Accession Number:

AD0678429

Title:

SINGLE-SHAFT LOW-POWER GAS-TURBINE ENGINE (ODNOVALNYI GAZOTURBINNYI DVIGATEL MALOI MOSHCHNOSTI),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Svetlakov,Ch. L.
• Klisanich,N. P.
• Kartashov,V. G.

Report Date:

1967-11-21

Pagination or Media Count:

5.0

Abstract:

The report introduces a low-power gas turbine engine incorporating a centrifugal compressor and a mixed-flow turbine. The turbines output shaft is connected perpendicularly to the engine shaft through a reducing gear located between the turbine and the compressor. This arrangement reduces the overall dimensions of the engine and provides for an axial air inlet into compressor. The reducer is composed of a pair of spur gears and a pair of conical gears. A one-way clutch and a starter are mounted co-axially with the shaft of the engine. Author

Descriptors:

• (*GAS TURBINES
• PATENTS)
• AXIAL FLOW COMPRESSORS
• MIXED FLOW COMPRESSORS
• REDUCTION GEARS
• ENGINE AIR SYSTEMS COMPONENTS
• POWER
• DRIVE SHAFTS
• USSR

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE