Otabek Khamidov

Having studied the formation of technical requirements for the energy complex of a medium-range aircraft for 150 passengers on electric traction with the development of an electricity generation system (with the development of a distributed electric power plant), I now want to move to the next step which is to calculate characteristics and design a compact stable electric motor with a power of 1 MW and a hydrogen power plant for an electric aircraft on hydrogen with a hydrogen power plant for medium and long-distance flight. Upon implementation of the above systems, my attention will be divided into three main components of the electric aircraft. The first component is a 1 MW electric motor. The second component is a power plant based on hydrogen-oxygen fuel cells suitable for operation at high altitudes. And the third component is, a stable system with a filter and a high-power air compressor. I want to develop and calculate these three main aspects to implement them in reality and apply them.