25 cm for stress monitoring to a 7-wire strand. Thus, the entire length of the LFBG sensor can reach 30–35 cm considering that bonding length of each end is set to about 5 cm. Generally, the total thickness of the sensor and the surrounding epoxy resin is less than 3 mm; this thickness is remarkably less than the diameter of a wire and space between the strand and duct.
Figure 2
Comparison of gauge length between LFBG sensor and the short-gauge sensor.
2.3. Installation Procedure of the LFBG Sensor
The installation procedure is designed to prevent the installed LFBG sensors from accidental failure caused by friction between adjacent strands and between the strand and duct. The restraining block is used to separate adjacent strands and provide space to the sensor. Figure 3a,b show the designed restraining blocks for a 7-strand tendon and 3-strand tendon, respectively. Every block is assembled of two symmetrical parts by connecting bolts. The central hole of the block can contain the core strand and six helical strands that are separated by six grooves. The practical sketch of the restraining blocks on a 7-strand tendon is illustrated in Figure 3c. The distance over 50–60 cm between the two restraining blocks is long enough to contain the LFBG sensors installed on the strands.
Figure 3
Sketches of the restraining block for (a) 7-strand tendon; (b) 3-strand tendon; and (c) for separating adjacent strands.
As shown in Figure 4a–f, the installation procedure is outlined as follows:
Figure 4
The installation procedure of the LFBG sensor. (a) Place the strands through the marked pipe; (b) strip the partial corrugated pipe; (c) install the restraining blocks; (d) attach the LFBG sensors; (e) connect the sensor to the optical cable; and (f) connect the protection sleeve.
Mark the corresponding region on the corrugated pipe. Then let the strands pass through the marked corrugated pipe.Peel the marked region of the corrugated pipe to expose the inner tendon. Clean the surface of the exposed tendons.Install the restraining blocks and tighten the bolts.Attach the LFBG sensors on the surface of the strands. The attachment position of the sensor on each outer strand should be pointed at and close to the core strand.Let the optical cable pass through a protective sleeve and connect to the sensors.Connect the protective sleeve to the corrugated pipe and use epoxy resin to seal off the contact area. Then the protection sleeve inside which the optical cable is placed can be extended away from the corrugated pipe to the nearest vent hole or drain hole.
3. The Calculation Method for Itemized Prestress Losses Based on the LFBG Measurements
The discussion proposes an optimized sensor configuration for pre-tensioning and post-tensioning and gives the calculation method for itemized prestress losses in both pre-tensioning and post-tensioning based on the LFBG measurements.
3.1. The Itemized Prestress Losses
In the Chinese Code [47], the total prestress loss comprises seven itemized prestress losses named as σl1–σl7. σl1 is the anchorage-seating loss. σl2 is the frictional loss containing the loss due to the friction between tendons and duct (σl2,I) and the loss due to draw-in of the wedge (σl2,II). σl3 is the loss due to the temperature difference between the tendon and the abutments in concrete curing. σl4 is the loss due to steel relaxation. σl5 is the loss due to creep and shrinkage of concrete. σl6 is the loss due to the case in which spiral prestressed rebar in annular structure, such as nuclear containment vessel, is extruded by adjacent concrete. σl7 is the loss due to elastic shortening of concrete.These seven itemized prestress losses are broadly classified into two groups: (1) immediate reductions during prestressing of the tendons and the prestress transferring from the tendons to the concrete members; and (2) time-dependent reductions occurring gradually during the in-service life of the structures. The immediate reductions contain σl1, σl2, σl3, σl6, and σl7. σl4, and σl5 belong to the time-dependent reductions.
3.2. The Case of Pre-Tensioning
As shown in Figure 5a–c, two abutments are fixed securely at both ends of a prestressing bed, and a high-strength steel tendon is pulled between the abutments before the concrete casting. When the concrete attains the required strength for prestressing, the tendon is cut from the abutments, and the prestress is transferred from the tendon to the concrete member through the bond between them. According to the Chinese Code [47], the total loss σ is the sum of several itemized prestress losses shown in Equation (1):
and the term σl2,I does not exist in pre-tensioning.
Figure 5
Three stages of pre-tensioning: (a) applying prestress to tendons; (b) casting and curing of concrete member; and (c) cutting of tendon.
A pre-tensioning beam is a typical kind of simply-supported beam. As illustrated in Figure 5, the LFBG sensors can be set on these regions of the tendon as follows: (1) regions near the ends of the beam (R1 and R3); (2) region near the mid-span of the beam (R2). The reason for the former choice is that σl1 and σl2,II constitute the main part of immediate losses, and σl3 and σl4 can be considered to be uniformly distributed along the tendon. The reason for the latter is that the mid-span usually has the maximum moment under the action of daily loads.Five stages (Stages a–e) exist in a prestressed structure from pre-tensioning to load bearing. Of those, Stages a–d are shown in Figure 5a–c, and Stage e represents the in-service stage of the structure. The measured strains at R1–R3 at Stages a–d are set as ~ (i = 1–3), respectively. The superscript Ri denotes the variable located at Ri (i = 1–3). The subscript a-d implies that the variable is used at Stages a-d, respectively.At the tensioning stage (Stage a), the relationship between the tensioning force and monitored strain is:
where A and E are the area and elastic modulus of prestressing tendon, respectively. F is the tensioning force obtained by the load cell. The value of E is determined by a tensile test carried out in the laboratory. No prestress loss occurs at this stage.σl1 and σl2 occur at Stage b of transferring the tensioning force from jack to prestressing bed. However, it is difficult to divide them without using special measurements, so the sum of σl1 and σl2 is shown as follows:At Stage c of concrete member curing, σl3 and begin to appear. Because the low-relaxation prestressing strand can finish its relaxation in several hundreds of hours, can be obtained entirely in Stage c. Thus, σl3 and can be respectively calculated by Equations (4) and (5):At Stage d, the tendons between the beam and the abutment are cut off, and the prestress is resisted by the entire section of the beam. At this time, , which can be obtained by Equation (6) comes into play:At the in-service stage (Stage e), can be obtained by Equation (7) when the live load is not applied on the structure:Finally, substituting Equations (3)–(7) into Equation (1), the total prestress losses at different locations of the structure are obtained.
3.3. The Case of Post-Tensioning
A remarkable limitation of the pre-tensioning system is that the tendons always have to be straight. However, the post-tensioning system enables the tendons to keep a curved profile before and after tensioning. The ducts inside which the tendons are placed can be fixed to the reinforcements to remain in the desired profile. Then, once the concrete reaches the desired strength, the tendons are tensioned and anchored using external anchors rather than depending on the bond between tendon and concrete as in the pre-tensioning case. Figure 6a–b show the two stages of the post-tensioning procedure.
Figure 6
The schematic of the two stages of post-tensioning: (a) Application of tensioning to tendons; and (b) Fitting the wedge and cutting the tendon.
According to the Chinese Code [47], the total loss σ is the sum of several itemized prestress losses shown in Equation (8):As shown in Figure 6, σl6 is zero. σl2,I exists and does not equal to zero because the profile of the duct is usually curved. σl7 is zero unless the tendons are tensioned batch-wise.The LFBG sensors can be set on the three regions (R1–R3) shown in Figure 6. In post-tensioning, the curve of the duct profile can be described as a combination of three parabolas. The two linking points between the three parabolas are key points in the design of prestressed structures. Thus, R1 and R3 are set to be near to these two linking points. R2 is set at the mid-span of the beam.There are three stages (Stages a~c) in a post-tensioned structure from post-tensioning to load bearing. Stages a and b are the tensioning stage and the stage of anchoring, respectively. Stage c is the stage of grout curing and in-service stage of the structure that is shown in Figure 6b.At Stage a, there are only the frictional losses σl2. In Equation (9), is the frictional loss in Ri:At Stage b, the stress variation equals as follows:At Stage c, the sum of and is shown in Equation (11). It also needs to be measured without live load action:This proposed method is also suitable for prestress loss calculation of more than one tendon in pre-tensioning and post-tensioning. Moreover, it is necessary to keep a distance between the sensor-placed regions near both ends of the strand and the anchor, since the violent variation of stress may threaten the safety of the LFBG sensors in prestress releasing. Finally, all the strain measurements should be updated by temperature compensation.
4. Verification for The Prestress Loss Monitoring Using LFBG Sensor: Experiment
This experiment in this study has two main purposes: to verify the applicability of the LFBG sensor to measure the prestress of a tendon and to investigate the accuracy of the proposed calculation method of prestress loss. In order to correspond to the proposed prestress loss monitoring methods in Section 3, this experiment includes two parts: pre-tensioning test and post-tensioning test.
4.1. Pre-Tensioning Test
4.1.1. Test Design
As shown in Figure 7a, a 7-wire strand inserted into a hollow steel tube was fixed at both abutments of a prestressing bed. The tube was held by two supports and separated from the strand. The strand was placed at the center of the tube. The lengths of the strand and hollow steel tube were 3000 mm and 2500 mm, respectively. The nominal diameter and elastic modulus of the strand were 15.2 mm and 200 GPa, respectively. The outside and inside diameters of the hollow tube were 50 mm and 48 mm, respectively. Three monitored regions (R1–R3) with a uniform length of 250 mm were set from the right end to the mid-point of the strand, and the distance between adjacent regions was 250 mm. Three LFBG sensors (S1–S3) with a uniform gauge length of 250 mm were placed on R1–R3, respectively. In each region, each helical wire was attached to a foil strain-gauge (FSG) to measure the strain precisely. The numbering rule is as follows. For example, the 6 FSGs in R1 are named as E11–E16. The first number means the sensor is in R1 and the second number represents the number of the wire. Details are given in Figure 7c about the sensor placement on the wire.
Figure 7
The sketches and photographs of the test design: (a) applying tensioning to the bare strand; (b) applying load on the cement-filled steel tube; (c) the photograph of the strand attached with sensor; (d) the photograph of tensioning and (e) the photograph of vertical load applied on the cement-filled steel tube.
The process of loading can be divided into three steps (Step I–III). At Step I, the increasing load F was applied by a jack to tension the strand through eight successive loading steps from 0 to 156 kN with an increment of 20 kN. After the final loading step, tensioning reduces from 156 kN to 149.8 kN because of the anchorage-seating loss and the loss due to draw-in of the wedge. At the beginning of Step II, the tube was filled with grout. When the strength of the grout exceeded 50 MPa (48 h after tensioning), the supports were removed. At Step III, a vertical load P was divided equivalently into two parts by a transferring steel board and applied at two points 500 mm away from both ends of the tube. P was increased with a loading step of 3 kN from 0 kN to 24 kN. Details about Step II and Step III are respectively shown in Figure 7b,d,e. The strains of R1–R3 in each helical wire at Steps I-III were measured by FSGs and LFBG sensors, respectively. In addition, the temperature was kept constant during the entire experiment to avoid the expansion or contraction of the abutments and strand. All measured data were updated by temperature compensation.
4.1.2. Results and Analysis
Table 1 gives the measured strains from the FSGs, the average values of the measured strains from the FSGs, and the measured strains from the LFBG sensors at Step I. Table 2 shows the comparison between the true stresses, the stresses calculated from the average values of the measured strains from the FSGs, and the stresses calculated from the strains obtained from the LFBG sensors. Four remarkable features are notable: First, most calculated stresses from sensor measurements are lower than the true stresses, the result ascribed to the gap between the adjacent wires. Second, the difference between the maximum and minimum strains of the six helical wires in the same region can approach or exceed 10% of the applied strain.
Table 1
The monitored strains of the strand at Step I. (Unit: με).
Region
F/kN
20
40
60
80
100
120
140
156
149.8
R1
E11
817
1487
2189
2879
3540
4201
4791
5246
5053
E12
520
1042
1656
2331
3045
3734
4400
5013
4708
E13
720
1314
1971
2670
3336
3978
4583
5124
4936
E14
671
1291
1979
2682
3381
4055
4692
5244
5080
E15
795
1576
2305
3014
3707
4374
5006
5550
5271
E16
716
1348
2028
2714
3393
4044
4665
5214
5095
Average strain(FSG) *
707
1343
2021
2715
3400
4064
4689
5232
5024
S1
713
1426
2129
2808
3524
4237
4940
5482
5270
R2
E21
695
1353
2013
2674
3356
3991
4593
5156
4929
E22
616
1254
1903
2553
3231
3857
4452
5004
4725
E23
753
1420
2076
2728
3410
4035
4631
5184
4976
E24
616
1211
1825
2456
3136
3753
4349
4892
4684
E25
705
1385
2062
2740
3460
4105
4727
5279
5149
E26
687
1329
1973
2616
3302
3911
4500
5031
4828
Average strain(FSG)
678
1325
1975
2628
3316
3942
4542
5091
4882
S2
685
1388
2035
2776
3425
4077
4814
5238
5028
R3
E31
707
1382
2080
2760
3384
4060
4716
5236
5014
E32
683
1359
2063
2756
3391
4073
4739
5265
5044
E33
705
1318
1959
2592
3187
3824
4456
4946
4826
E34
737
1425
2129
2820
3465
4135
4801
5308
4986
E35
621
1298
2004
2698
3350
4020
4690
5202
4979
E36
694
1379
2090
2788
3447
4120
4800
5307
5082
Average strain(FSG)
691
1360
2054
2736
3371
4039
4700
5211
4989
S3
711
1407
2064
2764
3500
4186
4900
5356
5128
* Average strain (FSG) represents the average value of the strains from the six FSGs obtained from the same region.
Table 2
The measurement errors in calculated stresses from the strains obtained from the FSGs and LFBG sensors.
F/kN
20
40
60
80
100
120
140
156
149.8
True Stress/MPa
143.0
285.7
428.6
571.4
714.3
857.1
1000.0
1114.3
1070.0
R1
Stress(FSG) */MPa
141.4
268.6
404.2
543.0
680.0
812.8
937.8
1046.4
1004.8
Error/%
−1.1
−6.0
−5.7
−4.8
−4.6
−6.2
−5.9
−6.1
−6.1
Stress(LFBG) **/MPa
142.6
285.2
425.8
561.6
704.8
847.4
988.0
1096.4
1054.0
Error/%
−0.3
−0.2
−0.7
−1.7
−1.3
−1.1
−1.2
−1.6
−1.5
R2
Stress(FSG)/MPa
135.6
265.0
395.0
525.6
663.2
788.4
908.4
1018.2
976.4
Error/%
−5.0
−7.3
−7.8
−8.0
−7.2
−8.0
−9.2
−8.6
−8.7
Stress(LFBG)/MPa
137.0
277.6
407.0
555.2
685.0
815.4
962.8
1047.6
1005.6
Error/%
−4.0
−2.8
−5.0
−2.8
−4.1
−4.9
−3.7
−6.0
−6.0
R3
Stress(FSG)/MPa
138.2
272.0
410.8
547.2
674.2
807.8
940.0
1042.2
997.8
Error/%
−3.5
−4.8
−4.2
−4.2
−5.6
−5.8
−6.0
−6.5
−6.7
Stress(LFBG)/MPa
142.2
281.4
412.8
552.8
700
837.2
980.0
1071.2
1025.6
Error/%
−0.6
−1.5
−3.7
−3.3
−2.3
−1.9
−2.0
−3.9
−4.1
* Stress (FSG) is the stress calculated from the average strain (FSG) in Table 1. ** Stress (LFBG) is the stress calculated from the measured strains by LFBG sensors in Table 1.
This result implies that the strain measured in one wire only does not necessarily represent the elongation of the whole strand. Moreover, the measured strains from the LFBG sensors are between the maximum and minimum strains from the FSGs and close to the average values of the measured strains from the FSGs. This result is attributed to the fact that LFBG can acquire the average elongation of six helical wires because the sensing part of the LFBG can cover the six wires.Finally, most of the differences between the true stresses in the strand and the calculated stresses by strains from LFBG sensors are less than 5%. The maximum error is 6.0%. However, the differences between the true stresses in the strand and the calculated stresses from the average values of the measured strains from the FSGs are over 5%. The maximum error is up to 9.2%. It appears that the errors in strains from LFBG sensors are approximately half of those obtained from FSGs. An important reason behind this effect is that the FSGs attached on the helical wires are not parallel with the tensioning direction. In summary, these features show LFBG sensor is better suited to monitor prestress in the strand than common FSG.Table 3 gives the monitored strains from different sensors at Step II. The comparison between the true stresses and the calculated stresses are shown in Table 4. Most of the losses calculated from the strains obtained from the LFBG sensors are approximate to or less than the corresponding losses calculated from the average values of the measured strains from the FSGs. Moreover, some FGSs become invalid at the end of this step. It further shows that the traditional electrical sensor may not satisfy the requirements of “local measurement in duct” due to the lack of long-term durability.
Table 3
The monitored strains of the strand at Step II. (Unit: με).
Time/Hour
0
1
2
3
12
24
48
F/KN
149.8
149.55
149.35
149.24
149.1
148.95
148.9
R1
E11
5053
5046
5040
5038
5032
5015
5009
E12
4708
4697
4689
4685
4674
4662
4656
E13
4936
4928
4921
4920
4918
-
-
E14
5080
5066
5061
5058
5044
5027
5022
E15
5271
5265
5261
5257
5249
5234
5226
E16
5095
5087
5081
5077
5068
5052
5044
Average strain of E11–E16
5024
5015
5009
5006
4998
4998
4991
S1
5270
5260
5253
5249
5242
5238
5234
R2
E21
4929
4918
4909
4904
4893
4880
4865
E22
4725
4720
4717
4715
4709
-
E23
4976
4967
4960
4958
4951
4931
4909
E24
4684
4673
4666
4662
4657
4633
4624
E25
5149
5143
5138
5135
5130
5113
5094
E26
4828
4820
4814
4810
4801
4777
4764
Average strain of E21–E26
4882
4874
4867
4864
4857
4867
4851
S2
5028
5019
5013
5009
5003
4997
4995
R3
E31
5014
5005
4997
4993
4989
4983
4980
E32
5044
5033
5025
5018
5008
5005
5002
E33
4826
4817
4810
4808
4801
4799
4795
E34
4986
4978
4972
4970
4967
4957
4951
E35
4979
4971
4964
4961
4957
4952
-
E36
5082
5070
5063
5058
5054
5048
5044
Average strain of E31–E36
4989
4979
4972
4968
4963
4957
4954
S3
5128
5117
5112
5108
5103
5097
5094
Table 4
The stresses and the measurement errors calculated from the strains obtained from the FSGs and LFBG sensors.
Time/Hour
1
2
3
12
24
48
True stress/MPa
1.78
3.2
4.0
5.0
6.07
6.43
R1
Stress(FSG)/MPa
1.8
3
3.6
5.2
5.2
6.6
Error/%
1.1
−6.3
−10.0
4.0
4.0
2.6
Stress(LFBG)/MPa
2
3.4
4.2
5.6
6.4
7.2
Error/%
12.4
6.3
5.0
12.0
5.4
12.0
R2
Stress(FSG)/MPa
1.6
3
3.6
5
3
6.2
Error/%
−10.1
−6.3
−10.0
0
50.5
−3.6
Stress(LFBG)/MPa
1.8
3
3.8
5
6.2
6.6
Error/%
1.1
−6.3
−5.0
0
2.1
2.6
R3
Stress(FSG)/MPa
2
3.4
4.2
5.2
6.4
7
Error/%
12.4
6.3
5.0
4.0
5.4
8.9
Stress(LFBG)/MPa
2.2
3.2
4
5
6.2
6.8
Error/%
23.6
0
0
0
2.1
5.8
Before the beginning of Step III, the values of P, F, and sensors are set to zero again based on the measured data in Step II. The measured strains at each loading step of Step III are shown in Table 5. Note that the relationship between F and strand strains does not match Equation (1) anymore because the force is undertaken by not only strand but also solid grout and steel tube. There are two notable characteristics in Table 5. On the one hand, the number of damaged FSGs grows with increasing load. By contrast, all LFBG sensors can measure the strains well in the entire loading process. On the other hand, although the strains in R1–R3 should be close in theory, the difference between the measured strains from S1–S3 is less than 10% only in the case of P ≤ 12 kN. This phenomenon may be attributed to the crack in grout occurring near R1 and R2. The chief reason for that is when P = 12 kN, the measured strain is about 150 με, which is close to the threshold of the tensile strain of most concrete. This phenomenon shows the durability of LFBG sensors in the case of grout cracking in practical prestress monitoring.
Table 5
The monitored strains of the strand at Step III. (Unit: με).
P/kN
3
6
9
12
15
18
21
24
F/kN
0.6
2.2
5.8
10.1
15.1
20.8
26.7
32.7
R1
E11
14
46
89
145
230
318
-
-
E12
16
63
105
155
258
376
516
682
E13
-
-
-
-
-
-
-
-
E14
6
34
73
123
-
-
-
-
E15
14
48
103
-
-
-
-
-
E16
8
42
88
153
233
-
-
-
Average strain(FSG)
12
47
92
144
240
347
516
682
S1
12
47
97
155
252
367
508
662
R2
E21
6
32
75
130
195
279
379
482
E22
-
-
-
-
-
-
-
-
E23
11
49
95
150
231
315
-
-
E24
11
43
92
141
221
312
425
551
E25
19
59
118
172
-
-
-
-
E26
22
66
116
174
260
365
-
-
Average strain(FSG)
14
50
99
153
227
318
402
517
S2
11
47
93
149
234
335
456
578
R3
E31
8
44
91
141
206
275
373
480
E32
14
50
98
157
236
-
-
-
E33
9
42
81
122
-
-
-
-
E34
19
61
-
-
-
-
-
-
E35
-
-
-
-
-
-
-
-
E36
6
33
74
124
196
273
384
-
Average strain(FSG)
11
46
86
136
213
274
379
480
S3
12
42
89
141
211
297
396
500
Based on Equations (3)–(7), Table 6 lists the itemized prestress losses calculated from the monitored strains. Because the temperature was kept constant during the test, σl3 is zero. In addition, σl7 is zero because the strand was not cut. σl5 is also zero because the interval between grout curing and loading was short. Compared with the losses calculated from the average values of the measured strains from the FSGs, the losses calculated from the measured strains from the LFBG sensors were closer to the true losses. The error in the latter is only half of that in the former. This result verifies that LFBG sensor has more accuracy than traditional FSG in prestress monitoring.
Table 6
Comparison of different prestress losses in the pre-tensioning experiment.
Itemized Prestress Loss
σl1 + σl2, II
σl2, I
σl3
σl4
σl5
σl6
σl7
Total Loss
True loss/MPa
44.3
- *
0
6.4
0 **
-
0
50.7
Loss(FSG)
Value/MPa
41.6
-
0
6.6
0
-
0
48.2
Error/%
−6.1
-
0
3.1
0
-
0
−4.9
Loss(LFBG)
Value/MPa
42.4
-
0
6.9
0
-
0
49.3
Error/%
−4.3
-
0
7.8
0
-
0
−2.8
* “-” denotes this loss does not exist in pre-tensioning case. ** “0” denotes that σl5 is small because the interval between grout curing and loading is short.
4.2. Post-Tensioning Test
4.2.1. Test Design
Details of the dimensions and reinforcement configuration of a simply-supported beam used in the experiment are shown in Figure 8a. The total length of the beam was 6000 mm, with a span of 5400 mm. The cross-section had a rectangular shape with 220 mm width and 450 mm depth. The compressive strength of the concrete was about 39 N/mm2. The elastic modulus and Poisson’s ratio of the concrete were 3.03 × 104 N/mm2 and 0.19, respectively. A curved duct with a diameter of 50 mm was embedded into the beam. The process of the test can be divided into two steps (Step I–II). At Step I, a 3-strand tendon was passed through the duct and tensioned by the jack with an increasing load from 0 to 120, 240, 360, 480 and 540 kN. To counteract the frictional loss, we overloaded the final tension force to 555 kN that is 3% higher than 540 kN. Because of the effect of the anchorage-seating loss σl1, the tensioning force reduced from 555 kN to 426.6 kN in the case of anchoring. At Step II, it took 72 h to observe the steel relaxation and creep of the concrete and for the strength of grout to reach 50 MPa.
Figure 8
Sketches and photographs of the experiment. (a) Applied tensioning to tendons; and (b) photographs of the restraining block and tensioning.
As shown in Figure 8a, we selected five regions located at the right linking point, 1/3 span, mid-span, 2/3 span, and left linking point (R1–R5) of the top strand for monitoring. Five LFBG sensors with a uniform gauge length of 250 mm were placed on R1–R5. 30 FSGs were successively attached on R1–R5 of the six helical wires of the strand. The numbering mode for the LFBG sensors and FSGs was the same as that in the last test. More details about the sensor installation and loading are illustrated in Figure 8b.
4.2.2. Results and Analysis
Different from the pre-tensioning case, the true stresses on R1–R5 cannot be obtained due to the frictional prestress loss distribution. Therefore, the theoretical prestress loss predictions by the Chinese Code [47] are used to replace the true prestress losses in the comparisons of σl2 and σl1. Table 7 gives the monitored strains from the FSGs and LFBG sensors at Step I. The differences between the maximum and minimum strains obtained from different wires also reaches or exceeds 10% of the applied strain. Assuming the average strain is approximate to the true strain, the large dispersion in the strain measurements demonstrates that the traditional short-gauge strain sensor is not suitable in prestress monitoring. Because the extending direction of the LFBG sensors is parallel to the tensioning force, most of the strains from LFBG sensor are larger than the average strains from FSG measurements at each loading step. This phenomenon also occurs in the previous test of pre-tensioning. Using Equation (9), Table 8 shows σl2 and σl1 calculated from LFBG sensor measurements at each loading step. Figure 9a,b show the comparisons between σl2 and σl1 calculated from the measured strains from the LFBG sensors and the theoretical predictions of prestress losses by the Chinese Code [47]. The developing trend of the calculated σl2 and σl1 are close to the loss profiles of theoretical predictions although there are some deviations between the calculated values and the predictions. This result also proves that the calculations for σl2 and σl1 are correct based on the strain measurements from the LFBG sensors.
Table 7
The monitored strains of the strand at Step I. (Unit: με).
F/kN
120
240
360
480
540
555
426.6
R1
E11
1371
2775
4193
5682
6368
6471
5214
E12
1336
2704
4111
5532
6218
6343
5111
E13
1300
2625
3993
5368
6046
6171
4807
E14
1257
2543
3786
5250
5846
5954
4968
E15
1325
2689
4161
5504
6243
6368
5125
E16
1382
2800
4229
5686
6371
6494
5227
Average strain(FSG)
1329
2689
4079
5504
6182
6300
5075
S1
1321
2689
4089
5529
6200
6336
5211
R2
E21
1357
2729
4179
5589
6289
6421
5546
E22
1318
2657
4079
5471
6132
6264
5439
E23
1264
2554
3896
5250
5932
6075
5271
E24
1236
2504
3807
5154
5825
5936
5154
E25
1289
2606
4006
5392
6079
6232
5451
E26
1361
2721
4204
5500
6236
6396
5496
Average strain(FSG)
1304
2629
4029
5393
6082
6221
5393
S2
1314
2657
4046
5461
6111
6250
5439
R3
E31
1321
2693
4125
5461
6150
6261
5461
E32
1296
2639
4046
5354
6036
6146
5375
E33
1254
2579
3893
5200
5896
6000
5246
E34
1229
2475
3829
5161
5686
5871
5164
E35
1243
2575
3950
5236
5875
5979
5229
E36
1351
2707
4115
5456
6142
6261
5432
Average strain(FSG)
1282
2611
3993
5311
5964
6086
5318
S3
1279
2607
3975
5307
5957
6061
5343
R4
E41
1282
2646
4025
5321
5986
6082
5404
E42
1279
2629
4036
5318
6007
6107
5421
E43
1204
2536
3793
5039
5646
5796
5129
E44
1189
2414
3743
5036
5579
5654
5079
E45
1218
2568
3871
5161
5807
5889
5275
E46
1329
2721
4057
5432
6114
6215
5575
Average strain(FSG)
1250
2586
3921
5218
5857
5957
5314
S4
1243
2571
3893
5182
5821
5911
5304
R5
E51
1236
2389
3861
5246
5814
5971
5689
E52
1246
2550
3936
5150
5761
5864
5618
E53
1186
2525
3900
5089
5721
5861
5518
E54
1182
2507
3789
5029
5650
5789
5554
E55
1150
2404
3257
4618
5193
5261
5018
E56
1286
2689
4097
5254
5975
6096
5731
Average strain(FSG)
1214
2511
3807
5064
5686
5807
5521
S5
1221
2525
3825
5079
5729
5829
5557
Table 8
σl2 and σl1 calculated from the strains of the LFBG sensors at Step I. (Unit: MPa).
Itemized Losses
σl2
σl1
P/kN
120
240
360
480
540
555
426.6
0 *
-
-
-
-
-
-
305.7
R1
20.8
32.2
37.2
34.2
45.0
53.8
225.0
R2
22.2
38.6
45.8
47.8
62.8
71.0
162.2
R3
29.2
48.6
60.0
78.6
93.6
108.8
143.6
R4
36.4
55.8
76.4
103.6
120.8
138.8
121.4
R5
40.8
65.0
90.0
124.2
139.2
155.2
54.4
* “0” is the zero point in the coordinate that represents the right end of the beam in Figure 8a.
Figure 9
The comparisons of the two calculated losses and the predictions according to the Chinese Code [44]: (a) σl2; and (b) σl1.
At Step II, Table 9 lists the strain decrements of R1–R5 in 72 h due to (1) steel relaxation of the strands; (2) creep and shrinkage of the concrete. The sum of the corresponding prestress losses, σl4 and σl5, are listed in Table 10. Compared with the data in Table 4, the losses in Table 10 imply that the major parts of the losses are triggered by the creep and shrinkage of concrete. Also, several FSGs are observed to be invalid in this step owing to the immersion of grout. The fact that the FBG sensors can measure during 72 h of grout curing again shows the durability to the sensing part of the LFBG sensor.
Table 9
The results of strain measurement from various sensors at Step II. (Unit: με).
Time/Hour
1
2
3
12
24
48
72
RR1
E11
5130
5111
5102
5052
5033
4999
4976
E12
5016
4988
4976
4923
4895
4862
4853
E13
4713
4687
4672
4609
4570
4544
4542
E14
4888
4868
4853
4790
4777
4752
4738
E15
5038
5012
5005
4955
4927
4899
4876
E16
5129
5097
5090
5021
4993
4955
4949
Average strain(FSG)
4985
4960
4949
4891
4865
4835
4822
S1
5141
5121
5113
5056
5026
4987
4970
RR2
E21
5450
5423
5411
5338
5329
5302
5275
E22
5348
5322
5309
5256
5231
5202
5183
E23
5182
5156
5137
5085
5057
5030
5006
E24
5068
5048
5039
4980
4963
4932
4905
E25
5362
5332
5317
5272
5256
5218
5197
E26
5402
5382
5377
5313
5293
5252
5248
Average strain of E21–E26
5302
5277
5266
5208
5189
5156
5136
S2
5366
5340
5324
5251
5223
5198
5184
RR3
E31
5407
5390
5377
5319
5310
5282
-
E32
5319
5295
5276
5245
5209
5180
5166
E33
5184
5162
5143
5097
5076
5044
5022
E34
5114
5097
5091
5041
5017
4986
-
E35
5175
5154
5144
5100
5082
5049
5029
E36
5377
5358
5350
5298
5287
5266
5246
Average strain of E31–E36
5263
5243
5230
5183
5164
5135
5116
S3
5266
5241
5231
5167
5155
5131
5118
RR4
E41
5309
5283
5270
5210
5174
5151
5126
E42
5321
5290
5281
5218
5181
5155
5121
E43
5035
5011
5004
4946
4907
4883
4848
E44
4991
4977
4964
4909
4876
4851
4825
E45
5184
5152
-
-
-
-
-
E46
5484
5454
5431
5371
5346
5319
5271
Average strain of E41–E46
5221
5195
5190
5131
5097
5072
5038
S4
5215
5191
5180
5108
5070
5021
4999
RR5
E51
5580
5544
5529
5451
5430
5392
5375
E52
5519
5507
5491
5447
5411
5380
5345
E53
5422
5406
5387
5310
5281
5252
-
E54
5454
5423
-
-
-
-
-
E55
4914
4878
4869
4808
4771
4736
4712
E56
5631
5592
5565
5562
5544
5504
5479
Average strain of E51–E56
5420
5392
5368
5316
5287
5253
5228
S5
5459
5432
5407
5363
5323
5271
5239
Table 10
The sum of σl4 and σl5 calculated from the strains obtained from the LFBG sensors. (Unit: MPa).
Itemized Losses
σl4+ σl5
Time/hour
1
2
3
12
24
48
72
0 *
17.3
21.7
26.1
35.7
42.1
45.3
46.3
R1
14.0
18.0
19.6
31.0
37.0
44.8
48.2
R2
14.6
19.8
23.0
37.6
43.2
48.2
51.0
R3
15.4
20.4
22.4
35.2
37.6
42.4
45.0
R4
17.8
22.6
24.8
39.2
46.8
56.6
61.0
R5
19.6
25.0
30.0
38.8
46.8
57.2
63.6
* “0” is the zero point in the coordinate that represents the right end of the beam in Figure 8a.
5. Verification for the Prestress Loss Monitoring Using LFBG: In-Site Monitoring
The specific aims regarding in-site monitoring are to observe whether the LFBG sensors installed by the proposed installation procedure in Section 2.3 are valid in long-term monitoring, and to obtain the itemized prestress losses in practical post-tensioning to ensure the security of the construction.
5.1. Member Fabrication and Sensor Placement
This practical prestress loss monitoring was based on the project of Multifunctional Drama Hall of the Fuzhou Straits Cultural Art Center in Fujian Province, China. The monitored beam had a length of 18.475 m. The width and the height of the beam were 1.3 m and 0.7 m, respectively. Details of the dimensions and reinforcement configuration are shown in Figure 10. Three 7-strand tendons were passed the curved duct, and all strands in three tendons had an identical nominal diameter of 15.2 mm. The ultimate tensile strength and elastic modulus of the strand were 1860 MPa and 200 GPa, respectively. The tensioning was controlled by the oil-pressure gauge of the jack used to apply tensioning to the tendons. There are three loading steps including 10 MPa, 20 MPa, and 28 MPa shown in the oil-pressure gauge to apply the prestresses of 358.40 MPa, 728.0 MPa, and 1023.7 MPa to the tendon, respectively. The applied prestress in the tendon at the final loading step contained an overstressing of 3% to counteract the frictional loss. Due to the anchorage-seating loss σl1, the applied prestress decreased from 1023.7 MPa to 862.3 MPa.
Figure 10
The schematic of the monitored beam in in-site measurement.
The six outer strands of the mid-tendon named as w1–w6 were used for prestress monitoring. As shown in Figure 10, two monitored regions were set nearby the linking points in the strands. 12 LFBG sensors were fixed in the regions. The numbering mode for the LFBG sensors is as follows. The six LFBG sensors on R1 of W1–W6 are named as S11–S16. The first number means the sensor is in R1, and the second number represents the number of the strand. The other six LFBG sensors on R2 of W1–W6 are named as S21–S26. At tensioning, the sensors measured the strain increments of each strand in each loading step. When the tensioning was finished, and the prestress began to transfer to the beam, the strain data were measured continuously. The entire monitoring lasted about 90 days, and all data were updated by temperature compensation.Moreover, all LFBG sensors were installed by the installation method proposed in Section 2.3. Figure 11a–d show the whole process of sensor placement.
Figure 11
Photographs of the LFBG sensor deployment in in-site monitoring: (a) Peeling the marked region to expose the tendon; (b) attaching the LFBG sensors on the strands; (c) connecting the sensor to the optical cable; and (d) connecting the protection sleeve to the pipe.
5.2. Results and Analysis
Table 11 lists the measured strains of the six helical strands and the average strains at each loading step in tensioning. The strains distributing in the strands are quite dispersed, and the deviation between the maximum and minimum strain can reach 50% of the average applied strains. This phenomenon implies that some strands such as w2 and w3 were still loose before the tensioning was applied. Moreover, the strand w1 may be ruptured earlier than other strands because it undertakes the extra prestress. Thus, a remarkable conclusion that can be derived from the data shown in Table 11 is that monitoring prestress in a tendon merely from the measured strains in one of the six helical wires using the traditional “short-gauge” strain sensor may ignore the uneven strain distribution in the same section. Table 12 and Table 13 give σl2 and σl1 calculated from the measured strains and their prediction based on the Chinese Code [47]. The fact that the calculated losses are close to the predictions implies that the prestress loss calculations are correct in principle based on the strain measurements from the LFBG sensors.
Table 11
The monitored strains of the strands at tensioning. (Unit: με).
Applied Stress/MPa
358.4
728.0
1023.7
862.3
R1
S11
2456
4938
6755
6196
S12
1320
3067
4254
3606
S13
1428
2941
4325
3972
S14
1621
3461
4988
4298
S15
1913
3911
5495
4805
S16
2066
3638
5091
4611
Average strain of S11–S16
1801
3659
5151
4581
R2
S21
2361
4705
6568
6561
S22
1074
2532
3643
3628
S23
759
1771
3003
2977
S24
1945
3832
5162
5151
S25
1888
3609
5152
5134
S26
2027
3898
4949
4931
Average strain of S21–S26
1676
3391
4746
4730
Table 12
σl2 and σl1 calculated from the strains of the LFBG sensors. (Units: MPa).
Itemized Prestress Losses
σl2
σl1
Applied stress
358.4
728.0
1023.7
862.3
R1
w1
−120.5
−234.9
−293.5
109
w2
101.0
129.9
194.2
126.3
w3
79.9
154.5
180.3
68.9
w4
42.3
53.1
51.0
134.6
w5
−14.6
−34.6
−47.8
134.5
w6
−44.5
18.4
31.0
93.6
Average(LFBG) *
7.3
14.4
19.2
111.2
Prediction(Code) **
7.9
16.0
22.5
108.4
R2
w1
−102.0
−189.5
−257.1
1.4
w2
149.0
234.3
313.3
2.9
w3
210.4
382.7
438.1
5.1
w4
−20.9
−19.2
17.1
2.2
w5
−9.8
24.2
19.1
3.5
w6
−36.9
−32.1
58.6
3.6
Average(LFBG) *
31.6
66.7
98.2
3.1
Prediction(Code) **
29.4
59.7
83.9
0
* represents the average stresses or prestress losses calculated from strains obtained from the LFBG sensors. ** the values are estimated based on the Chinese Code [47].
Table 13
The monitored strains of the strands at the in-service stage. (Unit: με).
Time
R1
R2
W1
W2
W3
W4
W5
W6
Average
W1
W2
W3
W4
W5
W6
Average
0
6196
3606
3972
4298
4805
4611
4581
6561
3628
2977
5151
5134
4931
4730
12 h
6052
3461
3875
4137
4681
4409
4436
6343
3454
2833
4961
4990
4800
4564
24 h
6031
3443
3857
4121
4663
4387
4417
6329
3436
2815
4950
4973
4782
4548
36 h
6020
3434
3838
4116
4654
4363
4404
6321
3427
2806
4937
4964
4771
4538
48 h
6011
3425
3819
4112
4645
4344
4393
6315
3418
2797
4923
4955
4766
4529
9 days
5959
3356
3780
4069
4582
4280
4338
6252
3353
2749
4876
4904
4714
4475
30 days
5862
3225
3717
3983
4496
4183
4244
6154
3236
2636
4776
4813
4626
4374
51 days
5810
3163
3695
3953
4459
4164
4207
6119
3209
2606
4718
4773
4599
4337
72 days
5794
3151
3686
3933
4433
4152
4192
6104
3194
2593
4694
4760
4582
4321
90 days
5784
3143
3683
3923
4422
4146
4183
6098
3181
2589
4681
4758
4570
4313
Table 13 records the strain reductions of W1–W6 due to steel relaxation of strands and creep of concrete in 90 days after anchoring. The calculated sum of the prestress losses, σl4 and σl5, is listed in Table 14 and illustrated in Figure 12.
Table 14
The sum of σl4 and σl5 calculated from the strains obtained from the LFBG sensors. (Units: MPa).
Time
R1
R2
W1
W2
W3
W4
W5
W6
Average
W1
W2
W3
W4
W5
W6
Average
12 h
28.1
28.3
18.9
31.4
24.2
39.4
28.4
42.5
33.9
28.1
37.1
28.1
25.5
32.5
24 h
32.2
31.8
22.4
34.5
27.7
43.7
32.1
45.2
37.4
31.6
39.2
31.4
29.1
35.7
36 h
34.3
33.5
26.1
35.5
29.4
48.4
34.5
46.8
39.2
33.3
41.7
33.2
31.2
37.6
48 h
36.1
35.3
29.8
36.3
31.2
52.1
36.8
48.0
41.0
35.1
44.5
34.9
32.2
39.3
9 days
46.2
48.8
37.4
44.7
43.5
64.5
47.5
60.3
53.6
44.5
53.6
44.9
42.3
49.9
30 days
65.1
74.3
49.7
61.4
60.3
83.5
65.7
79.4
76.4
66.5
73.1
62.6
59.5
69.6
51 days
75.3
86.4
54
67.3
67.5
87.2
73.0
86.2
81.7
72.3
84.4
70.4
64.7
76.6
72 days
78.4
88.7
55.8
71.2
72.5
89.5
76.0
89.1
84.6
74.9
89.1
72.9
68.1
79.8
90 days
80.3
90.3
56.4
73.1
74.7
90.7
77.6
90.3
87.2
75.7
91.7
73.3
70.4
81.4
Figure 12
The increment of the sum of σl4 and σl5 for 90 days: (a) R1; and (b) R2.
There are three features that may be observed in Table 14 and Figure 12. First, the phenomenon that all LFBG sensors can trace the stress variation proves that the LFBG has enough durability for long-term prestress loss monitoring, and the proposed installation method is valid. Second, the increment of the sum of σl4 and σl5 in each strand has a similar trend. It proves the stability of the LFBG in measurements. Finally, almost 50% losses are completed in 48 h and the monitored data become stable after the 51st day. This feature shows that the prestress loss monitoring should be applied at an early stage of prestressing and last until the loss data tends to stabilize.
6. Conclusions
We demonstrated the deployment of the LFBG sensor for prestress loss monitoring and Evaluation. An appropriate length design of LFBG sensor and the installation method were proposed. Then we showed the calculation methods for the itemized prestress losses in pre-tensioning and post-tensioning. The applicability of the LFBG for prestress loss monitoring was verified by experiments in the laboratory and in-site monitoring. From the results and discussions, the following conclusions can be drawn:An appropriate gauge length for LFBG sensor is at least 25 cm for prestress loss monitoring in the strand because the gauge can obtain the average strain by covering the six helical wires.Severe frictions between the strand and duct and the grout crack can bring accidental damage to LFBG sensor. The proposed installation method can prevent the LFBG sensor from these ruptures effectively occurring at not only tendon tensioning but also structure loading. The durability and stability of the LFBG sensor are proved to be better than those of traditional FSGs.The proposed calculation method acquired the itemized prestress losses at different stages of applying pretension accurately. Our results from the experiments including the cases of pre-tensioning and post-tensioning showed that the losses calculated from the measured strains of the LFBG sensors were more precise compared to those calculated from traditional FSGs. Moreover, from the in-site monitoring, we obtained the uneven stress distribution in different strands, measured the immediate losses at tensioning, and traced the time-dependent losses for 90 days. Thus, this calculation method can be easy to apply in the itemized prestress losses monitoring.Compared with the traditional electrical sensor, the LFBG sensor is proved to have better durability for long-term prestress loss monitoring in practice, especially in the case of grout cracking and aggressive environment.