Accession Number:

AD0481384

Title:

CONTINENTAL TS120 TURBOSHAFT ENGINE. POWER CONTROL SYSTEM. SUPPLEMENT

Descriptive Note:

Design rept.

Corporate Author:

CONTINENTAL AVIATION AND ENGINEERING CORP DETROIT MI

Personal Author(s):

Report Date:

1965-12-01

Pagination or Media Count:

30.0

Abstract:

This report presents the design of the power control system for a basic single-spool turboshaft engine and the variations possible with this basic design. These variations cover engines with outputs of 60, 90, and 120 horsepower, recuperated and non-recuperated versions, along with direct drive and geared output speeds. Included are schematic diagrams, description of the fuel control scheduling and governing methods, estimated engine fuel schedules, and a brief discussion of those changes which have been made to the power control system since the submission of the main engine design report.

Descriptors:

• *GAS TURBINES
• ACCELERATION
• CONTROL SYSTEMS
• ENVIRONMENTAL TESTS
• EXHAUST GASES
• FLOWMETERS
• FUEL CONSUMPTION
• FUEL FILTERS
• FUEL METERS
• FUEL NOZZLES
• FUEL PUMPS
• GAS FLOW
• HIGH PRESSURE VALVES
• MEASURING INSTRUMENTS
• OPERATION
• PERFORMANCE(ENGINEERING)
• PRESSURE
• TEMPERATURE CONTROL

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE