Assembly for aircraft, comprising a specific architecture for the distribution of fuel composition and electricity

An aircraft, comprising:

• an assembly of:
• at least one wing provided with at least one propulsion structure, referred to as a pod, and
• a fuselage,
• a zone, referred to as a hot zone, including elements at temperatures, referred to as hot temperatures, greater than or equal to a temperature, referred to as a hot zone temperature, and another zone, referred to as a cold zone, including elements at temperatures, referred to as cold temperatures, less than or equal to a temperature, referred to as a cold zone temperature, the hot zone and the cold zone being distinct from each other, and the cold zone temperature being lower than the hot zone temperature,
• an electricity generation system being located in the hot zone, and
• at least one fuel composition storage tank for supplying said electricity generation system being located in the cold zone, and
• an electric propulsion unit including a motor and a motor control unit configured to be electrically powered by the electricity generation system to produce thrust.