Abstract

Organic Rankine cycle (ORC) systems are a readily available technology to convert thermal energy from renewable- and waste heat sources into electricity. However, their thermal performance is relatively low due to the low temperature of the available heat sources, but more importantly, due to the low efficiency of the employed expander. Designing the turboexpander is exceptionally challenging, because the flow field is highly supersonic and unsteady, and since the expansion takes place in the highly non-ideal dense-vapor region. In this work, we perform unprecedented three-dimensional unsteady simulations of several high-expansion cantilever ORC turbines to highlight distinctive loss mechanisms. The simulations indicate strong unsteady effects in the rotor blade passage, as a result of unsteady propagating shock waves interacting with viscous wakes and boundary layers. Moreover, the flow field in the rotor blade passage is strongly affected by three-dimensional secondary flow features and a sharp expansion in the shroud region at the inlet of the rotor blade. These span-wise mechanisms and unsteady flow interactions introduce irreversible losses which must be taken into account for designing highly efficient ORC expanders.

Highlights

  • Organic Rankine cycle (ORC) power systems are a viable alternative to convert low-tomedium grade heat sources at temperatures between 120 and 500 + C[1] to electrical power

  • Three shock waves are depicted in the rotor blade passage named in Fig. 4(d): (1) a bow shock (BS) produced at the rotor leading edge (RLE) because the flow is supersonic in the relative frame of reference (Marelz1:3), (2) a separation shock wave (SW) generated by the flow detachment at the suction side of the blade, and (3) the reflected shock (R) from the tail of SW impinging at the PS of the rotor blade

  • This article presents detailed unsteady numerical simulations via three-dimensional calculations of high-expansion radial inflow ORC turbines, which operates in the dense-vapor region

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Summary

Introduction

ORC power systems are a viable alternative to convert low-tomedium grade heat sources at temperatures between 120 and 500 + C[1] to electrical power. To evaluate large expansion ratio ORC turbines (PR > 10) operating with an organic compound with a relatively low speed of sound, it is of paramount importance to consider time-resolved unsteady simulations. Such machines have a transonic/supersonic flow at the exit of the stator. To the authors’ knowledge, the present study is the first CFD investigation of a ORC turbine stage with a pressure ratio larger than 100 which accounts for the combination of real gas effects, unsteady stator/rotor interaction, and three-dimensional effects. The final section of this article presents conclusions and future works

System
Turbine stage geometry
Numerical domain
Solver and models
Boundary conditions
Flow field analysis of the CFD simulations
Unsteady flow interaction
Three-dimensional flow analysis
Quantitative analysis of the turbine stages
Accumulative rate of entropy generation
Q3D simulations By examining the accumulative entropy generation for the two
Turbine performance
Findings
Conclusion and future works
Full Text
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