Delivery set of Fire detection system SOP-62:
- 6 signaling device channels;
- possibility to protect two compartments (3 signaling device channels per compartment);
- low probability of false operation (mean time between such failures as false operation no less than 5х107 hours);
- continuous monitoring of the signaling device channels and continuity of the executive unit circuits;
- data exchange on two dual-redundant buses CAN (ARINC 825);
- low power consumption (less than 200 mА);
- possibility of power supply by two independent direct current buses with a voltage from 18 to 32.2 V;
- registration of the system operating time during the flight and on the ground.
Specification of Integrated fire protection system for trendsetting aircrafts SOP-62
| Executive unit BI-062C | ||
| Length | 220 mm | |
| Width | 132 mm | |
| Height | 83 mm | |
| Unit weight | no more than 0.9 kg | |
| Operating temperature | -60...+85 °С | |
| Universal fire signaling device USP-3 | ||
| Signaling device weight | no more than 0,061 kg | |
| Channel response temperature | from 200 to 350 °С | |
| Number | 18 pcs | |
| Operating temperature in the protected compartment | no more than 180 °С | |
The fire detection system SOP-62 is intended to generate a signal “FIRE” in blown engine compartments of the aircraft power plant.
