23-06-2023 дата публикации
Номер: CN116280219A
Принадлежит:
The invention provides an electrolyzed water injection type aircraft which comprises an aircraft body and a lift power system, the lift power system comprises an electrolyzed water device and a gas injection device, the gas injection device comprises a combustion chamber, a spark plug and a spray pipe, the electrolyzed water device and the combustion chamber are both arranged in the aircraft body, and the electrolyzed water device is connected with the combustion chamber. Mixed gas generated by the water electrolysis device can be conveyed into the combustion chamber, the spark plug is arranged in the combustion chamber and can ignite the mixed gas, one end of the spray pipe is connected with the combustion chamber, the other end of the spray pipe extends out of the aircraft body, and high-pressure gas generated after combustion in the combustion chamber is sprayed out through the spray pipe. According to the electrolyzed water injection type aircraft, hydrogen and oxygen are controllably ...
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