The aim of this thesis was the design of a retractable, electric propulsion system for
sailplanes, which could eliminate the main drawbacks of internal combustion
engines. The design process was based on a number of modern sailplanes, within
the 12 - 15 meter class, with sustainer operation in mind. One of the goals was to
create a universal propulsion system that could be fitted to various aircrafts.
The first part of the project concerned the selection of the key components of an
electric propulsion system. First, the required power and thrust were calculated, and
based on the obtained results a suitable electric motor was chosen. For this motor,
an electronic controller was selected. Later, the estimation of propeller parameters
was performed. Finally, battery basics were discussed and a battery was selected.
The second part of the project concerned CAD modeling of the retractable electric
propulsion system. The used materials were discussed in the beginning. The design
process focused on two main assemblies: the propeller folding mechanism and the
retractable structure. The complete result, the individual sub-assemblies and the
most important solutions were presented. The use of composite materials was an
important point of this thesis. Performance analysis was done after the system had
been designed.
The retractable electric propulsion system was designed with optimum results. A fullscale
CAD model was created. The designed propulsion system can be considered
as universal due to its relatively low weight, adequate power and compact size in the
retracted position. Custom-made accessories facilitate mounting. A visit to the glider
manufacturer Allstar PZL was the source of information about possible mounting
solutions and battery placement options. The designed propulsion system can be
used as a sustainer for all designated sailplanes. Self-launching proved possible in
case of the lightest sailplanes. With similar power and flight duration, the electric
propulsion system should be able to compete with petrol powered sustainer systems
within the same class.
