• 제목/요약/키워드: Gas turbine generator

검색결과 207건 처리시간 0.023초

HTGR PROJECTS IN CHINA

  • Wu, Zongxin;Yu, Suyuan
    • Nuclear Engineering and Technology
    • /
    • 제39권2호
    • /
    • pp.103-110
    • /
    • 2007
  • The High Temperature Gas-cooled Reactor (HTGR) possesses inherent safety features and is recognized as a representative advanced nuclear system for the future. Based on the success of the HTR-10, the long-time operation test and safety demonstration tests were carried out. The long-time operation test verifies that the operation procedure and control method are appropriate for the HTR-10 and the safety demonstration test shows that the HTR-10 possesses inherent safety features with a great margin. Meanwhile, two new projects have been recently launched to further develop HTGR technology. One is a prototype modular plant, denoted as HTR-PM, to demonstrate the commercial capability of the HTGR power plant. The HTR-PM is designed as $2{\times}250$ MWt, pebble bed core with a steam turbine generator that serves as an energy conversion system. The other is a gas turbine generator system coupled with the HTR-10, denoted as HTR-10GT, built to demonstrate the feasibility of the HTGR gas turbine technology. The gas turbine generator system is designed in a single shaft configuration supported by active magnetic bearings (AMB). The HTR-10GT project is now in the stage of engineering design and component fabrication. R&D on the helium turbocompressor, a key component, and the key technology of AMB are in progress.

가스터빈 열병합발전 시스템의 설계점 설정 및 부분부하 성능해석 (Analysis of Design and Part Load Performance for gas Turbine Cogeneration Systems)

  • 김동섭;노승탁
    • 대한기계학회논문집
    • /
    • 제18권8호
    • /
    • pp.2167-2176
    • /
    • 1994
  • This paper presents some useful design criteria for the turbine cogeneration system through both the design and off-design analysis. Comparative analysis of the part load performance is carried out for several gas turbines which have different design parameters represented by the turbine inlet temperature and pressure ratio. It is shown that the variation in part load efficiency considerably depends on the design parameter. The off-design operation of the heat recovery steam generator is simulated by introducing adequate assumptions for the heat transfer process. It is turned out that the design parameters of heat recovery steam generator should be determined by considering the favorable operation at the off-design conditions.

가스터빈 발전기 고정자 권선의 절연상태 평가 (Assessment of Insulation Condition in Gas Turbine Generator Stator Windings)

  • 김희동;양규현;주영호
    • 전기학회논문지
    • /
    • 제59권8호
    • /
    • pp.1423-1428
    • /
    • 2010
  • The results of off-line and on-line diagnostic tests performed on the stator winding of an air-cooled gas turbine(G/T) generator are reported in this paper. Off-line diagnostic tests included measurements of the ac current, dissipation factor(tan${\delta}$), and partial discharge(PD). Six epoxy-mica capacitors were installed in the three phases of G/T generator for performing on-line diagnostic testing with the turbine generator analyzer(TGA). The TGA showed that the normalized quantity number(NQN) and the PD magnitude($Q_m$) were high in phase A of the stator winding. Internal discharges were generated in phases B and C, and slot discharge occurred in phase A. According to the trend analyses of the NQN and $Q_m$ values available for insulation condition assessment for G/T generator stator windings, it was concluded that phases B and C were in good condition, whereas phase A has been significantly deteriorated.

추진제 공급압력이 액체로켓엔진의 성능에 미치는 영향 (Effect of Propellant-Supply Pressure on Liquid Rocket Engine Performance)

  • 조원국;박순영;남창호;김철웅
    • 대한기계학회논문집B
    • /
    • 제34권4호
    • /
    • pp.443-448
    • /
    • 2010
  • 가스발생기 사이클 액체로켓엔진에서 추진제의 공급압력 변화에 대한 성능 즉, 연소압, 터빈 파워, 엔진 혼합비, 가스발생기 연소가스의 온도 변화를 제시하였다. 로켓엔진의 주요 13개 시스템 레벨 변수를 이용하여 엔진 성능을 수치적으로 계산한다. 산화제 공급압이 증가하면 연소압과 터빈 파워는 증가하며 연료 공급압이 증가하면 연소압과 터빈 파워가 감소한다. 연료 유량 증가에 따라 감소된 가스 발생기의 혼합비는 연소가스 온도를 감소시키며 터빈 구동매질로서의 연소가스 물성을 저하시킨다. 연료 유량 증가에 따라 감소된 터빈 파워는 엔진 추력에 직접 영향을 미치는 주연소기의 연소압을 감소 시킨다.

터빈-발전기 조속기의 동특성 시험시스템 개발에 관한 연구 (A study on the Turbine-Generator Governor Dynamic Characteristic Testing System)

  • 최형주;이흥호
    • 전기학회논문지
    • /
    • 제61권10호
    • /
    • pp.1399-1411
    • /
    • 2012
  • The grid frequency is controlled cooperatively by the governor of the Turbine-Generator and the automatic generation controller(AGC) of the KPX(Korea Power Exchange). It is a basic requirement that the reliability of the governor is verified to enhance the power system stability but it is not easy to confirm the response characteristics of the governor because all generators are operated in the grid system that has the constant voltage and frequency. Therefore, it is necessary to study a new test method in order to examine the governor dynamic characteristic in the similar fault conditions. A study has shown that it is verified to simulate the turbine-generator power control system, the governor response characteristic under limited conditions and contribution of AGC with the gas turbine generator simulation model as well as demonstrate the dynamic response of the governor with the developed governor dynamic characteristic tester based on digital controller while the turbine-generator is connected to the grid system. This tester is constructed by the built-in functions of the turbine-generator main controller. In this treatise, the theoretical background, development method and the results of both simulations and demonstrations are described as another way to verify the turbine-generator governor dynamic characteristics.

가스발생기 내부 유동 특성에 관한 수치 연구 (Numerical study on the reactive flow in Gas Generator)

  • 유정민;이창진
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
    • /
    • pp.198-202
    • /
    • 2005
  • 가스발생기는 액체 추진 로켓의 터보 펌프 시스템에서 터빈을 구동시키기 위한 중요한 장치이다. 터빈 블레이드의 보호를 위해서 가스발생기의 출구 온도가 제한을 받으며, 이를 위해 농후 연소를 발생시킨다. 본 연구에서는 가스발생기의 연소에 대한 수치적 연구를 통하여 가스발생기 내부의 유동 특성을 이해하고 나아가 가스발생기의 성능을 예측할 수 있는 수치 해석 도구의 개발을 목표로 하고 있다.

  • PDF

액체산소/케로신 가스발생기 사이클 액체로켓엔진 터빈 노즐목 면적 변화 추정 방법 (Estimation Methods for Turbine Nozzle Throat Area Reduction of A LOx/Kerosene Gas Generator Cycle Liquid Propellant Rocket Engine)

  • 남창호;문윤완;박순영;김진한
    • 한국추진공학회지
    • /
    • 제23권5호
    • /
    • pp.101-106
    • /
    • 2019
  • 액체산소/케로신 가스발생기 사이클 엔진의 터빈 노즐목 수트(soot) 침착 특성을 파악하기 위한 변수를 정의하고 한국형발사체 1단 엔진 시험결과에 적용하였다. 터빈 가스의 물성치를 이용한 노즐목의 분출 계수 정의를 하는 방법이 있고 터빈 노즐목 전단과 터빈 배기 노즐목 전단의 압력비와 온도비를 이용하여 분출계수를 정의할 수 있다. 한국형발사체 1단 엔진 시험 결과를 분석한 결과 터빈 노즐목의 분출계수(discharge coefficient)는 시간에 따라 감소하며 동일 엔진에 대한 누적 연소시간에 대해서도 감소하는 경향을 보인다. 누적 시험 초기에는 터빈 노즐목 감소가 그 다음 시험과 연계되지만 일정 시간 이후에는 일정 범위에서 등락을 거듭하는 듯한 특성을 보인다.

Analysis of Insulation Diagnosis and Failure in Stator Windings of Air-Cooled Gas Turbine Generator

  • Kim, Hee-Dong;Kong, Tae-Sik;Kim, Kyeong-Yeol
    • KEPCO Journal on Electric Power and Energy
    • /
    • 제2권3호
    • /
    • pp.421-424
    • /
    • 2016
  • In order to evaluate the insulation deterioration in the stator windings of air-cooled gas turbine generators(119.2 MVA, 13.8 kV) which has been operating for more than 15 years, diagnostic test and AC dielectric breakdown test were performed on phases A, B and C. Diagnostic test included measurements of AC current, dissipation factor, partial discharge (PD) magnitude and capacitance. ${\Delta}I$ and ${\Delta}tan{\delta}$ in all three phases (A, B, and C) of generator stator windings showed that they were in good condition but PD magnitude indicated marginally serviceable condition. After the diagnostic test, an AC overvoltage test was performed by gradually increasing the voltage applied to the generator stator windings until electrical insulation failure occurred, in order to determine the breakdown voltage. Although phase A of generator stator windings failed at breakdown voltage of 29.0 kV, phases B and C endured the 29.0 kV. The breakdown voltage in all three phases was higher than that expected for good-quality windings (28.6 kV) in a 13.8 kV class generator.

마이크로 가스터빈 시험 장치 개발 (Development of Test Facility for Micro Gas Turbine)

  • 임형수;최범석;박무룡;황순찬;박준영;서정민;방제성;임영철;오인균;김병옥;조주형
    • 한국유체기계학회 논문집
    • /
    • 제18권5호
    • /
    • pp.42-48
    • /
    • 2015
  • To improve the core technology of the micro gas turbine, the performance test facility was developed. This paper is focusing on the explanation of the characteristics of micro gas turbine and its assist devices. Major part of micro gas turbine were radial type of compressor, annular type of combustor, radial type of turbine, thrust foil bearing, radial foil bearing and generator. The assist devices were consist of exhaust duct, inverter, data acquisition system, load bank and test cell. Before building up the test facility, the component test was previously conducted to confirm the component performance. After the test facility was prepared, the motoring test was conducted to investigate the rotor dynamic characteristics of the micro gas turbine. Also, the part load performance test was performed. With a developed micro gas turbine test facility, the improved core technology about the micro gas turbine can be suggested to the related industries.

부하차단시험에 의한 서인천복합화력 발전기.제어계의 모델링 및 검증 (Modeling and verification of generator/control system of Seo-Inchon combined-cycle plant by load rejection test)

  • 최경선;문영환;김동준;추진부;류승헌;권태원
    • 대한전기학회논문지
    • /
    • 제45권4호
    • /
    • pp.501-510
    • /
    • 1996
  • The gas-turbine generator of Seo-Incheon combined-cycle plant was tested for derivation of a model for dynamic analysis. Load rejection and AVR step test was performed to get the dynamic response of generator. The parameters of generator/control system model were determined by these measured data. No-load saturation test was performed for the saturation characteristics of the generator under steady state. V-curve test was also performed so as to find exact generator parameters. Q-axis parameters of generator was derived by measuring power angle. AVR and governor constants have been tuned by their oscillatory period and setting time characteristics. The derived parameters of generator control system is verified by one-machine infinite bus system simulation. (author). 7 refs., 20 figs., 5 tabs.

  • PDF