A Review of Fibre Reinforced Polymer Structures
Abstract
:1. Introduction
2. FRP Applications
2.1. All-FRP New-Build Structurs
2.2. FRP as Reinforcement
2.3. FRP in Strengthening Applications
3. Materials and Manufacturing
3.1. Constituent Materials
3.1.1. Fibres
- E-glass (electrical glass);
- A-glass (window glass);
- C-glass (corrosion resistant, also known as AR-glass or alkali- resistant glass);
- S-glass (Structural or high-strength glass).
Material | Grade | Density (g/cm3) | Tensile Modulus (GPa) | Tensile Strength (MPa) | Max Elongation (%) | Fibre Architecture | Glass Transition Temperature (°C) | |
---|---|---|---|---|---|---|---|---|
Fibre | Glass | E | 2.57 | 72.5 | 3400 | 2.5 | Isotropic | - |
A | 2.46 | 73.0 | 2760 | 2.5 | ||||
C | 2.46 | 74.0 | 2350 | 2.5 | ||||
S | 2.47 | 88.0 | 4600 | 3.0 | ||||
Carbon | Standard | 1.70 | 250.0 | 3700 | 1.2 | Anisotropic | - | |
High strength | 1.80 | 250.0 | 4800 | 1.4 | ||||
High modulus | 1.90 | 500.0 | 3000 | 0.5 | ||||
Ultrahigh modulus | 2.10 | 800.0 | 2400 | 0.2 | ||||
Aramid | - | 1.40 | 70.0–190.0 | 2800–4100 | 2.0–2.4 | Anisotropic | ||
Polymer Resin | Polyester | - | 1.20 | 4.0 | 65 | 2.5 | - | 70–120 |
Epoxy | - | 1.20 | 3.0 | 90 | 8.0 | - | 100–270 | |
Vinylester | - | 1.12 | 3.5 | 82 | 6.0 | - | 102–150 | |
Phenolic | - | 1.24 | 2.5 | 40 | 1.8 | - | 260 | |
Polyurethane | - | varies | 2.9 | 71 | 5.9 | - | 135–140 [75] |
- Standard modulus (SM);
- Intermediate modulus (IM);
- High strength (HS);
- Ultrahigh modulus (UHM).
- Rovings—parallel bundles of continuous untwisted filaments;
- Yarn—bundles of twisted filaments;
- Fibre mats with chopped or continuous fibres;
- Woven and non-woven fabrics;
- Stitched fabrics, grid, mesh and fleece;
- Carbon fibre tows.
3.1.2. Polymer Resins
3.1.3. Other Materials—Additives and Fillers
3.2. Manufacturing Process
3.2.1. Pultrusion
3.2.2. Hand or Wet Layup
3.2.3. Other Manufacturing Processes
3.3. Sustainabilty of FRP Materials
4. FRP Plate-to-Plate Bolted Connections
4.1. Failure Modes
4.1.1. Bearing Failure
4.1.2. Net-Tension Failure
4.1.3. Shear-Out Failure
4.1.4. Cleavage Failure
4.2. Effect of Geometry
- Bearing failure is a pseudo-ductile failure giving us warning before failure;
- Connections should be designed for bearing failure, if practically possible;
- Bearing failure is enforced if e1/d0 > 3 and w/d0 ≥ 4;
- Shear-out failure happened when e1/d0 ≤ 4;
- Net-tension failure happened when w/d0 ≤ 3;
- Net-tension and cleavage are brittle failures and should be avoided;
- Increase in plate thickness and width increases connection resistance;
- For values beyond e1/d0 > 2.5 and w/d0 > 4, there is no change in connection resistance;
- Bolt-diameter-to-plate-thickness ratio should be in the range of 1.0 ≤ (d/t) ≤ 1.5 for ensuring the ductile bearing failure mode.
4.3. Effect of Fibre Orientation
- Strength and stiffness decrease when pultrusion angle changes from 0° to 90°;
- Bearing failure happens for off-axis pultrusion angle lower than 45°;
- Net-tension failure occurs for off-axis pultrusion angle greater than 45°.
4.4. Effect of Fastener Parameters and Lateral Restraint
- Connection strength with FRP bolt is about half the strength using steel bolt;
- Bolt thread reduces bearing strength; threaded pin-bearing strength is 0.6 of the plain pin-bearing strength;
- Pin-bearing strength is reduced by 20–30% by hot-wet aging
- Clearance hole of 1.6 and 6.4 mm leads to 2% and 9% reduction, respectively, in connection resistance compared with no-clearance condition;
- Bolt clearance hole of 1.6 to 2 mm is acceptable for ease in fabrication;
- Lightly clamped (3 Nm) and fully clamped (30 Nm) connections showed a 45% and 80% increase in load compared to pin-bearing state (0 bolt torque with no lateral restraint);
- Bolt torque increases connection resistance;
- Bolt tightening cannot be relied on due to viscoelastic nature of FRP;
- Connection strength increases with confinement area.
4.5. Multi-Bolted Connections
- The strongest connection that can fail in bearing has only single row of bolts;
- The failure in multi-bolted connections is either net-tension or cleavage;
- Connection resistance may not be sum of load per bolt;
- First row transfers more load than the other rows;
- Connection strength depends on bolts numbers but may not be directly proportional;
- Only 25% increase in strength is achieved by adding a second row with two bolts;
- Resin injected bolted connections are suitable for FRP bridges;
- Basalt FRP bolts can replace steel bolts.
Parameter | Researcher | Set Up | e1/d0 | w/d0 | Main Findings |
---|---|---|---|---|---|
Geometry | Rosner, Rizkalla [93,102,103] | Double-lap | 0.9–10 | 1.2–12.2 |
|
Abd-El-Naby and Hollaway [108] | Double-lap: high fibre volume |
| |||
Turvey and Cooper [104] | Double-lap | 2–8 | 2–8 |
| |
Wang [90] | Bearing load via steel pin and no lateral restraints | 1–5 | 2–8 |
| |
Turvey [105,106] | Single-lap | 1.5–4 |
| ||
Lee [109] | Double-lap | 2–7 | 5–7 |
| |
Fibre orientation | Rosner [102,103] | Double-lap |
| ||
Turvey, Cooper [101,110] | Double-lap Fibre: 0°, 30°, 45°, 90° | 2–6 | 4–10 |
| |
Yuan and Liu [111] | Double-lap, Fibre: 0°, 15°, 30°, 45°, 60°, 75°, 90° | 3 | 7 |
| |
Fastener parameters | Erki [112] | Double-lap |
| ||
Yuan et al. [113] | Double-lap |
| |||
Mottram [87,89,94,114] | Semi-notched FRP samples with pin |
| |||
Lateral restraint | Abd-El-Naby [108] | Double-lap |
| ||
Cooper Turvey [101] | Double-lap |
| |||
Khashaba [115] |
| ||||
Yuan and Liu [111] | Double-lap |
| |||
Multi-bolted connections | Hart-Smith [97] | Theoretical model |
| ||
Abd-El-Naby [107] | Double-lap |
| |||
Prabhakaran [116,117] | Double-lap (Row × bolts): (2 × 1), (1 × 2) and (2 × 2) |
| |||
Hassan [118,119] | Double-lap (2 × 1), (1 × 2) (3 × 1), (1 × 3) and (2 × 2) Fibre: 0, 45, 90 | 2–5 | 9.9–14.8 |
| |
Ascione [120] | Double-lap 9 bolts |
| |||
Mottram [98] | Theoretical |
| |||
Abdelkerim [121,122] | Double-lap BFRP |
| |||
Qureshi [123,124,125,126] | Double-lap |
| |||
Mottram, Turvey [88,127] | Review papers |
|
5. FRP Bolted Frame Joints
5.1. Joints Subjected to Monotonic Loading
- Steel-like joint detailing is not suitable for FRP joints;
- Use of FRP cleats leads to delamination cracking at the heel of the angle;
- Use of steel cleats results in tensile tearing of column flange from web;
- Adhesive bonding on its own is not suitable for FRP joints;
- Hybrid joints combining bolting and bonding are suggested for fail-safe mechanism;
- Semi-rigid analysis is suggested due to limited commercially available FRP profiles;
- Top cleat is the main weakness in FRP joints for I-shaped sections;
- Connectors using different fibre architecture are proposed to replace top cleat;
- First failure defined as start of hairline cracking or audible acoustic emissions;
- First failure or damage onset is related to prying due to hogging moments;
- Cuff/sleeve connectors with steel tube and plate are useful for joining box sections;
- Serviceability deflection limit for FRP beams is span/340;
- FRP web cleats possess sufficient tying resistance for robustness;
- The flexural strength of beam–column joints using pultruded FRP plate sandwiched between built-up channel sections is about 20 times higher than the conventional beam–column joints with web/flange cleats;
- In a three bolted web cleated joint, the middle bolt is unnecessary.
5.2. Joints Subjected to Cyclic Loading
- Steel-like joints are inefficient in resisting cyclic loading;
- Web-flange junction of I-shaped profiles is the weakest spot;
- Alternative manufacturing suggested for producing cleat pieces;
- Most joint details produced low dissipated energy and almost no ductility.
- FRP frames with infill walls showed better cyclic performance;
- Hybrid joints produced higher dissipated energy than bolted only joints;
- Bonded sleeve joints and joints between tubular profile and built-up channel sections showed promising cyclic behaviour;
- Flange cleated or web and flanged cleated combined showed same cyclic response and therefore, flange cleats are redundant as they make no difference to cyclic joint behaviour;
- Only steel connecting components are used to join tubular sections; no effort made to try FRP connecting elements;
- A guide for cyclic testing of FRP joints should be developed; presently FRP testing relies heavily on testing procedures from steel structures;
- Several cyclic loading protocols are dependent on yielding of steel, which is absent in FRP
6. Setbacks and Future
7. Conclusions and Research Growth Areas
- Joint detailing from steel structures is not suitable for FRP structures;
- There is no design code for FRP beam-to-column joints;
- Available formulae for beam–column joints are taken from plate-plate connections;
- Design of FRP members is controlled by serviceability deflections;
- Tubular members are better suited for FRP structures due to high buckling resistance;
- Use of FRP cleats leads to delamination cracking;
- Use of steel cleats results in outward flexural deformation in I-shaped FRP columns;
- Choice of FRP section sizes is limited; semi-rigid analysis may help in better economy
- Bearing is the most desirable and ductile failure in plate-plate connections;
- Connection strength depends on geometry, lateral restraint, fastener parameters, fibre orientation and number of bolt rows.
- FE modelling with progressive failure can be useful to estimate joints’ behaviour;
- Environmental considerations, fire performance and durability should be studied;
- A comparison between single-lap and double-lap plate-to-plate connections;
- Extreme loading conditions, such as blast, earthquake, dynamic and impact loads.
- Robustness and disproportionate collapse of all-FRP structures;
- Plate thickness, pitch and gauge distance, staggered bolts should be investigated;
- More research is needed on serviceability deflection limits for different joint detailing.
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Conflicts of Interest
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Estimated Fibre Volume | 25–40% | ||
Fibre architecture | Roving and mat | ||
Strength (MPa) | Tensile | Longitudinal | 207–317 |
Transverse | 48–83 | ||
Compressive | Longitudinal | 207–359 | |
Transverse | 110–138 | ||
Shear | In-plane | 31–48 | |
Out-of-plane | 27–31 | ||
Flexural | Longitudinal | 207–338 | |
Transverse | 69–131 | ||
Bearing | Longitudinal | 207–269 | |
Transverse | 179–234 | ||
Modulus (GPa) | Tensile | Longitudinal | 18–28 |
Transverse | 6–10 | ||
Compressive | Longitudinal | 18–26 | |
Transverse | 7–13 | ||
Shear | In-plane | 3.0–3.4 | |
Flexural | Longitudinal | 11–14 | |
Transverse | 6–12 | ||
Poisson’s ratio | Longitudinal | 0.33–0.35 |
Property | Material | |||
---|---|---|---|---|
Steel | GFRP | CFRP | AFRP | |
Longitudinal modulus (GPa) | 200 | 35 to 60 | 100 to 580 | 40 to 125 |
Longitudinal tensile strength (MPa) | 450 to 700 | 450 to 1600 | 600 to 3500 | 1000 to 2500 |
Ultimate tensile strain (%) | 5 to 20 | 1.2 to 3.7 | 0.5 to 1.7 | 1.9 to 4.4 |
Property | GFRP | CFRP | AFRP |
---|---|---|---|
E-Glass/Epoxy | Carbon/Epoxy | Kevlar 49/Epoxy | |
Fibre volume fraction | 0.55 | 0.65 | 0.60 |
Density (kg/m3) | 2100 | 1600 | 1380 |
Longitudinal modulus (GPa) | 39 | 177 | 87 |
Transverse modulus (GPa) | 8.6 | 10.8 | 5.5 |
In-plane shear modulus (GPa) | 3.8 | 7.6 | 2.2 |
Major Poisson’s ratio | 0.28 | 0.27 | 0.34 |
Minor Poisson’s ratio | 0.06 | 0.02 | 0.02 |
Longitudinal tensile strength (MPa) | 1080 | 2860 | 1280 |
Transverse tensile strength (MPa) | 39 | 49 | 30 |
In-plane shear strength (MPa) | 89 | 83 | 49 |
Ultimate longitudinal tensile strain (%) | 2.8 | 1.6 | 1.5 |
Ultimate transverse tensile strain (%) | 0.5 | 0.5 | 0.5 |
Longitudinal compressive strength (MPa) | 620 | 1875 | 335 |
Transverse compressive strength (MPa) | 128 | 246 | 158 |
Researcher | Set Up | Sizes | Joint Configuration | Main Findings |
---|---|---|---|---|
Bank [129,130,131] | Direct Compression |
|
|
|
Mottram [24,132,133,134] | Double cantilever |
|
|
|
Mosallam [135,136] | Direct compression |
|
|
|
Qureshi [27,28,29,137] | Double cantilever |
|
|
|
Turvey [138,139,140,141,142] | Double cantilever |
|
|
|
Qureshi [80] | Tension pull test |
|
|
|
Smith [143,144,145] | Direct Compression |
|
|
|
Zafari [33,146] | Single cantilever |
|
|
|
Russo [147,148,149] | Simply supported beam |
|
|
|
Zhang [150] | Single cantilever |
|
|
|
Martins [151,152,153] | Single cantilever and full frame |
|
|
|
Ascione [18,154] | Single cantilever |
|
|
|
Mosallam [155] | Web-flange junction tests |
|
|
|
Researcher | Set Up | Sizes | Joint Configuration | Main Findings |
---|---|---|---|---|
Bruneau and Walker [156] | Simply support beam |
|
|
|
Mosallam [135] | Direct compression |
|
|
|
Smith [144,145], Singamsethi [157], Carrion [158] | Direct compression |
|
|
|
Zhang, Qiu [150,159,160] | Single cantilever or beam splice connection |
|
|
|
Martins [161,162] | Single cantilever |
|
|
|
Razaqpur [163] | Single cantilever |
|
|
|
Qureshi [8,128] | Single cantilever |
|
|
|
Test Set Up | Joint Configuration | Advantages and Findings | Limitations |
---|---|---|---|
Direct compression | - |
|
|
Simply supported beam | - |
|
|
Double cantilever beam | - |
|
|
Single cantilever beam | - |
|
|
Full scale frame | - |
|
|
- | Cleated joints |
|
|
- | Sleeve/cuff joints |
|
|
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Qureshi, J. A Review of Fibre Reinforced Polymer Structures. Fibers 2022, 10, 27. https://doi.org/10.3390/fib10030027
Qureshi J. A Review of Fibre Reinforced Polymer Structures. Fibers. 2022; 10(3):27. https://doi.org/10.3390/fib10030027
Chicago/Turabian StyleQureshi, Jawed. 2022. "A Review of Fibre Reinforced Polymer Structures" Fibers 10, no. 3: 27. https://doi.org/10.3390/fib10030027
APA StyleQureshi, J. (2022). A Review of Fibre Reinforced Polymer Structures. Fibers, 10(3), 27. https://doi.org/10.3390/fib10030027