The Control System of the Soviet Turbofan Engine D-30

Abstract

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.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1972
Accession Number
AD0742368

Entities

People

  • Emil Wegrzyn

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Pressure
  • Compressors
  • Control Systems
  • Engines
  • Flow
  • Foreign Technology
  • Guide Vanes
  • High Pressure
  • High Pressure Compressors
  • Hypervelocity Flow
  • Inlet Guide Vanes
  • Regulators
  • Resistance
  • Solenoid Valves
  • Solenoids
  • Speed Regulators
  • Turbofan Engines

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerodynamics.
  • Petroleum Engineering