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100kW급 증기터빈 설계기술 개발에 관한 연구A Study of the Design Technology for Developing a 100kW Class Steam Turbine

Other Titles
A Study of the Design Technology for Developing a 100kW Class Steam Turbine
Authors
김영철안국영조종현조수용
Issue Date
2009
Publisher
한국유체기계학회
Keywords
Steam Turbine; Aerodynamic Design; Partial Admission; Supersonic Nozzle; Rotordynamic Analysis; 증기터빈; 공력설계; 부분분사; 초음속노즐; 회전체동역학적 해석
Citation
한국유체기계학회 논문집, v.12, no.3, pp 46 - 54
Pages
9
Indexed
KCI
Journal Title
한국유체기계학회 논문집
Volume
12
Number
3
Start Page
46
End Page
54
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/26874
ISSN
2287-9706
Abstract
Small scale steam turbines are used as mechanical drivers in chemical process plant or power generators. In this study, a design technology was developed for a 100kW class steam turbine which will be used for removing CO2 from the emission gas on a reheated cycle system. This turbine is operated at a low inlet total pressure of 5kgf/cm2. It consists of two stages and operates at the partial admission. For the meanline analysis, a performance prediction method was developed and it was validated through the performances on the operating small steam turbines which are using at plants. Their results showed that the output power was predicted within 10% deviation although the steam turbines adopted in this analysis were operated at different flow conditions and rotor size. The turbine blades was initially designed based on the computed results obtained from the meanline analysis. A supersonic nozzle was designed on the basis of the operating conditions of the turbine, and the first stage rotor was designed using a supersonic blade design method. The stator and second stage rotor was designed using design parameters for the blade profile. Finally, Those blades were iteratively modified from the flow structures obtained from the three-dimensional flow analysis to increase the turbine performance. The turbine rotor system was designed so that it could stably operate by 76% separation margin with tilting pad bearings.
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공과대학 > Department of Aerospace and Software Engineering > Journal Articles

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