The Control System of the Soviet Turbofan Engine D-30
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
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In the article they have described the operation principles of main components of control system of sovietic turbofan engine D-30 the fuel flow control unit NR 30 that retains constant rotational speed of the high pressure compressor in various flight conditions the centrifugal governor CR IW that limits the low pressure compressor speed and the centrifugal governor CR 2W that controls the bleed valves and the inlet guide vanes of the high pressure compressor.
- Jet and Gas Turbine Engines