FIELD: automatic control units; flying vehicle air-conditioning systems. SUBSTANCE: proposed device has damper operated by electric motor, damper position feedback unit, pressure sensor unit, intellectual channels for calculation of required pressure in pressure cabin, channel serviceability monitoring unit, arbitrator for selecting drive channel, reserve channel and controllers of multiplex information exchange channel with on-board systems. EFFECT: enhanced reliability; improved quality of control. 1 dwg
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Authors
Dates
2003-11-20—Published
2001-10-08—Filed