Basic thermodynamic design of a two-stage turbocharging system for a kerosene-powered reciprocating piston aircraft engine

Project name

Basic thermodynamic design of a two-stage turbocharging system for a kerosene-powered reciprocating aircraft engine

Project duration

01.01.2016 - 30.06.2019

Brief description

The aim of this research project is to demonstrate the potential for increasing the efficiency of the Centurion 2.0 with the aid of two-stage turbocharging. Two-stage turbocharging is a proven means of increasing performance and efficiency in vehicle engine construction. The project is a joint project with the Chair of Internal Combustion Engines at TU Dresden. The TU Dresden is to support the project with its expertise in the use of simulation tools and its experience in matching turbochargers to combustion engines. As part of the project, an engine in the aircraft is to be measured according to the specifications of TU Dresden so that they can create and validate a simulation model. This model will then be used to examine and evaluate various charger configurations. The best-value variant will then be implemented in a research setup on the engine test bench in order to confirm the results of the simulation.

Cooperation partner

• Technify Motors GmbH, - (Germany)

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