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Faculty of Aerospace Engineering

Field of Research
Electronic military equipment weight as well as MAV flight time is highly dependent on achievable electric energy density. Therefore, the development of a 300W kerosene driven Ultra Micro Gas Turbine (UMGT) prototype is proposed, which is foreseen to triple energy density compared to current Li-Ion batteries. UMGT developments of previous research projects did not achieve useful electric power output due to manufacturing limitations and unstable air bearings. To encounter these shortcomings, the proposed project will facilitate an additive ceramic manufacturing approach, allowing outstanding design flexibility and material properties. As current high-end ball bearing technology is suitable for the demanding operating conditions of UMGTs, ceramic hybrid bearings will lead to reliable operation of the turbine rotor. In accordance with experimental tests, an analytic engine model will be established to evaluate multiple engine configurations, leading to a highly redundant development process that will result in a multi-parameter optimized UMGT prototype.
Hiring

Requested profile (background and skills):

  • A pre-existing solid background, or a strong desire to acquire knowledge, in the following subjects is essential: Cycle Analysis, Aero-Thermal Design of Gas Turbines,
    Turbomachinery Aerodynamics, Optimization.
  •  Expertise in finite element / volume solvers (such as COMSOL, ANSYS, Fluent, CFX), and proficiency in MATLAB is a strong benefit.
  • High level of English language proficiency is desirable.
  • Candidates are expected to be self-motivated, hardworking and team players.

This position is for MSc and PhD students

Start Date: Immediate

Apply to:
beni@cukurel.org

Website: https://bcukurel.net.technion.ac.il/

Professor Beni Cukurel
Email: beni@cukurel.org

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