Aircraft cabin temperature regulating method based on three-wheel high-pressure water removing system

The invention relates to the technology of control over the temperature of an aircraft cabin, in particular to an aircraft cabin temperature regulating method based on a three-wheel high-pressure water removing system. The regulating method comprises the following steps that a temperature control valve and a cold air channel regulating valve are controlled to be started according to initial opening degrees; the temperature control valve is controlled according to a first control period, and the opening degree of the cold air channel regulating valve is regulated according to the difference value of the target temperature value of an outlet of a gas compressor and the actual temperature value, collected in real time, of the outlet of the gas compressor; the cold air channel regulating valve is controlled according to a second control period, and the opening degree of the temperature control valve is regulated according to the difference value of the target temperature value of the supplied air of the cabin and the actual measurement temperature value, collected in rear time, of the supplied air of the cabin. According to the aircraft cabin temperature regulating method based on the three-wheel high-pressure water removing system, on the condition that the temperature of supplied air of the cabin is not exceeded, quick cooling and heating of the cabin are achieved, the problem that the temperature of the supplied air is low when a cabin temperature control system is started is solved, and meanwhile the response speed of the cabin temperature in the operating process of the system is increased.