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 High Performance Centrifugal Compressor Vaned Diffusers
Redesign of an Industrial Compressor Stage
Design of Refrigeration Compressor Stage in R134a
Design of an Automobile Torque Converter
Design of a Cooling Fan
Design of a Double-Suction Fan Stage
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 Axial Turbine Stages with More Uniform Exit Flow
Publications
- Optimization of Pump Blades Using Three Dimensional Inverse Design Method
- Hydrodynamic Design System for Pumps Based on 3-D CAD, CFD and Inverse Design Method
- Compact Design of Diffuser Pumps Using Three-Dimensional Inverse Design Method
- 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
Case Studies
- Design of Mixed Flow Pump Stage Using TURBOdesign1 and CFD Code, Hyosung-Ebara
- Design of a Compact Reactor Coolant Pump with Higher Efficiency and Cavitation Performance by using TURBOdesign1
- Application of TURBOdesign1 for the Compact Design of Rocket Engine Turbopump - JAXA
- CDI Marine Applies TURBOdesign1 & CFD to Design a Marine Waterjet
- Design of a Second Stage Hydrogen Rocket Turbopump by TURBOdesign1
Hydrodynamic Design of Pump Diffuser Using Inverse Design Method and CFD
A new approach to optimizing a pump diffuser was presented, based on a three-dimensional inverse design method and a Computational Fluid Dynamics (CFD) technique. The blade shape of the diffuser was designed for a specified distribution of circulation and a given meridional geometry at a low specific speed of 0.109 (non-dimensional) or 280 (m3/min, m, rpm). To optimize the three dimensional pressure fields and the secondary flow behavior inside the flow passage, the diffuser blade was more fore-loaded at the hub side as compared with the casing side. Numerical calculations, using a stage version of Dawes three dimensional Navier-Stokes code, showed that such a loading distribution can suppress flow separation at the corner region between the hub and the blade suction surface, which was commonly observed with conventional designs having a compact bowl size (small outer diameter). The improvements in stage efficiency were confirmed experimentally over the corresponding conventional pump stage. The application of multi-color oil-film flow visualization confirmed that the large area of the corner separation was completely eliminated in the inverse design diffuser.

