Pressure control system УФ90154М1–063.00.00Product components
The pressure regulating system includes the following components:
1. Control device, left
2. Control device, right
3. Actuating mechanism, left
4. Actuating mechanism, right
5. Dividing valve
Basic technical specifications
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Function
The pressure control system (in Russian "SRD") is used to supply hot air into anti-icing system of a wing and empennage of an aircraft, to regulate air pressure and to stop air supply according to digital control signal. In respect to resistance to mechanical and climatic effects the pressure control system complies with the requirements of "Unified Norms of Airworthiness" ENLG-S and has been certified in accordance with the Aviation Regulations AP-21.
Application
The system has-been entirely developed (optimized) and is used in the hot-air anti-icier for an aircraft of type AN-38.
Its design is protected by patents.
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