FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. System for power supply of aircraft of vertical take-off and landing, which includes: M aircraft beams, where M is an integer, ≥ 4, leading to electric motors of rotors through electronic stroke controllers (ESC); N lithium-ion elements, where N is an integer, ≥ 30, interconnected rigidly or flexibly depending on binder element - plate or wire blocks in parallel or in series; Z internal insulated cavities of aircraft body, where Z is an integer, ≥ 1. Lithium-ion elements are spatially spaced apart and arranged in blocks in inner isolated cavities of aircraft assemblies in beams and/or in internal insulated cavities of aircraft body. Lithium-ion cells form battery-conductor of energy from centre of aircraft body to electric motors of rotors by beams.
EFFECT: longer duration and range of aircraft flight is achieved.
1 cl, 1 dwg
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