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Modeling The Hyperloop With COMSOL® · Hyperloop Pod competition in 2018. During the development...

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The EPFLoop student team from Ecole Polytechnique Fédérale de Lausanne developed a capsule thanks to which it won third place at the SpaceX Hyperloop Pod competition in 2018. During the development of the EPFLoop pod, COMSOL Multiphysics® was used to study the design of composite pressurised subsystems. The pressure vessels (PVs) are used to store electrical components in a pressurized environment (1 atm). The aim is to avoid a direct exposure of the components to the vacuum, which would be destructive for the electronics inside. The composite structure of the PVs should safely resist to the conditions in vacuum during the run while being light. In order to find such an arrangement, a structural analysis was done. To ensure the safe functioning of the electronics inside the PVs (Fig. 1 and 2), the temperature must not exceed 50 C. A thermal analysis has been done to ensure that the PV will not overheat due to power losses at full power. The structural analyses have resulted in a safe design of the PVs, which has been confirmed by the thermal analysis. The PVs have been successfully tested at nominal pressure (1 atm). This work pointed out how interdisciplinary and polyhedral skills can lead to new solutions in engineering. EPFLoop, thanks to COMSOL and others partners, will participate at the 2019 SpaceX Competition. REFERENCES: 1. Gay D. (2015). Composite Materials Design and Applications, Boca Raton, FL, CRC Press 2. SpaceX 2018 Competition Safety document Modeling The Hyperloop With COMSOL® : On the Design Of The EPFLoop Pressurized Systems Z. Sajó 1 , L. Benedetti 2 , N. Riva 3 We thank EPFL, EE, COMSOL and our advisors for their support. Figure 1. Main pressure vessel (MPV). Figure 2. Lateral pressure vessel (LPV) Figure 5. MPV inner and outer ply (L to R) Tsai-Wu safety factor at MAWP. To evaluate the BURST and MAWP pressures, a of pressure sweep from 1 bar to 10 bars inside the PVs has been carried out (Fig. 7). Additional loads were the weight of the components during acceleration and deceleration. Figure 7. Minimum Tsai-Wu safety factor vs inner pressure. Figure 8. Leak test (LPV). Introduction Conclusion Figure 6. MPV inner shell principal stresses 1, 2, 3 (L to R) at BURST. The plies were arranged in order to ensure a safety factor of 2 with a pressure of 1.2 bar (MAWP). After several iterations, the safety factor is of 2 everywhere on the PVs. The performance of the composite pressure vessels is determined using the Tsai-Wu model (Fig. 5) . The analysis of the distribution of principal stresses (Fig. 6) made it possible to localize the direction of stress and the areas where the structure needed to be reinforced. To validate the FEA, the pressure vessels have been tested: compressed air was injected up to 1.5 bar, to check the presence of leaks at MAWP (Fig. 8). Remarkably low leakages were observed (<20 mbar/h for all the PVs). Structural Stationary Analysis The PV’s failure under load was studied using a stationary simulation with the Shells module, where shells represent the plies of the carbon fiber-epoxy and foam sandwich structure. During the design, the assessment of the MAWP (Maximum Allowable Working Pressure, where the safety factor is >2 everywhere) and the BURST pressure (safety factor <1 in some areas) was required [REF SpaceX] In order to assess these values, a parametric sweep varying the inside pressure has been performed, during which the changing of the Tsai-Wu safety factor and the principal stresses were studied. Figure 4. LPV quad mesh. The applied loads are given by the deceleration, the weight of the components inside the PV and a constant and uniform pressure of 1 atm applied on the inner surfaces. A free triangular mesh was applied on the PVs. Its quality was measured by skewness (Fig. 4). A curvilinear coordinate interface on each layer has been used to simulate the anisotropic properties and the irregular geometry. Thermal Analysis The functioning of the electronic components in the MPV is guaranteed as long as the temperature inside of the MPV does not exceed 50 °C. Heat transfer in solid coupled with laminar flow, during idle mode and full power functioning has been done in order to ensure that the dissipated power will not heat the MPV, which would lead to possible malfunctioning of the electronics (Fig. 3). Figure 3. Temperature and free buoyancy during 1 hour. 1. EPFL and EPFLoop M.Sc. Student in Materials science and engineering, STI, Lausanne, Switzerland 2. EPFL and EPFLoop PostDoc, GEL - GeoEnergy Laboratory, ENAC, Lausanne, Switzerland 3. EPFL and EPFLoop PhD candidate, SCI IC BD Applied Superconductivity, STI, Lausanne, Switzerland The heat load is the heat dissipated via Joule effect, emitted by surfaces. The simulations, showing an upper temperature of 47 °C, have been validated through measurements. Excerpt from the Proceedings of the 2018 COMSOL Conference in Lausanne
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Page 1: Modeling The Hyperloop With COMSOL® · Hyperloop Pod competition in 2018. During the development of the EPFLoop pod, COMSOL Multiphysics® was used to study the design of composite

The EPFLoop student team from Ecole Polytechnique Fédérale de Lausannedeveloped a capsule thanks to which it won third place at the SpaceXHyperloop Pod competition in 2018. During the development of the EPFLooppod, COMSOL Multiphysics® was used to study the design of compositepressurised subsystems. The pressure vessels (PVs) are used to storeelectrical components in a pressurized environment (1 atm). The aim is toavoid a direct exposure of the components to the vacuum, which would bedestructive for the electronics inside. The composite structure of the PVsshould safely resist to the conditions in vacuum during the run while beinglight. In order to find such an arrangement, a structural analysis was done.To ensure the safe functioning of the electronics inside the PVs (Fig. 1 and 2),the temperature must not exceed 50

∘C. A thermal analysis has been done to

ensure that the PV will not overheat due to power losses at full power.

The structural analyses have resulted in a safe design of the PVs, which has beenconfirmed by the thermal analysis. The PVs have been successfully tested atnominal pressure (1 atm). This work pointed out how interdisciplinary andpolyhedral skills can lead to new solutions in engineering. EPFLoop, thanks toCOMSOL and others partners, will participate at the 2019 SpaceX Competition.

REFERENCES:1. Gay D. (2015). Composite Materials Design and Applications, Boca Raton, FL, CRC Press2. SpaceX 2018 Competition Safety document

Modeling The Hyperloop With COMSOL® :On the Design Of The EPFLoop Pressurized Systems

Z. Sajó1, L. Benedetti2, N. Riva3

We thank EPFL, EE, COMSOL and our advisors for their support.

Figure 1. Main pressure vessel (MPV). Figure 2. Lateral pressure vessel (LPV)

Figure 5. MPV inner and outer ply (L to R) Tsai-Wu safety factor at MAWP.

To evaluate theBURST and MAWPpressures, a ofpressure sweepfrom 1 bar to 10bars inside the PVshas been carriedout (Fig. 7).Additional loadswere the weight ofthe componentsduring accelerationand deceleration.

Figure 7. Minimum Tsai-Wu safety factor vs inner pressure.

Figure 8. Leak test (LPV).

Introduction

Conclusion

Figure 6. MPV inner shell principal stresses 1, 2, 3 (L to R) at BURST.

The plies were arranged inorder to ensure a safety factorof 2 with a pressure of 1.2 bar(MAWP). After severaliterations, the safety factor isof 2 everywhere on the PVs.The performance of thecomposite pressure vessels isdetermined using the Tsai-Wumodel (Fig. 5) .

The analysis of thedistribution of principalstresses (Fig. 6) made itpossible to localize thedirection of stress and theareas where the structureneeded to be reinforced.

To validate the FEA, the pressure vessels have been tested:compressed air was injected up to 1.5 bar, to check the presence ofleaks at MAWP (Fig. 8). Remarkably low leakages were observed (<20mbar/h for all the PVs).

Structural Stationary Analysis

The PV’s failure under load was studied using a stationary simulation with theShells module, where shells represent the plies of the carbon fiber-epoxy andfoam sandwich structure.

During the design, the assessment of the MAWP (Maximum Allowable WorkingPressure, where the safety factor is >2 everywhere) and the BURST pressure(safety factor <1 in some areas) was required [REF SpaceX]In order to assess these values, a parametric sweep varying the inside pressure hasbeen performed, during which the changing of the Tsai-Wu safety factor and theprincipal stresses were studied.

Figure 4. LPV quad mesh.

The applied loads are given by thedeceleration, the weight of thecomponents inside the PV and aconstant and uniform pressure of 1atm applied on the inner surfaces.A free triangular mesh was applied onthe PVs. Its quality was measured byskewness (Fig. 4).A curvilinear coordinate interface oneach layer has been used to simulatethe anisotropic properties and theirregular geometry.

Thermal Analysis

The functioning of the electronic components in the MPV is guaranteed aslong as the temperature inside of the MPV does not exceed 50 °C.

Heat transfer in solid coupled withlaminar flow, during idle mode andfull power functioning has beendone in order to ensure that thedissipated power will not heat theMPV, which would lead to possiblemalfunctioning of the electronics(Fig. 3). Figure 3. Temperature and free buoyancy

during 1 hour.

1. EPFL and EPFLoop M.Sc. Student in Materials science and engineering, STI, Lausanne, Switzerland2. EPFL and EPFLoop PostDoc, GEL - GeoEnergy Laboratory, ENAC, Lausanne, Switzerland3. EPFL and EPFLoop PhD candidate, SCI IC BD Applied Superconductivity, STI, Lausanne, Switzerland

The heat load is the heat dissipated via Joule effect, emitted by surfaces.The simulations, showing an upper temperature of 47 °C, have beenvalidated through measurements.

Excerpt from the Proceedings of the 2018 COMSOL Conference in Lausanne

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