34th Congress of the International Council of the Aeronautical Sciences

07 - Systems, Subsystems and Equipment

SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS

R. Tirschmann¹, D. Metzler², T. Koch², M. Spieler¹, W. Nendel¹, L. Kroll¹; ¹Technische Universität Chemnitz, Germany ;²Liebherr-Aerospace Lindenberg GmbH, Germany

Comprehensive simulations & tests were conducted in order to develop a deep understanding of the hydraulic rotor gap parameter of a novel High Efficient hydraulic Motor Pump (HEPP) for aerospace applications, which is essential for sizing and optimization. The simulation was verified with a lab demonstrator and real pump data giving confident about the estimated quality.


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