Integrated system backup devices PSOE-2, PSOE-50
http://www.temp-avia.ru/catalog/detail/58/
Title:
Integrated system backup devices PSOE-2, PSOE-50
Category:
System
The system is designed to replace a number of redundant flight control and navigation of electromechanical devices and provides independent measurement and indication of the spatial position of the aircraft to roll, pitch, gyromagnetic course as well as an indication of altitude-airspeed parameters.
Features:
The system is designed on the basis of the scheme gimballess orientation and active matrix liquid crystal panel. As sensors are used precision accelerometers, gyroscopes and fiber external magnetometer.
Specifications:
- Error in determining the indication of the angles:
- Roll and pitch in a steady level flight ± 0,5 °;
- On the gyromagnetic rate at 0.06 N ground - 0,27 Oe ± 2 °;
- Range of a given course of ± 180 °;
- The pressure at the Earth 520 - 806 mm Hg;
- Relative pressure altitude from -500 to 30000 m;
- Dash speed of 90 - 1480 km / h;
- Barometric vertical speed of ± 500 m / s;
- Mach 0.2 - 3.0;
- Overloading the normal -4 9;
- Rb radio ± 180 °;
- The size of the working field of the indicator:
- PSOE-2 61,2 × 61,2 mm;
- PSOE-50 61,2 × 81,2 mm;
- MTBF 10000ch;
- Warm-up time 3 min;
- Continuous operation time: 12h;
- Reception and delivery of information:
- In the form of serial bipolar code in accordance with GOST 18977-79 and 1495-75 for the RTM PSOE-2;
- Serial interface trunk GOST 52070-2003 for the PSOE-50;
- Power supply:
- DC voltage of 27V from two sides;
- Weight:
- Not more than 3,2 kg for block orientation and display;
- Not more than 0,5 kg for the magnetometer;
- Dimensions of the unit orientation: 105 × 105 × 230mm;
- External influences on the GOST RV 20.39.304