Abstract

The efficiency of expanders is of prime importance in determining the overall performance of a variety of thermodynamic power systems, with reciprocating-piston expanders favoured at intermediate-scales of application (typically 10–100 kW). Once the mechanical losses in reciprocating machines are minimized (e.g. through careful valve design and operation), losses due to the unsteady thermal-energy exchange between the working fluid and the solid walls of the containing device can become the dominant loss mechanism. In this work, gas-spring devices are investigated numerically in order to focus explicitly on the thermodynamic losses that arise due to this unsteady heat transfer. The specific aim of the study is to investigate the behaviour of real gases in gas springs and to compare this to that of ideal gases in order to attain a better understanding of the impact of real-gas effects on the thermally induced losses in reciprocating expanders and compressors. A CFD-model of a gas spring is developed in OpenFOAM. Three different fluid models are compared: (1) an ideal-gas model with constant thermodynamic and transport properties; (2) an ideal-gas model with temperature-dependent properties; and (3) a real-gas model using the Peng-Robinson equation-of-state with temperature and pressure-dependent properties. Results indicate that, for simple, mono- and diatomic gases, like helium or nitrogen, there is a negligible difference in the pressure and temperature oscillations over a cycle between the ideal and real-gas models. However, when considering heavier (organic) molecules, such as propane, the ideal-gas model tends to overestimate the pressure compared to the real-gas model, especially if the temperature and pressure dependency of the thermodynamic properties is not taken into account. In fact, the ideal-gas model predicts higher pressures by as much as 25% (compared to the real-gas model). Additionally, both ideal-gas models underestimate the thermally induced loss compared to the real-gas model for heavier gases. This discrepancy is most pronounced at rotational speeds where the losses are highest. The real-gas model predicts a peak loss of 8.9% of the compression work, while the ideal-gas model predicts a peak loss of 5.7%. These differences in the work loss are due to the fact that the gas behaves less ideally during expansion than during compression, with the compressibility factor being lower during compression. This behaviour cannot be captured with the ideal-gas law. It is concluded that real-gas effects must be taken into account in order to predict accurately the thermally induced loss mechanism when using heavy fluid molecules in such devices.

Highlights

  • Reciprocating machines have potential applications in the efficient conversion of external low and medium-grade heat to useful work

  • Reciprocating piston expanders in organic Rankine cycles (ORCs) have speeds ranging from 50 to 4000 RPM [9,10,11] which translates into a Peclet number from somewhere around 500 to 50000

  • The oscillatory Peclet number, P e, is used as a dimensionless measure for the rotational speed of the gas spring: Pe where ω is the angular frequency, α0 = k/ρcp is the time and spatially-averaged thermal diffusivity and Dh = 4Vmd/Amd is the hydraulic diameter at mid-stroke (Vmd and Amd are the cylinder volume and surface area at mid-stroke)

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Summary

Introduction

Reciprocating machines have potential applications in the efficient conversion of external low and medium-grade heat (e.g. solar, geothermal, waste) to useful work. For instance, are a viable alternative to turbomachines and other positive displacement (volumetric) expanders in organic Rankine cycles (ORCs) at intermediate-scales of application (typically 10–100 kW). They provide higher efficiencies at these lower power outputs and at off-design operating speeds which may occur due to the intermittent nature of the aforementioned heat sources. Thermodynamic losses occur due to mechanical friction between moving parts, flow losses through valves and due to leakage, and irreversibilities due to heat transfer across finite temperature differences. Induced losses tend to peak around intermediate rotational speeds with Peclet numbers (defined in Sec. 2.1) on the order of 10. Thermofluidic oscillators have frequencies on the order of 0.01 to 1 Hz [1,2,3] which is equivalent to Peclet numbers from 0.1 to 100 (assuming a cylinder diameter of 2 cm)

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