TURBOdesign Pumps & Fans
TURBOdesign Suite provides tools to designers to put them in direct control of aerodynamic design to streamline every step of the design process for turbomachinery components.
Our Pumps & Fans packages
TURBOdesign Compressors & Turbines
TURBOdesign Suite provides tools to designers to put them in direct control of aerodynamic design to streamline every step of the design process for turbomachinery components.
Our Compressors and Turbines packages...
TURBOdesign Optima
TURBOdesign Suite provides tools to designers to put them in direct control of aerodynamic design to streamline every step of the design process for turbomachinery components.
TURBOdesign Optima is our automatic optimization package
3D Blade Design
Our turbomachinery design toolkits include one on 3D blade design...
Meanline Design
TURBOdesign Suite provides tools to designers to put them in direct control of aerodynamic design to streamline every step of the design process for turbomachinery components.
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Suspendisse varius enim in eros elementum tristique.
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Suspendisse varius enim in eros elementum tristique. Duis cursus, mi quis viverra ornare, eros dolor interdum nulla, ut commodo diam libero vitae erat. Aenean faucibus nibh et justo cursus id rutrum lorem imperdiet. Nunc ut sem vitae risus tristique posuere.
Volute/Scroll Geometries
TURBOdesign Suite provides tools to designers to put them in direct control of aerodynamic design to streamline every step of the design process for turbomachinery components.
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Suspendisse varius enim in eros elementum tristique. Duis cursus, mi quis viverra ornare, eros dolor interdum nulla, ut commodo diam libero vitae erat. Aenean faucibus nibh et justo cursus id rutrum lorem imperdiet. Nunc ut sem vitae risus tristique posuere.
Multi-Objective Optimization
TURBOdesign Suite provides tools to designers to put them in direct control of aerodynamic design to streamline every step of the design process for turbomachinery components.
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Suspendisse varius enim in eros elementum tristique. Duis cursus, mi quis viverra ornare, eros dolor interdum nulla, ut commodo diam libero vitae erat. Aenean faucibus nibh et justo cursus id rutrum lorem imperdiet. Nunc ut sem vitae risus tristique posuere.
Compressors
Test
Fans and Blowers
Test
Pumps and Hydraulic Turbines
Test
High Speed Turbines
Test
Academia
Test
Design Consultancy
Test
Research and Development
Test
Training
Blog
Catch up with the very latest and useful articles
Case Studies
Read our success stories from companies of all sizes who are transforming the way they design turbomachinery components.
Consultancy Summaries
Read our success stories from companies of all sizes who are transforming the way they design turbomachinery components.
Publication
Browse the latest and previous editions of our publications library
On-Demand Webinar Library
Playback our webinars
White Paper
Browse our white paper library.
For this project, ADT engineers were asked to design the compressor stage using the refrigerant R134a for a cooling system.
The client is a global leader in providing customized, high performing, highly engineered cooling systems. They asked ADT to design a compressor stage of a cooling system including an impeller with splitter blades, a vaneless diffuser and a volute for a target pressure and an efficiency level of about 3 points above their existing designs. Other constraints in the design were the maximum allowable stress level and vibration constraints.
Design targets
To design a refrigeration compressor stage using R134a to improve performance of the entire stage (impeller, vaneless diffuser and volute) and to meet various flow rates and pressure ratio requirements by trimming the impeller.
Deliverables
Three sets of geometries, including the full impeller, vaneless diffuser and volute as well as meridional trimmed impeller and spanwise trimmed impellers.
Impact
State-of-the-art compressor stage and series of trimmed geometries meeting all design targets.
Fig. 1. Flow streamlines in the compressor stage.
Mehrdad Zangeneh is Founder and Managing Director of Advanced Design Technology and professor of Thermofluids at University College London.
View All ArticlesIn the first part of this article, we showed how to perform the initial design of a radial inflow turbine rotor using the 3D inverse design method.
...
Share This Post