A Compatible Aircraft Liquid Cooling Equipment
A compatible and aircraft technology, applied in the direction of cooling/ventilation/heating transformation, etc., can solve problems such as low efficiency, high equipment cost, and bulky equipment, and achieve the effects of cost reduction, lower working level, and enhanced adaptability
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[0038] The present invention will be described in detail below with reference to the drawings and embodiments.
[0039] The system block diagram of the compatible liquid cooling equipment of the present invention is shown in figure 1 As shown, it is mainly composed of: power distribution unit 1, controller unit 2, operation panel 3, hydraulic unit 4, refrigeration unit 5 and equipped with some necessary oil, gas, and electric pipelines.
[0040] The function of the power distribution unit 1 is to transform and rectify the external power supply, and distribute it to the controller unit, hydraulic unit, refrigeration unit and loading truck to drive the operation of various parts. It is mainly composed of rectifier modules, AC contactors, circuit breakers, relays, drivers and other electrical components.
[0041] The controller unit 2 is used to receive operation panel signals, collect pipeline flow, pressure, temperature and other sensor signals, input analog and digital signals to the...
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