Draft:TURBOdesign

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Last edited by LBossiADT (talk | contribs) 0 seconds ago. (Update)

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Comment: In accordance with Wikipedia's Conflict of interest policy, I disclose that I have a conflict of interest regarding the subject of this article. LBossiADT (talk) 18:30, 2 May 2025 (UTC)

TURBOdesign Suite is a software package developed by Advanced Design Technology (ADT), a UK-based engineering software company specializing in turbomachinery design. The suite is known for its unique use of three-dimensional inverse design methods to optimize the aerodynamic and hydrodynamic performance of turbomachinery components, such as compressors, turbines, pumps, hydraulic turbines, fans and blowers and torque converters.

Overview

TURBOdesign Suite employs unique 3D inverse design approach which unlike conventional turbomachinery design tools that rely on direct methods, where blade geometry is specified and analysed iteratively. In TURBOdesign users specify the desired fluid dynamic performance, typically in terms of characteristic requirements such as pressure ration, RPM and mass flow rate in compressors and turbines or head, / pressure rise and volume flow rate in pumps and fans, then impose optimal blade loading or pressure distribution, and the software rapidly computes the optimal blade geometry to meet those specifications.

The inverse method allows for direct control over flow features, leading to significant enhancements in efficiency, performance, and range in a shorter design cycle.

TURBOdesign Suite Environment

TURBOdesign Suite consists of several integrated modules:

TURBOdesign Pre – A tool for the meanline and preliminary design of turbomachinery stages, it covers applications for axial, mixed-flow, centrifugal compressors, turbines, pumps, hydraulic turbines, fans and blowers. In addition meanline capabilities are integrated in the refrigeration and heat pump cycles.
TURBOdesign1 – The 3D inverse design tool for generating blade geometries based on prescribed pressure loading and circulation distribution. The code supports the application of all bladed turbomachinery across wide range of specific speeds and working fluids.
TURBOdesign Volute – A specialized tool for the design of volutes in centrifugal compressors, pumps and fans which uses a two-dimensional inverse method for the calculation of the angular momentum and conservation of mass to identify the limiting streamline on the volute casing. TURBOdesign Volute supports the specification of a non-uniform variation of Vr and Vt at the inlet of the volute circumference.
TURBOdesign Optima – An optimization platform for automated multi-objective optimization of turbomachinery components. Optima relies on a range of numerical algorithms for optimization of the turbomachinery performance based on user defined constraints and objectives. The capabilities includes traditional optimization methods such as Multi Objective Genetic Algorithms (MOGA) as Non-Sorting Genetic Algorithms of Type 2 (NSGA-II) and Surrogate Modelling Optimization, starting from Design of Experiments Methods such as Optimal Latin Hypercube (OLH) and Response Surface Modelling with Kriging.
Reactive Response Surface (RRS) - A novel generation Machine Learning algorithm developed specifically for application to turbomachinery design challenges where high fidelity, small dataset are required for the performance optimization.

Optimum Blade Loading for Suppression of Adverse Flow Phenomena in Turbomachinery

The application of 3D inverse design methods in turbomachinery has enabled engineers to systematically suppress a range of adverse flow phenomena by directly manipulating the blade loading distribution to control flow behaviour. In radial pumps and compressors, inverse design has been shown to effectively reduce secondary flow and improve flow uniformity across the blade passage^[1]. By tailoring surface pressure distributions, it also aids in mitigating cavitation by reducing low-pressure zones on blade suction surfaces^[2]. In transonic centrifugal compressors, optimized blade loading helps suppress shock wave formation and associated losses. Additionally, in axial fans, inverse design has enabled a reduction in tip leakage flow by controlling the spanwise work distribution, leading to improved aerodynamic efficiency and lower noise emissions^[3].

Notable Customers

TURBOdesign Suite is widely used by industrial and academic institutions worldwide,

The Japan Aerospace Exploration Agency (JAXA) collaborated with Advanced Design Technology (ADT) to design a compact, high-performance turbopump for their rocket engines. By employing TURBOdesign1's 3D inverse design methodology, JAXA moved beyond traditional empirical approaches, enabling the development of innovative blade geometries that enhanced energy density while reducing weight and development time. This approach provided deeper insights into the pump's fluid dynamics, leading to improved performance and efficiency.

Red Bull Ford Powertrains (RBFPT) has adopted Advanced Design Technology's TURBOdesign Suite to develop high-performance turbochargers for their 2026 Formula 1 power unit. Utilizing TURBOdesign's 3D inverse design capabilities, RBFPT aims to streamline the turbocharger development process from initial conception through engine matching to detailed 3D component optimization. This approach enables rapid exploration of design options, allowing the engineering team to efficiently meet aerodynamic and mechanical performance requirements.

Avio Aero collaborated with Advanced Design Technology (ADT) to enhance their aeronautical turbine design process using TURBOdesign1 and TURBOdesign2. By adopting 3D inverse design methods, Avio transitioned from traditional 2D section-based approaches to direct 3D blade geometry generation, enabling rapid exploration of high-lift turbine blade concepts. This shift led to improved thermodynamic efficiency, reduced specific fuel consumption, and a significant decrease in engineering time through streamlined design-analysis iterations.

WEG, a global leader in electro-electronic equipment, adopted Advanced Design Technology's TURBOdesign Suite to enhance the design and optimization of their hydraulic turbines. By leveraging TURBOdesign's 3D inverse design methodology, WEG accelerated the development process, reduced manual workload, and improved turbine performance for both new and refurbishment projects. The integration of TURBOdesign Suite streamlined their workflow, enabling efficient generation of blade profiles and seamless compatibility with existing CAD, CFD, and FEA tools.^[4]

References

^ Zangeneh, M.; Goto, A.; Harada, H. (1998-10-01). "On the Design Criteria for Suppression of Secondary Flows in Centrifugal and Mixed Flow Impellers". Journal of Turbomachinery. 120 (4): 723–735. doi:10.1115/1.2841783. ISSN 0889-504X.
^ Bonaiuti, Duccio; Zangeneh, Mehrdad; Aartojarvi, Reima; Eriksson, Jonas (2010-03-18). "Parametric Design of a Waterjet Pump by Means of Inverse Design, CFD Calculations and Experimental Analyses". Journal of Fluids Engineering. 132 (031104). doi:10.1115/1.4001005. ISSN 0098-2202.
^ Okamoto, Hidenobu; Goto, Akira; Furukawa, Masato (2010-07-26). "Design of a Propeller Fan Using 3-D Inverse Design Method and CFD for High Efficiency and Low Aerodynamic Noise". American Society of Mechanical Engineers Digital Collection: 165–171. doi:10.1115/FEDSM2009-78454. {{cite journal}}: Cite journal requires |journal= (help)
^ Ltd, Advanced Design Technology. "WEG Selects TURBOdesign Suite for Leveraging the Hydraulic Turbine Design Process, Improving Substantially its Speed and Efficiency". www.adtechnology.com. Retrieved 2025-05-02.

Zangeneh, M., Goto, A., and Harada, H. (October 1, 1998). "On the Design Criteria for Suppression of Secondary Flows in Centrifugal and Mixed Flow Impellers." ASME. J. Turbomach. October 1998; 120(4): 723–735. https://doi.org/10.1115/1.2841783

Bonaiuti, D., Zangeneh, M., Aartojarvi, R., and Eriksson, J. (March 18, 2010). "Parametric Design of a Waterjet Pump by Means of Inverse Design, CFD Calculations and Experimental Analyses." ASME. J. Fluids Eng. March 2010; 132(3): 031104. https://doi.org/10.1115/1.4001005

Zangeneh, M. & Nikpour, B. & Watanabe, H.. (2010). Development of a high performance centrifugal compressor using a 3D inverse design technique. 135-145. 10.1243/17547164C0012010010.

Okamoto, H, Goto, A, & Furukawa, M. "Design of a Propeller Fan Using 3-D Inverse Design Method and CFD for High Efficiency and Low Aerodynamic Noise." Proceedings of the ASME 2009 Fluids Engineering Division Summer Meeting. Volume 2: Fora. Vail, Colorado, USA. August 2–6, 2009. pp. 165-171. ASME. https://doi.org/10.1115/FEDSM2009-78454

[1] Zangeneh, M.; Goto, A.; Harada, H. (1998-10-01). "On the Design Criteria for Suppression of Secondary Flows in Centrifugal and Mixed Flow Impellers". Journal of Turbomachinery. 120 (4): 723–735. doi:10.1115/1.2841783. ISSN 0889-504X.

[2] Bonaiuti, Duccio; Zangeneh, Mehrdad; Aartojarvi, Reima; Eriksson, Jonas (2010-03-18). "Parametric Design of a Waterjet Pump by Means of Inverse Design, CFD Calculations and Experimental Analyses". Journal of Fluids Engineering. 132 (031104). doi:10.1115/1.4001005. ISSN 0098-2202.

[3] Okamoto, Hidenobu; Goto, Akira; Furukawa, Masato (2010-07-26). "Design of a Propeller Fan Using 3-D Inverse Design Method and CFD for High Efficiency and Low Aerodynamic Noise". American Society of Mechanical Engineers Digital Collection: 165–171. doi:10.1115/FEDSM2009-78454. {{cite journal}}: Cite journal requires |journal= (help)

[4] Ltd, Advanced Design Technology. "WEG Selects TURBOdesign Suite for Leveraging the Hydraulic Turbine Design Process, Improving Substantially its Speed and Efficiency". www.adtechnology.com. Retrieved 2025-05-02.

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