کنفرانس بین المللی فناوری و مدیریت انرژی

صفحه اصلی / نهمین کنفرانس بین المللی فناوری و مدیریت انرژی

Conceptual Design of a Partial Hybrid Electric Engine for Small UAVs Propulsion System

نویسندگان :

Amin Anjomrouz¹

1- دانشگاه صنعتی شریف

کلمات کلیدی :

electric engine،hybrid،SFC،turbine engine،thrust

چکیده :

Turbine and electric engines are used in many applications that in some cases are similar to each other like propulsion sources in unmanned aerial vehicles (UAVs). For this reason, hybridization is a good idea to use both turbine and electric engines advantages. In this research, the conceptual design of a partial hybrid electric engine is performed. Engine modeling and validation of the results are done. Both series and parallel configurations are investigated and a good improvement in thrust and specific fuel consumption (SFC) of the engine is achieved. As a result, in the partial parallel hybrid configuration, the engine thrust is increased and SFC is decreased by about 2.95 and 2.86 % respectively.

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