Development of a 30PS Class Small Gas Turbine and Its Power-Up VersionSource: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 002::page 225DOI: 10.1115/1.3240240Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Due to the recent popularity of small and medium-sized industrial gas turbines in many fields, gas turbines below 100 SHP have been employed as prime movers, a power range traditionally reserved for diesel and gasoline engines. Generally speaking, however, small gas turbines have many design difficulties in thermal efficiency, high rotational speed, compact auxiliary equipment, etc., derived from limitations of their dimensions. Small gas turbines S5A-01 and S5B-01, which have 32 PS output power at standard conditions, have been developed and are being produced. Presently, a 30 percent growth rated power producer for S5A-02 and S5B-02 gas turbines is under development. These engines’ configurations are as follows: single-stage centrifugal compressor; single-stage radial turbine; single can combustor; hybrid fuel nozzle with pressure atomizer and airblast atomizer; fuel control valve with pulse width modulation system; electric motor drive fuel pump. In this paper, the authors describe the design features and development history of the base engine and the experimental results with the growth rated version.
keyword(s): Gas turbines , Fuels , Engines , Turbines , Design , Valves , Diesel , Pulse width modulation , Gasoline engines , Dimensions , Compressors , Fuel pumps , Industrial gases , Combustion chambers , Nozzles , Pressure AND Electric motors ,
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contributor author | A. Hoshino | |
contributor author | T. Sugimoto | |
contributor author | T. Tatsumi | |
contributor author | Y. Nakagawa | |
date accessioned | 2017-05-08T23:29:59Z | |
date available | 2017-05-08T23:29:59Z | |
date copyright | April, 1989 | |
date issued | 1989 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26665#225_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/105398 | |
description abstract | Due to the recent popularity of small and medium-sized industrial gas turbines in many fields, gas turbines below 100 SHP have been employed as prime movers, a power range traditionally reserved for diesel and gasoline engines. Generally speaking, however, small gas turbines have many design difficulties in thermal efficiency, high rotational speed, compact auxiliary equipment, etc., derived from limitations of their dimensions. Small gas turbines S5A-01 and S5B-01, which have 32 PS output power at standard conditions, have been developed and are being produced. Presently, a 30 percent growth rated power producer for S5A-02 and S5B-02 gas turbines is under development. These engines’ configurations are as follows: single-stage centrifugal compressor; single-stage radial turbine; single can combustor; hybrid fuel nozzle with pressure atomizer and airblast atomizer; fuel control valve with pulse width modulation system; electric motor drive fuel pump. In this paper, the authors describe the design features and development history of the base engine and the experimental results with the growth rated version. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Development of a 30PS Class Small Gas Turbine and Its Power-Up Version | |
type | Journal Paper | |
journal volume | 111 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3240240 | |
journal fristpage | 225 | |
journal lastpage | 231 | |
identifier eissn | 0742-4795 | |
keywords | Gas turbines | |
keywords | Fuels | |
keywords | Engines | |
keywords | Turbines | |
keywords | Design | |
keywords | Valves | |
keywords | Diesel | |
keywords | Pulse width modulation | |
keywords | Gasoline engines | |
keywords | Dimensions | |
keywords | Compressors | |
keywords | Fuel pumps | |
keywords | Industrial gases | |
keywords | Combustion chambers | |
keywords | Nozzles | |
keywords | Pressure AND Electric motors | |
tree | Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 002 | |
contenttype | Fulltext |