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This paper presents the results of the development of a cryogenic pump, consisting of inducer, impeller and diffuser, for Liquefied Natural Gas (LNG) transfer and pressurization. The newly designed pump was tested by using water test tunnel and showed good suction performance.

In this paper, a methodology is proposed for 3D multi-objective design of axial turbine blades in which a 3D inverse design method is coupled with a multi-objective genetic algorithm.

 Within the present study a runner-blade profile for a low head pumpturbine has been developed. This paper has been presented during the 25th IAHR Symposium on Hydraulic Machinery and Systems.

This paper presents a design process coupling a 3D inverse design approach with a Multi Objective Genetic Algorithm (MOGA) for axial cooling fan.

ADT is one of ALPHEUS project partner: a €5m project funded by the European Union’s Horizon 2020 program. It will improve reversible pump/turbine (RPT) technology and adjacent civil structures needed to make pumped hydro storage economically viable in shallow seas and coastal environments with flat topography.

The design of waste water pumps requires complicated trade-off between non-clogging characteristic of the impeller with its efficiency and cavitation performance. In this webinar, we will show an automated process for optimizing the design of waste water pumps by using 3D inverse design method.

The client is one the leading manufacturers of torque converter in automotive industry. In this project they asked ADT to perform a hydrodynamic design optimisation of a torque converter using the inverse design code TURBOdesign1.

The client is a major manufacturer of large industrial pumps. They needed an accurate performance prediction of a double-suction volute pump with an estimated design flow rate of 6.00 cubic meters per second. 

This webinar present a rapid and efficient design and optimization process for axial contra-rotating fans. The speakers - Prof. Mehrdad Zangeneh, Saurabh Gupta and Tobis Sieger - present application of TURBOdesign tools for the preliminary multi-blade row design of the axial fan where the rpm and pressure rise repartition of the different stages are varied.