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Standby Engine Indicators

Unified range of standby engine indicators IRDX-X

Destination:

Measuring and indication of the main parameters of two aviation engines simultaneously.

Main technical characteristics:

  • Measurement of input electrical signals of each engine from:
  • - two speed sensors;
  • - one thermocouple;
  • - one parameter from Engine Control Unit in ARINC-429 form.
  • Processing and displaying of 4 parameters of each engine on liquid-crystal display (LCD) in digital form.

Application in the aircrafts:

  • Beriev - 200 (IRD1-1)
  • Tupolev - 334 (IRD2-1)
  • Tupolev - 204 (IRD2-2/7)
  • Tupolev - 214 (IRD2-2/7)
Unified range of standby engine indicators IRDX-X

Standby engine indicator IRD1-2

Destination:

Receiving in code form and displaying of the main parameters of two aviation engines simultaneously.

Main technical characteristics:

  • Receiving of code signals by ARINC-429 from electronic modules of each engine
  • Processing and displaying of the following parameters of each engine on liquid-crystal display (LCD) in digital form:
  • - two rotor speed;
  • - gas temperature behind the turbine;
  • - "Degree of pressure increase in compressor" parameter.
  • Processing and displaying of 4 parameters of each engine on liquid-crystal display (LCD) in digital form.

Application in the aircrafts:

  • Beriev  - 200 (IRD1-2)
Standby engine indicator IRD1-2

ABRIS  JSC
Dudko street 3 liter X, Saint-Petersburg, 192029    Russia
Tel:7(812)242-05-56

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