Accession Number:

AD0742368

Title:

The Control System of the Soviet Turbofan Engine D-30

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1972-02-01

Pagination or Media Count:

13.0

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.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE