| 摘要 |
An electrical aircraft comprises a piston or rotary or turbojet or jet internal combustion engine, comprising a carburetor or a technical device for preparing the mixture of working fuel from detonating mixture, atmospheric air, gasoline or diesel fuel or rapeseed oil, a technical device for production of detonating mixture of global energy according to the physical and chemical technology, namely decomposition of working snow or rain water by electrochemical method comprising: sealed, prefabricated dielectric housing made with upper and lower lids, upper nozzle with a supply valve and lower supply valve, valve with a funnel and a device for measuring the level of filling working snow or rain water and filling with dry KOH, a nozzle with a valve of consumption of working snow or rain water, a pipe with a suction valve, a circulating pump, a delivery valve of working snow or rain water, n number of electric circuit breakers of high frequency low dc, 5% aqueous solution of KOH, a chamber of detonating mixture with a pipe and a drain valve of detonating mixture, a receiver with a pressure gauge, an electric contact, a check valve, a pipe with a control valve for drain-supply of detonating mixture of global energy. It comprises a cigar-shaped housing made of light polymer material comprising a fixed lower stand that comprises a fixed piston engine with a gear box and an electric generator, on 3 supports of a forks with shock absorbers and on axes with inflatable wheels, a cockpit of pilot and flight engineer, a cabin for 3 passengers, an upper stand that comprises a fixed U-380v electric engine of vertical take-off, whose rotor axle comprises fixed propeller blades, which comprises a fixed bearing plate-shaped wing of durable and lightweight polymer material comprising two identical engines U-380v of horizontal take-off on identical brackets, whose rotor axles at both ends contain identical blades of propellers having a flight stabilizer in the air, which comprises identical hydraulic actuators of elevators and rudder comprising an oil pump. |
