Applications
Design of High Performance Pump Stage
Design Optimisation of a Strongly Interacting Diffuser Pump Stage
Design of a Double-Suction Volute Pump
Multi-Objective Optimisation of a Centrifugal Pump Stage by Means of Design of Experiment Coupled with Inverse Design Method
Design of an Inducer Pump with High Suction Performance and Backflow Control
Design High Efficiency Impellers with Splitter Blades
Design of an Automobile Torque Converter
Design of a Cooling Fan
Design of a Double-Suction Fan Stage
Redesign of an Industrial Compressor Stage
Design of Refrigeration Compressor Stage in R134a
Hydraulic Design Optimisation of a Torque Converter
Design of a 3 Stage Axial LP Turbine for Aeroengine Applications
Design High Performance Centrifugal Compressor Impellers
Design High Performance Centrifugal Compressor Vaned Diffusers
Design High Performance Axial Turbine Stages with More Uniform Exit Flow
Publications
- Choice of Optimum Blade Loading in Application of 3D Inverse Design to Design of Pumps and Fans.
- A Fast 3D Inverse Design Based Multi-Objective Optimization Strategy for Design of Pumps
- Turbomachinery Blade Design Using 3-D Inverse Design Method, CFD and Optimization Algorithm
- A Multi-Objective Automatic Optimization Strategy for Design of Waterjet Pumps
- Development of Cryogenic Pump Hydrodynamics Using Inverse Design Method and CFD
Case Studies
- Design of Mixed Flow Pump Stage Using TURBOdesign1 and CFD Code, Hyosung-Ebara
- CDI Marine Applies TURBOdesign1 & CFD to Design a Marine Waterjet
- Design of a Compact Reactor Coolant Pump with Higher Efficiency and Cavitation Performance by using TURBOdesign1
- Design of a Second Stage Hydrogen Rocket Turbopump by TURBOdesign1
- TURBOdesign1 is Extensively Used at Voith Turbo for the Design of Hydrodynamic Torque Converters
Study on Pump Impeller With Splitter Blades Designed by 3-D Inverse Design Method
The performance of pump impellers with splitter blades, designed using a three-dimensional inverse design method, is examined. The designs were chosen for a specific speed of 400 (m3/min, m, min-1) or 0.155 (non-dimensional), and analyzed numerically with CFD and experimentally with model tests. Experimental validation showed that the peak efficiency of the impeller with conventional splitter blades, having the same shape as full blades and located mid-pitch between full blades, was remarkably lower than that of the corresponding impeller without splitter blades. However, the peak efficiency of impeller with splitter blades designed using the 3-D inverse design method, having different shape from full blades, was almost the same as the corresponding impeller without splitter blades. It was also found that the suction performance of the impellers with splitter blades was improved from that of the corresponding impeller without splitter
blades. The suction performance was improved mainly at partial flow rates if the leading edges of splitter blades were located at 20% of the meridional chord length and improved mainly at larger flow rates if the leading edges of splitter blades were located at 40% of the meridional chord length. Unstable phenomena occurring at partial flow rates under low suction pressure were also investigated.

