Comparative Analysis of Polyurethane Drive Belts with Different Cross-Section Using Thermomechanical Tests for Modeling the Hot Plate Welding Process
Abstract
:1. Introduction
1.1. Origins of the Research Problem
1.2. Hot Plate Welding Process
- Developing a mathematical model of the welding process, which will be used to derive the relationship of welding parameters to the process input sizes (material type, belt diameter),
- Belt alignment on the surface of the hot plate (Figure 1a), during which the ends of the belt (1), captured by the jaws (2), are pre-pressed to the surface of the hot plate (3) at velocity vm. Upon reaching contact between the hot plate and the belt ends, they are pressed against it with force Fm. This action is intended to pre-melt uneven parts of the belt head and adjust it to the surface of the hot plate in order to improve heat conduction conditions,
- Proper heating (Figure 1b), during which the belt ends (1) are pressed against the hot plate (3) with force Fh, resulting in the belt heating along its axis. This stage ends when the welding temperature Tw is reached at a distance p from the surface of the hot plate,
- The hot plate (3) removing from the area between the belt ends (1) (Figure 1c),
- The belt connecting (Figure 1d), during which the ends of the belt (1) are pushed together at velocity vj and pressed against each other with force Fj. At this stage, chemical reactions and physical interactions between the polymer macromolecules begin, resulting in the formation of a permanent connection,
- Cooling the weld (Figure 1e), during which the stiffness and strength of the weld are increased.
- Contact conduction of heat Qp3-1 from the hot plate (3) to the belt (1),
- Conduction of heat Qp1 inside the material volume, occurring mainly along the belt axis (1),
- Convective exchange of heat Qc1 between the belt (1) and the environment at temperature T0, occurring on the surface of the belt at a distance of h from the surface of the hot plate,
- Radiative exchange of heat Qr1, between the belt and the environment at temperature T0, occurring on the surface of the belt at a distance of h from the surface of the hot plate.
1.3. Aspects of Welding Process Research
- Specific heat capacity Cp,
- Thermal diffusion coefficient a,
- Melting temperature Tp,
- Dynamic viscosity η,
- Density ρ.
- Type A samples taken from the belt of circular cross-section and diameter d = 18 mm,
- Type B samples taken from the flat belt of the rectangular cross-section, width b = 140 mm and thickness g = 4 mm.
2. Materials and Methods
- Machining—concurrent milling on the EMCO Concept Mill 240D numeric machine tool (EMCO GmbH, Salzburger, Austria), using cutters adapted to machining plastics,
- Plastic treatment—knife cutting using a single-shot punch.
- Range of heating temperature: from +30 to +950 °C, recorded in continuous mode,
- Two types of gaseous atmosphere in which the samples were placed during the test: atmospheric air or protective gas—chemically pure nitrogen,
- The flow rate of the gas surrounding the samples was 20 cm3/min,
- Samples weighing 5 ± 0.2 mg,
- Heating of samples in crucibles made of aluminum trioxide.
- Type A samples, taken from the belt of the circular cross-section and diameter d = 18 mm, machined into the form of rectangular beams of the following dimensions: 53.50 ± 0.31 × 10.21 ± 0.20 × 3.74 ± 0.33 mm,
- Type B samples, taken from the flat belt, guillotined into the form of rectangular beams of the following dimensions: 49.67 ± 0.13 × 9.84 ± 0.15 × 3.93 ± 0.08 mm.
- Test temperature of approximately 22.5 °C,
- Oscillation amplitude A = 0.02%,
- Oscillation frequency f = 1 Hz.
- Temperature range from −100 to +180 °C recorded in continuous mode,
- Rate of temperature change = +5 °C/min during heating and = −5 °C/min during cooling,
- Oscillation amplitude A = 0.02%,
- Oscillation frequency f = 1 Hz.
- Intersections of tangent relations of the shear storage modulus G′ and temperature,
- The maximum value of the shear loss modulus G″,
- The maximum value of the loss coefficient tan δ.
- Temperature range from −80 to +300 °C recorded in continuous mode,
- Application of an inert protective atmosphere in the form of a flow of chemically pure nitrogen at a rate of 20 cm3/min,
- Two heating cycles at the rate of temperature change = +20 °C/min and one cooling cycle at the rate of temperature change = −10 °C/min,
- Use of samples weighing 6 ± 0.2 mg.
- Temperature range from 0 to 150 °C, with a narrower test temperature range compared to the basic DSC analysis, due to the need of ensuring the absence of phase transitions of the material that would impair the correct determination of the specific heat Cp, which is also due to apparatus requirements,
- Application of a protective inert atmosphere in the form of chemically pure nitrogen with a flow rate of 20 cm3/min,
- One heat cycle at the rate of temperature change = +20 °C/min,
- Use of the reference material in the form of synthetic sapphire (α-A2O3) with the mass similar to that of the analyzed samples.
- Isotropic nature of heat flow inside the sample,
- Heating the sample in a low-pressure atmosphere to reduce the effect of convection on sample heating,
- Thermoelectric cells were introduced to half the depth of the sample,
- Maximum heater temperature Tg = 100 °C,
- Contact surfaces between the heater and the sample, as well as thermoelectric cells, and the sample connected by a thermal conductive paste with the heat conductivity coefficient λ = 0.88 W/m∙K,
- Maximum heating time tg = 300 s,
- The distance between the thermoelectric cells b = 5 ± 0.1 mm and was measured for each sample tested.
- The density of the material according to the picnometric method, in a normalized manner [62]. The material was shredded into sections of the following size: 10 mm for sample A and 5 × 30 mm for sample B. A 25 cm3 glass picnometer was used for determination. The environment temperature at the time of determination was T0 = 22.5 °C,
- Standard Shore hardness test, using the Bareiss hardness meter (HP, Bareiss Prüfgerätebau GmbH, Oberdischingen, Germany), with a maximum value indicator [63].
3. Results
- Glass transition temperature of soft polyurethane segments TgA1SS = −38.1 °C,
- Glass transition temperature of polyurethane hard segments TgA1HS = 63.2 °C,
- Additional endothermic effect TmpA1 = 211.5 °C.
- Glass transition temperature of soft polyurethane segments TgA2SS = −30.2 °C,
- Glass transition temperature of polyurethane hard segments TgA2HS = 112.2 °C,
- No additional endothermic effect at a higher temperature.
- Glass transition temperature of soft polyurethane segments TgB1SS = −37.4 °C,
- Glass transition temperature of polyurethane hard segments TgB1HS = 72.1 °C,
- Additional endothermic effect TmpB1 = 208.3 °C.
- Glass transition temperature of soft polyurethane segments TgB2SS = −33.9 °C,
- Glass transition temperature of polyurethane hard segments TgB2HS = 108.1 °C,
- No additional endothermic effect at a higher temperature.
- The specific heat capacity Cp in both cases increases in a linear manner as the temperature increases,
- The difference in the specific heat capacity Cp for both samples is almost constant throughout the test temperature range.
4. Discussion
- The processes of material structure relaxation that take place after the first cycle. As in the case of tests at the standard temperature of material usage [68], as a result of mechanical and thermal stresses cyclically applied, the sequencing of the chains and reduction of the entropy of the system occurs [52,55,71,73].
5. Conclusions
- At the maximum temperature Tw, which reaches 310 °C, during the hot plate welding carried out in the atmospheric air, the structural changes in both belts materials, from the thermal decomposition point of view, are negligible. Therefore, the thermal decomposition phenomenon can be omitted during the analysis of the welding process, because the temperature values in which changes are noticeable are not reached,
- Both of the belts have the identical structure and chemical composition,
- Considering cyclic loads for both types of the belt, the shear modulus G and the dynamic viscosity η at room temperature change their values, as a result of stress relaxation after the first applied load, and they remain constant during subsequent cycles of loading. Adding the temperature variation causes these parameters, for both types of the belt, to become uniformed, as a result of stress relaxation and migration of the plasticizing additives. Therefore, as regards the hot plate welding process, which involves the compression of the belt under elevated temperature conditions, the difference between a circular (A) and a flat belt is negligible (B),
- As a result of cyclical mechanical and thermal loads, the basic chemical structure of the material of both belts does not change,
- Once heated to the same degree, both belts harmonize their properties with respect to mechanical response for cyclical loads and the energy demand of the heating process. These factors cause the properties of the belt during the welding process becomes more predictable,
- Both: circular (A) and flat (B) belts do not show a clear melting limit,
- Both samples differ in the specific heat capacity Cp; however, this difference is constant, and thanks to that, it can be taken into account when modeling the welding process in an easy way,
- Both the circular (A) and flat (B) cross-section belts have approximately equal density and hardness.
- Welding temperature Tw higher than 220 °C and lower than 310 °C,
- Welding without the use of inert protective atmospheres,
- The application of the correction factor ∆Cp, for specific heat capacity Cp, to model the heat flow of the process.
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Conflicts of Interest
References
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Atmosphere | Sample | Temperature at 1% Mass Loss Tmr1% [°C] | Temperature at Maximum Mass Change Rate Tvmr [°C] | Time at Maximum Mass Change Rate tvmr [min] | ||||
---|---|---|---|---|---|---|---|---|
1. Stage | 2. Stage | 3. Stage | 1. Stage | 2. Stage | 3. Stage | |||
Atmospheric air | A | 270.1 | 349.2 | 409.5 | 549.8 | 17.63 | 20.58 | 27.58 |
B | 275.1 | 350.1 | 410.7 | 563.5 | 17.76 | 20.67 | 28.26 | |
Nitrogen (N2) | A | 215.6 | 371.2 | – | – | 18.70 | – | – |
B | 270.2 | 346.6 | 395.8 | – | 17.59 | 20.02 | – |
Sample | Cycle | Temp T [°C] | G′ [MPa] | G″ [MPa] | η [MPa⸳s] | tan δ [–] |
---|---|---|---|---|---|---|
A | 1 | 22.47 ± 0.02 | 29.40 ± 1.55 | 2.03 ± 0.23 | 4.69 ± 0.25 | 0.0669 ± 0.0041 |
2 | 22.43 ± 0.02 | 24.87 ± 3.75 | 1.90 ± 0.31 | 3.97 ± 0.60 | 0.0763 ± 0.0009 | |
3 | 22.43 ± 0.02 | 26.00 ± 3.59 | 2.02 ± 0.31 | 4.15 ± 0.58 | 0.0776 ± 0.0011 | |
B | 1 | 22.47 ± 0.02 | 18.90 ± 0.62 | 1.58 ± 0.056 | 3.02 ± 0.10 | 0.0840 ± 0.0004 |
2 | 22.43 ± 0.02 | 13.60 ± 0.89 | 1.17 ± 0.093 | 2.17 ± 0.14 | 0.0862 ± 0.0014 | |
3 | 22.47 ± 0.02 | 13.90 ± 0.95 | 1.22 ± 0.095 | 2.22 ± 0.15 | 0.0874 ± 0.0016 |
Sample Type | Cycle | TgSS [°C] by G′ | Module G′ [MPa] at TgSS | TgSS [°C] by G″ | Max G″ [MPa] | TgSS [°C] by tan δ | Max tan δ [–] |
---|---|---|---|---|---|---|---|
A | 1 | −48.10 ± 4.31 | 848.80 ± 115.68 | −40.70 ± 2.77 | 108.33 ± 1.53 | −31.93 ± 2.30 | 0.2963 ± 0.0057 |
2 | −47.24 ± 0.56 | 1233.28 ± 114.83 | −36.97 ± 0.25 | 130.33 ± 10.41 | −27.23 ± 0.12 | 0.3783 ± 0.0090 | |
3 | −47.23 ± 0.56 | 1248.15 ± 110.62 | −36.93 ± 0.21 | 131.33 ± 10.21 | −27.23 ± 0.12 | 0.3740 ± 0.0079 | |
B | 1 | −51.84 ± 3.84 | 861.81 ± 146.01 | −39.90 ± 2.77 | 103.87 ± 12.71 | −27.83 ± 1.10 | 0.3273 ± 0.0051 |
2 | −47.28 ± 0.20 | 1369.58 ± 29.11 | −36.73 ± 0.13 | 148.67 ± 3.51 | −24.87 ± 0.06 | 0.4987 ± 0.0064 | |
3 | −46.40 ± 0.04 | 1374.80 ± 33.89 | −36.77 ± 0.06 | 149.00 ± 3.00 | −24.80 ± 0.01 | 0.4943 ± 0.0067 |
Sample | Cycle | TgHS °C by tan δ | Min tan δ |
---|---|---|---|
A | 1 | 65.37 ± 5.84 | 0.0425 ± 0.0013 |
2 | 74.67 ± 3.55 | 0.0476 ± 0.0004 | |
3 | 74.70 ± 2.69 | 0.0487 ± 0.0003 | |
B | 1 | 57.76 ± 0.06 | 0.0452 ± 0.0012 |
2 | 73.03 ± 3.61 | 0.0555 ± 0.0004 | |
3 | 70.03 ± 1.27 | 0.0571 ± 0.0004 |
Cycle | Sample | TgSS [°C] | TgHS [°C] | Tmp [°C] |
---|---|---|---|---|
1st heat | A | −38.1 | 63.2 | 211.5 |
2nd heat | A | −30.2 | 112.2 | - |
1st heat | B | −37.4 | 65.8 | 208.3 |
2nd heat | B | −33.9 | 108.1 | - |
Sample | Specific Heat Cp [J/g⸳K] | |||||||
---|---|---|---|---|---|---|---|---|
Tg [°C] | 20 °C | 40 °C | 60 °C | 80 °C | 100 °C | 120 °C | 140 °C | |
A | 1.843 | 1.728 | 1.812 | 1.874 | 1.951 | 2.022 | 2.100 | 2.170 |
B | 1.470 | 1.292 | 1.414 | 1.470 | 1.527 | 1.583 | 1.640 | 1.694 |
Difference | – | 0.436 | 0.398 | 0.404 | 0.424 | 0.439 | 0.460 | 0.476 |
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Wałęsa, K.; Wrzesińska, A.; Dobrosielska, M.; Talaśka, K.; Wilczyński, D. Comparative Analysis of Polyurethane Drive Belts with Different Cross-Section Using Thermomechanical Tests for Modeling the Hot Plate Welding Process. Materials 2021, 14, 3826. https://doi.org/10.3390/ma14143826
Wałęsa K, Wrzesińska A, Dobrosielska M, Talaśka K, Wilczyński D. Comparative Analysis of Polyurethane Drive Belts with Different Cross-Section Using Thermomechanical Tests for Modeling the Hot Plate Welding Process. Materials. 2021; 14(14):3826. https://doi.org/10.3390/ma14143826
Chicago/Turabian StyleWałęsa, Krzysztof, Anna Wrzesińska, Marta Dobrosielska, Krzysztof Talaśka, and Dominik Wilczyński. 2021. "Comparative Analysis of Polyurethane Drive Belts with Different Cross-Section Using Thermomechanical Tests for Modeling the Hot Plate Welding Process" Materials 14, no. 14: 3826. https://doi.org/10.3390/ma14143826
APA StyleWałęsa, K., Wrzesińska, A., Dobrosielska, M., Talaśka, K., & Wilczyński, D. (2021). Comparative Analysis of Polyurethane Drive Belts with Different Cross-Section Using Thermomechanical Tests for Modeling the Hot Plate Welding Process. Materials, 14(14), 3826. https://doi.org/10.3390/ma14143826