Applications
Design High Efficiency Impellers with Splitter Blades
Design of an Automobile Torque Converter
Redesign of an Industrial Compressor 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
Design of High Performance Pump Stage
Design Optimisation of a Strongly Interacting Diffuser Pump Stage
Design of a Cooling Fan
Design of a Double-Suction Fan Stage
Design of a Double-Suction Volute Pump
Design of Refrigeration Compressor Stage in R134a
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 Performance Centrifugal Compressor Vaned Diffusers
Publications
- Parametric Design of a Waterjet Pump by Means of Inverse Design, CFD Calculations and Experimental Analyses
- Improvements of Pump Suction Performance Using 3D Inverse Design Method
- A Compressible Three-Dimensional Design Method for Radial and Mixed Flow Turbomachinery Blades
- Choice of Optimum Blade Loading in Application of 3D Inverse Design to Design of Pumps and Fans.
- Propulsor Design Using Clebsch Formulation
Case Studies
- TURBOdesign1 is Extensively Used at Voith Turbo for the Design of Hydrodynamic Torque Converters
- CDI Marine Applies TURBOdesign1 & CFD to Design a Marine Waterjet
- Design of Mixed Flow Pump Stage Using TURBOdesign1 and CFD Code, Hyosung-Ebara
- TURBOdesign1 an efficient design tool for the development of compact fan guide vanes at ebm-papst
- Design of a Compact Reactor Coolant Pump with Higher Efficiency and Cavitation Performance by using TURBOdesign1
Development of A 3D Inverse Design Code for Application to Different Turbo and Hydraulic Machinery Components
This paper describes the current stage of development of a code for 3D inverse design of the blade and meridional geometry of different turbo and hydraulic machinery components. The paper starts by describing the basic features of the method, in which the blades are represented by sheets of vorticity whose strength is related to a specified circulation distribution or rVθ. The extension of the method to design of blades with splitters and the design of meridional geometry of turbomachines is then briefly described. The application of the method to design of blade geometry of the impeller of a radial-inflow turbine, a centrifugal compressor and a mixed flow pump, indicate the considerable potential of the method in designing blades with superior performance as compared with the corresponding state-of-the-art conventional impellers. Applications of the method to other turbomachinery components such as vaned diffusers and the design of the meridional geometry show the robustness and the generality of this code.

