GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

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1 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
Lorenzo Talluri1, Olivier Dumont2, Giampaolo Manfrida1, Vincent Lemort2 and Daniele Fiaschi1 1Department of Industrial Engineering (DIEF) University of Florence Florence, Italy 2Thermodynamics laboratory, Aerospace and Mechanical Engineering Department, University of Liège, Allée de la Découverte 17, Belgium

2 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
Table of contents Tesla turbine 2D model Geometry assessment Rotor channel width/inlet diameter ratio Rotor outlet/inlet diameter ratio & Throat/width ratio Fluid dynamics assessment Assessment of correct geometry Efficiency versus Power and Expansion Ratio Conclusions GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

3 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
Multiple parallel flat rigid disks The disks are arranged co-axially in order to maintain a very small gap between them. The radial-inflow admission of the working fluid is from one or more tangential nozzles, providing a strong tangential component. The working fluid moves from the inlet to the outlet radius due to the difference in pressure determined by friction and by the exchange of momentum, and exits from openings made on the disks and/or shaft at the inner radius. Plenum chamber Nozzles Rotor Fluid Trajectory inside the rotor Fluid discharged axial direction Admission to plenum chamber GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

4 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
2D model The model hypothesizes the fluid as real and compressible with steady and viscous flow. GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

5 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
Geometry Assessment GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

6 Rotor channel width/inlet diameter ratio
Total-to-total efficiency of the turbine vs. channel width, at fixed 100°C total inlet temperature and total inlet pressure corresponding to a 10 K super heating level. Loci of best efficiency, η The quadratic interpolated equation for the determination of the non-dimensional rotor channel width B, which allows achieving the highest efficiency vs. rotor outer diameter D2 B = D22 – D GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

7 Rotor outlet/inlet diameter ratio & Throat/width ratio
When the optimal non-dimensional channel width correlation is applied, the best value for practically every turbine size is always in the range 0.3 – 0.4 Total-to-total efficiency increases linearly with decreasing TWR. => low TWRs imply higher velocities at the throat, which are beneficial for rotor efficiency. The power output shows an opposite behaviour, steadily increasing with increasing TWR. TWR= TW∗ H s ∗ Z stat 2∗π∗ r 2 ∗b∗ n disk GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

8 Fluid dynamics assessment
Increasing throat Mach number allows an improvement of both efficiency and power. The tangential velocity ratio σ is one of the most important parameters for Tesla turbine optimization. The right matching of rotor inlet tangential velocity and peripheral speed is of paramount importance to achieve a high efficiency. 𝜎= 𝑣 𝑡2 𝑢 2 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

9 Assessment of correct geometry
Considering different working fluids, the obtained geometry as a function of rotor outer diameter results to be optimized within similar ranges of the main design parameters: 0.3 < R< 0.4, TW = 0.02, Ma = 1 σ = 1. Fluid Non-dimensional rotor channel width (B) R1233zd(E) R245fa R1234yf n-Hexane GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

10 Assessment of correct geometry
When constrained rotational velocity applications are considered, high expander efficiencies are directly related to a proper selection of the rotor diameter. => Expansion ratio β and efficiency η are maximised when σ approaches unity GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

11 Efficiency versus Power and Expansion Ratio
3.5 < β < 5.5 0.005 < P < 35 kW η> 60% for all fluids GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

12 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
Geometric sizing guidelines are proposed to achieve high performance of Tesla turbine working with 4 different fluids. The most critical parameters for achieving good turbine performance are found to be the rotor inlet tangential velocity ratio σ, the non-dimensional rotor channel width B and the rotor outlet/inlet diameter ratio R. Proper design expansion ratios for the Tesla turbine are determined between 3.5 and 5.5. Hydrocarbon fluids are suitable for micro power generation. Specifically, n-Hexane achieves high efficiency at low-pressure levels. Nonetheless, if a high power per unit volume is required, organic refrigerants appear to be a good choice, as the power output per channel is definitely higher when compared to hydrocarbons. GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC

13 GEOMETRY AND PERFORMANCE ASSESSMENT OF TESLA TURBINES FOR ORC
Lorenzo Talluri1, Olivier Dumont2, Giampaolo Manfrida1, Vincent Lemort2 and Daniele Fiaschi1 1Department of Industrial Engineering (DIEF) University of Florence Florence, Italy 2Thermodynamics laboratory, Aerospace and Mechanical Engineering Department, University of Liège, Allée de la Découverte 17, Belgium