| Literature DB >> 35859704 |
Naresh Kumar1, L Natrayan2, G Kasirajan3, S Kaliappan4, M D Raj Kamal4, Pravin P Patil5, Muse Degefe Chewaka6.
Abstract
Natural fibre reinforcement is used in important sectors such as medical, aerospace, automobile, and many other fields. Many articles have reported that natural fibre has the potential to replace synthetic fibres. Natural fibre reinforcement has given good results as a brake friction material. It has already been proven that asbestos causes lung cancer and mesothelioma in brakes. Many people died from the effects of asbestos. According to the World Health Organization's trending brake report, this material leads to serious health issues. This work is going on for the replacement of these materials. Mulberry fibre is a unique material, and PAN fibre is combined with mulberry fibre and used as a brake reinforcement material to replace Kevlar fibre. The brake pads were fabricated with the various wt% of mulberry fibres and PAN fibre [3-12%] with an equal ratio and aramid fibre [3-6%] in the hydraulic hind brake moulding machine. The mechanical, chemical, physical, tribological, and thermal properties were evaluated. MF-2 [6 wt%] mulberry-PAN-fibre-based brake pad composites have shown better results for ultimate shear strength and proof stress, tensile strength, compressive strength, and impact energy.Entities:
Year: 2022 PMID: 35859704 PMCID: PMC9293573 DOI: 10.1155/2022/6426763
Source DB: PubMed Journal: Bioinorg Chem Appl Impact factor: 4.724
Figure 1(a) PAN fibre. (b) Raw material of mulberry fibre. (c) Developed brake pads of mulberry-PAN fibre.
Composite fabrication details.
| Condition for moulding | Procedure |
|---|---|
| Mixing condition | (i) Proper mixing of basic braking ingredients [phenolic resin, mulberry fibre, PAN fibre/aramid, and Lapinus ingredients for ten minutes] |
| (ii) The other remaining ingredients were mixed with previous ingredients [graphite, potassium barium, titane, vermiculite, and aluminum oxide and vermiculite mixed for next another 10 minutes] | |
| Conditions for moulding |
|
| Condition for oven curing | Time( |
where t = time, P = pressure, T = temperature.
Compositional details of materials.
| Fabrication of the composites | |||||||
|---|---|---|---|---|---|---|---|
| Sr No | Ingredients used | FK-1 | FK-2 | MF-1 | MF-2 | MF-3 | MF-4 |
| 1 | Aramid | 5 | 10 | 0 | 0 | 0 | 0 |
| 2 | Mulberry fibre [reinforced] | 0 | 0 | 1.5 | 3 | 4.5 | 6 |
| 3 | PAN fibre [reinforced] | 0 | 0 | 1.5 | 3 | 4.5 | 6 |
| 4 | Alumina [friction] | 5 | 5 | 5 | 5 | 5 | 5 |
| 5 | Lapinus [modifier] | 15 | 15 | 15 | 15 | 15 | 15 |
| 6 | Potassium titane | 5 | 5 | 5 | 5 | 5 | 5 |
| 7 | St. Phenolic Resign [binder] [binder] | 10 | 10 | 10 | 10 | 10 | 10 |
| 8 | Graphite [lubricant] | 5 | 5 | 5 | 5 | 5 | 5 |
| 9 | Barium [filler] | 50 | 45 | 52 | 49 | 46 | 43 |
| 10 | Vermiculite [modifier] | 5 | 5 | 5 | 5 | 5 | 5 |
Figure 2Chase machine for the tribological test.
Characterizations of mulberry fibre and PAN fibre and aramid fibre composites [mechanical, physical, and chemical].
| Properties | Standard followed | % and units | 3% Kevlar FK-1 | 6% Kevlar FK-2 | 3% Fibre [MF-1] | 6% Fibre [MF-2] | 9% Fibre [MF-3] | 12% Fibre [MF-4] |
|---|---|---|---|---|---|---|---|---|
| Compressibility | ISO 6310 | % [percentage] | 1.25 | 1.37 | 1.40 | 1.69 | 1.73 | 1.76 |
| Water | ISO 6310 | % [percentage] | 1.70 | 1.80 | 1.77 | 1.86 | 1.90 | 2.20 |
| Porosity of newly developed composites | JISD 4418 standard | % [percentage] | 3.25 | 3.32 | 3.4 | 3.70 | 4.12 | 4.05 |
| Heat swelling | SAE J 160 JNU80 | % [percentage] | 1.3 | 1.76 | 1.45 | 1.53 | 1.74 | 1.79 |
| Ash content | ASTMD570-98 | % [percentage] | 75.30 | 72.48 | 74.75 | 74.07 | 72.98 | 71.06 |
| Density | ASTM C271/C271 M-16 | (g/cm3) [Gram per centimeter cubic] | 2.45 | 2.40 | 2.38 | 2.20 | 2.14 | |
| Hardness | Rockwell-R-scale | HRR | 116.6 | 113.2 | 112.8 | 111.6 | 109.5 | 103.9 |
| Acetone extraction | ASTMD494 | % [percentage] | 0.57 | 0.53 | 0.59 | 0.64 | 0.68 | 0.71 |
| Impact energy | Standard | (J) [joule] | 0.289 | 0.276 | 0.252 | 0.326 | 0.224 | 0.206 |
| Shear strength | ASTM D256 | (kgf) [kilogram force] | 1870 | 2090 | 2267 | 2520 | 1932 | 1721 |
| Tensile strength | ASTM D732 | (MPa) [Mega-Pascal] | 17.45 | 17.34 | 15.4 | 16.8 | 13.2 | 11.8 |
| Flexural strength | ASTM E8 | (MPa) [Mega-Pascal] | 62.83 | 60.23 | 59.78 | 55.37 | 51.12 | 50.34 |
| Tensile modulus | ASTM D790 | (MPa) [mega-Pascal] | 4450 | 4518 | 4257 | 3956 | 3784 | 3657 |
| Flexural modulus | ASTM E8 | (GPa) [Mega-Pascal] | 2.60 | 2.78 | 2.55 | 2.50 | 2.35 | 2.30 |
| Failure strain | ASTM D790 | (%) [Percentage] | 1.20 | 1.24 | 1.48 | 1.54 | 1.60 | 1.69 |
| Proof stress | ASTM E8 | (MPa) [Mega-Pascal] | 3.4 | 2.9 | 2.8 | 3.6 | 3.2 | 2.75 |
| Ultimate compressive strength | ASTM E8 | (MPa) [Mega-Pascal] | 162.3 | 167.5 | 165.7 | 176 7 | 160.9 | 140.6 |
Attributes used in Tri-biological performance.
| Attributes used | Favourable |
|---|---|
| Wear rate | Wear should show minimum values |
| COP | Coefficient performance should show the highest values |
| Recovery% | Recovery percentage should be high as possible and favourable more than 100% |
| % Fade | Fade should show minimum values |
|
| The recovery coefficient should show the highest values |
|
| The variability coefficient should show the lowest values |
| ∆ | The fluctuation coefficient should show minimum values |
Figure 3Fade and recovery cycles of developed samples.
Figure 4Frictional Behavior of Sμ [stability coefficient] and Vμ [variability coefficient] of developed composites.
Figure 5Frictional behavior of fade %F and %R of developed composites.
Figure 6µ Behavior of developed composites.
Figure 7Frictional (COF) and wear behavior of advanced composites.
Figure 8TGA of mulberry-PAN fibre and aramid-based composites in O2 and N2 atmosphere.