Design and Optimization of a Radial Turbine to Be Used in a Rankine Cycle Operating with an OTEC System

Abstract

Design and optimization of a radial turbine for a Rankine cycle were accomplished ensuring higher thermal efficiency of the system despite the low turbine inlet temperature. A turbine design code (TDC) based on the meanline design methodology was developed to construct the base design of the turbine rotor. Best design practices for the base design were discussed and adopted to initiate a robust optimization procedure. The baseline design was optimized using the response surface methodology and by coupling it with the genetic algorithm. The design variables considered for the study are rotational speed, total to static speed ratio, hub radius ratio, shroud radius ration, and number of blades. Various designs of the turbine were constructed based on the Central Composite Design (CCD) while performance variables were computed using the in-house turbine design code (TDC) in the MATLAB environment. The TDC can access the properties of the working fluid through a subroutine that links NIST’s REFPROP to the design code through a subroutine. The finalization of the geometry was made through an iterative process between 3D-Reynolds-Averaged Navier-Stokes (RANS) simulations and the one-dimensional optimization procedure. 3D RANS simulations were also conducted to analyze the optimized geometry of the turbine rotor for off-design conditions. For computational fluid dynamics (CFD) simulation, a commercial code ANSYS-CFX was employed. 3D geometry was constructed using ASYS Bladegen while structured mesh was generated using ANSYS Turbogrid. Fluid properties were supplied to the CFD solver through a real gas property (RGP) file that was constructed in MATLAB by linking it to REFPROP. Computed results show that an initial good design can reduce the time and computational efforts necessary to reach an optimal design successfully. Furthermore, it can be inferred from the CFD calculation that Response Surface Methodology (RSM) employing CFD as a model evaluation tool can be highly effective for the design and optimization of turbomachinery.

Ocean Thermal Energy Conversion: Technological Readiness and Indonesia Progress

“…In addition to the number of blades, the shroud radius ratio and the hub radius ratio of the turbine stator also affect the turbine power output in the OTEC cycle. The shroud radius ratio has more influence on the turbine power output than the hub radius ratio (Alawadhi et al, 2020). As shown in Figure 2.15, for higher shroud radius ratio, the turbine power output increases with increasing hub radius ratio, while for lower shroud radius ratio, the turbine power output decreases with increasing hub radius ratio.…”

Parameter Optimization and Performance Research: Radial Inflow Turbine in Ocean Thermal Energy Conversion

“…The three-dimensional modeling of the volute and stator was completed using SolidWorks. The rotor modeling was completed with reference to Ansys-Bladegen [29]. The three-dimensional model of the initial scheme is shown in Figure 3.…”

Experimental Study and 3D Optimization of Small-Scale Solar-Powered Radial Turbine Using 3D Printing Technology

“…Similar research efforts have been carried out [14][15][16][17]. Both mechanical and thermal loads, with their impact on the aerodynamic and deformation performance of the impeller for a micro gas radial turbine, have been analysed [14].…”