Applications
Redesign of an Industrial Compressor Stage
Design of Refrigeration Compressor Stage in R134a
Hydraulic Design Optimisation of a Torque Converter
Design of High Performance Pump Stage
Design of a 3 Stage Axial LP Turbine for Aeroengine Applications
Design High Efficiency Impellers with Splitter Blades
Design High Performance Centrifugal Compressor Vaned Diffusers
Design of an Automobile Torque Converter
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
Multi-Objective Optimisation of a Centrifugal Pump Stage by Means of Design of Experiment Coupled with Inverse Design Method
Design High Performance Centrifugal Compressor Impellers
Design of an Inducer Pump with High Suction Performance and Backflow Control
Design High Performance Axial Turbine Stages with More Uniform Exit Flow
Publications
- Inviscid-Viscous Interaction Method for Three-Dimensional Inverse Design of Centrifugal Impellers
- Optimization of 6.2:1 Pressure Ratio Centrifugal Compressor Impeller by 3D Inverse Design
- On the Coupling of Inverse Design and Optimization Techniques for the Multiobjective, Multipoint Design of Turbomachinery Blades
- Inverse Design of Centrifugal Compressor Vaned Diffusers in Inlet Shear Flows
- Three-Dimensional Automatic Optimization Method for Turbomachinery Blade Design
Case Studies
- Improving Turbocharger Centrifugal Compressor Efficiency by TURBOdesign1 - Cummins Turbo
- TURBOdesign1 is Extensively Used at Voith Turbo for the Design of Hydrodynamic Torque Converters
- CDI Marine Applies TURBOdesign1 & CFD to Design a Marine Waterjet
- Inverse Design of Aeronautical Turbines in Avio S.p.A Design Process
- TURBOdesign1 an efficient design tool for the development of compact fan guide vanes at ebm-papst
Development of a High Performance Centrifugal Compressor Using a 3D Inverse Design Technique
Diesel engines developed to meet future US and European emissions regulations place an unprecedented demand on compressor performance in terms of pressure ratio and flow range capability. Additionally the direct impact compressor efficiency has on engine fuel consumption means that the new generation of centrifugal compressors designed for Turbochargers will have to meet very demanding efficiency targets. Cummins Turbo Technologies have been exploring the application of inverse design techniques for improved compressor efficiency and pressure ratio. This paper describes the application of 3D inverse design method TURBOdesign-1 to a centrifugal compressor wheel. The baseline compressor is a production impeller with straight filament blades. In this paper the main features of the inverse design method and its design parameters are described. The impeller computed by the inverse design method has 3D geometry and has a pitchwise splitter location that is automatically optimized across the span. The structural and vibration characteristic of the new impeller are computed and compared with the conventional impeller by using 3D Finite Element Analysis. The flow through the inverse designed and conventional impellers are analysed by using a 3D CFD code both for impeller only and whole stage configurations. Furthermore comparison of the measured performance map of the inverse designed and conventional stages are presented. The results confirm that the inverse designed impeller results in improved stage efficiency of up to 3 points and improvements in pressure ratio of up to 4.5% while maintaining or slightly improving the compressor’s stable operating range.

