Applications
Design of an Inducer Pump with High Suction Performance and Backflow Control
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 a 3 Stage Axial LP Turbine for Aeroengine Applications
Design High Performance Centrifugal Compressor Vaned Diffusers
Design High Performance Axial Turbine Stages with More Uniform Exit Flow
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 High Efficiency Impellers with Splitter Blades
Design High Performance Centrifugal Compressor Impellers
Publications
- Development of Cryogenic Pump Hydrodynamics Using Inverse Design Method and CFD
- Study of Turbopump Inducers Designed by 3-D Inverse Design Method
- Improvements of Pump Suction Performance Using 3D Inverse Design Method
- Improvements of Inducer Inlet Backflow Characteristics Using 3-D Inverse Design Method
- Effects of Blade Loading on Pump Inducer Performance and Flow Fields
Case Studies
- Design of a Second Stage Hydrogen Rocket Turbopump by TURBOdesign1
- 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
- Application of TURBOdesign1 for the Compact Design of Rocket Engine Turbopump - JAXA
- TURBOdesign1 is Extensively Used at Voith Turbo for the Design of Hydrodynamic Torque Converters
Design Optimisation of Cryogenic Pump Inducer
This paper presents the result of design optimization for three-bladed pump inducer using a three-dimensional (3-D) inverse design approach, Computational Fluid Dynamics (CFD) and DoE (Design of Experiments) taking suction performance and cavitation instability into consideration. The parameters to control streamwise blade loading distribution and spanwise work (free vortex or non-free vortex) for inducer were chosen as design optimization variables for the inverse design approach. Cavitating and non-cavitating performances for inducers designed using the design variables arranged in the DoE table were analyzed by steady CFD. Objective functions for non-cavitating operating conditions were the head and efficiency of inducers at a design flow (Qd ), 80% Qd and 120% Qd . The volume of the inducer cavity region with a void ratio above 50% was selected as the objective function for inducer suction performance. In order to evaluate cavitation instability by steady CFD, the dispersion of the blade surface pressure distribution on each blade was selected as the evaluation parameter. This dispersion of the blade surface pressure distribution was caused by non-uniformity in the cavitation length that was developed on each inducer blade and increased when the cavitation number was reduced. The effective design parameters on suction performance and cavitation instability were confirmed by sensitivity analysis during the design optimization process. Inducers with specific characteristics (stable, unstable) designed using the effective parameters were evaluated through experiments.

