FIELD: fire fighting equipment.
SUBSTANCE: invention relates to fire engineering and is intended for use on aircraft. Fire protection control system for aircraft is characterized by that it comprises first fire protection means control unit, fire protection second control unit, m units of concentrators, n universal fire alarms, main multiplex channel of information exchange, wherein first fire equipment control unit comprises first commands power commands unit, module for limitation of currents of the first unit, connected to each other, and module of power commands of the first unit is connected to fire extinguishing devices, main channel of the first unit, which includes module of main channel processor of the first unit, interface module of the main channel of the first unit, power module of the main channel of the first unit connected to each other, wherein interface module of the main channel of the first unit interacts with on-board radioelectronic equipment and control elements of fire extinguishing in aircraft cabin.
EFFECT: technical result consists in wider range of the same purpose tools.
1 cl, 1 dwg
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Authors
Dates
2020-07-21—Published
2019-12-17—Filed