FIELD: ventilation.
SUBSTANCE: aircraft air-conditioning system control device comprises a transformation module and the computing module power command loop control air flow, the module power command temperature control loop mode control unit air conditioning, on-board computer system, and a control bidirectional multiplex bus information exchange. All the modules contain main channel and the control, respectively, and power module and control means.
EFFECT: increase the operational safety of the aircraft, the reliability, and validity of information formed in any configuration of air-conditioning systems.
2 cl, 1 dwg
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Authors
Dates
2017-04-21—Published
2015-10-19—Filed