Comparison of Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion

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Comparison of Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion ( comparison-concepts-classic-jet-propulsion-turbo-electric-pr )

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15 The turbo-electric concept has been researched by various manufacturers and researchers for a while. But the initial information and explanation about various electric propulsion concepts were provided by Scholz (2018b) and NAS (2016). The NAS (2016) consisted of the basic definitions and comparison of the all the electric propulsion concepts. Gesell (2017) and Aigner (2018) also helped in the basic working principle of the concept. There are many pa- pers regarding this subject published by NASA and two of them that were helpful are Welstead 2016 and Felder 2011. For the Life Cycle Assessment of the aircraft, there are various concepts available to use. Jo- hanning (2016) served as a compilation all such concepts with a well-designed tool. Since the A320 aircraft was used a reference aircraft, a lot of basic parameters of the aircraft was required. These values were mostly extracted from Nita (2013) and Airbus (2019). 1.5 Structure of the Work The structure of this thesis is explained below Chapter 2 Chapter 3 Chapter 4 Chapter 5 Chapter 6 It gives an overview of existing research of all the propulsion concepts along with their basic working principle. It also includes the advantages and disadvantages of the concepts. This chapter covers the sizing method of turboprop, turboshaft, hydraulic and electric propulsion system. It mainly includes the mass estimations and architecture of the systems. It of consists of existing and newly developed empirical models. The preliminary sizing for the aircraft concepts are explained briefly here. The calculation of direct of costs and life cycle assessment of the aircraft is also determined. This section covers the results of the calculation done. The results are repre- sented in tables and graphs. The results are also briefly discussed, and rea- soning is given. Conclusion and summary of all the concepts are provided here. The best concept chosen.

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