• Title/Summary/Keyword: 정압조건

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Turbo Expander Power Generation Using Pressure Drop at Valve Station in Natural Gas Transportation Pipeline (천연가스 정압기지의 압력강하를 이용한 터보팽창기 전력생산)

  • Ha, Jong-Man;Hong, Seong-Ho;You, Hyun-Seok;Kim, Kyung-Chun
    • Journal of the Korean Institute of Gas
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    • v.16 no.3
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    • pp.1-7
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    • 2012
  • Natural gas through pipeline is supplied to consumers after its pressure gets down compulsorily. The waste pressure energy of this process can be restored by use of turbo expander which can produce electricity. So, turbo expander conducts two functions - pressure reduction and power generation. The power amount is the enthalpy difference between the inlet and outlet states. The five main factors which affect economic profit are facility price, produced power amount, pre-heating amount, electricity cost, and fuel gas cost. Power generation depends mainly on flow amount because inlet and outlet states are fixed. A methodology to estimate economy in irregular flow pattern is proposed and using this way, a case study was carried out.

Mach 5 Performance Tests of Scramjet Engine Intake Using Free-jet Type Ground Propulsion Test Facility (자유제트형 지상추진 시험설비를 사용한 스크램제트 엔진 흡입구의 마하 5 성능시험)

  • Lee, Yang Ji;Yang, Inyoung;Lee, Kyung Jae;Oh, Jung Hwan;Choi, Jin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.26 no.4
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    • pp.10-20
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    • 2022
  • The performance analysis test of the scramjet engine intake was conducted under the Mach 5 condition of the scramjet engine test facility, a free-jet ground test facility of the Korea Aerospace Research Institute. A pitot/static pressure rake installed at the rear of the isolator was designed and manufactured to measure the total pressure recovery rate and mass capture ratio, which are typical performance factors of the scramjet engine intake. The effect of the rake mounted at the rear of the isolator on the intake, the performance analysis measured by the rake, and the change in wall static pressure distribution according to the angle of attack were performed. Finally, the point at which the intake unstart occurred was confirmed by using the rear back pressure adjusting device, which simulates pressure rise in the combustor, and the results are summarized in this paper.

최신 전자기술에 의한 항공기 전체 계통의 변화(2)

  • Lee, Sang-Jik;Byeon, U-Seo;Byeon, Jin-Gu
    • Defense and Technology
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    • no.7 s.245
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    • pp.38-47
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    • 1999
  • 대기의 상태는 지역, 시간, 기상 조건 등에 따라 변하므로 고도를 계산하는데는 북반구 중위도 지방에서 관측된 기상자료 등을 기준으로 제정한 표준대기를 적용한다. 속도를 계산하는데 전압과 정압의 압력차로 정의하는 항공기용 대기속도계 차압표를 사용한다. 계산된 에어 데이터는 비행계기나 cockpit display에 표시되어 조종사에게 정보로 전달됨과 동시에 자동조종 장치, 관성항법 장치, 비행관리 시스템, 항공관리 트랜스폰더 등에 기초 자료로 공급된다

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터보펌프 인듀서의 유동해석

  • Choi, Chang-Ho;Hong, Soon-Sam;Kim, Jin-Han
    • Aerospace Engineering and Technology
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    • v.2 no.2
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    • pp.25-32
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    • 2003
  • In the present paper, a computational study on the hydrodynamic behavior of the inducer are presented including the effect of the mass flow rate. The adopted inducer showed very low head rise with high volume flow rates, which may be caused by the small passage area near the trailing edge. The static pressure distributions at the shroud surface are compared with experimental results showing very good agreements. The overall performance of the inducer such as, efficiency, head rise is also compared with experiments. The computational results are generally in good agreements with experimental ones near the design point, but at the high flow rate, the two results shows discrepancy.

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Inverter Motor Drive System Development for High Static Pressure Ventilation Fan (고정압용 프리미엄 환풍기를 위한 인버터형 모터 드라이브 시스템 개발)

  • Cha, Hyun-Rok;Lee, Sung-Ho;Kim, Kyung-Su;Lee, Kyu-Seok;Jun, Seong-Kyu;Song, Doo-Yong
    • Proceedings of the KIEE Conference
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    • 2008.07a
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    • pp.1193-1194
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    • 2008
  • 본 논문은 주거환경 변화 및 공기 중 부유물질로 인한 피해를 보호하기 위해 제정된 공기질 관리법안에 적합한 대기 환경 조건을 구현하기 위한 고정압 환풍기용 모터 및 제어 알고리즘에 관한 논문이다. 외기에 압력이 변화하는 외란에도 일정한 풍량을 낼 수 있도록 하기 위해서 속도와 전류의 두 물리량을 곱의 형태로 취하여 profile을 만들고 이에 추종하는 방식을 본 논문에서 제안하였다. 제품의 상용화를 위해서 풍량센서가 없는 센서리스 방식을 구현하기 위해서 전류 값을 토대로 압력 변화량을 일정하게 제어하는 방식을 취하였다. 고정압제어를 위해서 Open-loop상태에서 모터의 P-Q(압력-풍량)data를 측정하고 이를 기초로 예상 구동 영역을 유추하고 이를 토대로 Profile을 만들고 이 Profile을 추종하는 제어를 통해서 고정압제어를 실현하였다. Reference로 속도를 기준으로 하였으며, 동일 속도에서 전류의 값을 비교하여 제어하고자 하는 전류 값이 되도록 함으로써 정압을 실현하였다.

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Shear Behavior of Sands Depending on Shear Box Type in Direct Shear Test (직접전단실험시 전단상자의 종류에 따른 모래시료의 전단거동)

  • Hong, Young-Ho;Byun, Yong-Hoon;Chae, Jong-Gil;Lee, Jong-Sub
    • Journal of the Korean Geotechnical Society
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    • v.31 no.3
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    • pp.51-62
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    • 2015
  • Shear behavior obtained by direct shear tests is dependent on shear box and boundary condition. The objective of this study is to analyze problems of conventional direct shear test (type-A) and provide the reliable results by developing type-C direct shear apparatus. Experimental tests are carried out for Ulleung sand by using type-A and -C direct shear devices. The soil specimens, which are prepared at the relative density of 60%, and are applied to vertical confining stresses of 50, 100, 200, 300, and 400 kPa, are sheared at a constant shear strain rate of 0.5 mm/min. By comparing the results obtained by type-A and -C direct shear apparatus under constant normal load (CNL) condition, the performance of new one is verified. In addition, two constrained conditions including constant normal load (CNL) and constant pressure (CP) are applied to type-C one. Experimental results show that type-A direct shear apparatus has some problems such as rotating of loading plate and upper shear box, and the frictional forces between soil and inner wall of upper shear box. Thus, the shear strengths obtained by type-A device are overestimated or underestimated depending on shear box and boundary condition. On the other hand, type-C device produces clear and consistent test results regardless of constrained conditions. This study represents that type-C direct shear apparatus not only can solve the problems of type-A direct shear apparatus but provide the reliable results.

Numerical Study on the Hydrodynamic Performance Prediction of a Turbopump Inducer (인듀서 성능예측에 대한 수치해석적 연구)

  • Choi, Chang-Ho;Hong, Soon-Sam;Kim, Jin-Han
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.6
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    • pp.72-78
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    • 2003
  • In the present paper, computational studies on the hydrodynamic behavior of the inducer for the rocket-engine turbopump are presented including the effect of the mass flow rate. As the mass flow rate is increased, the inducer showed better performance with weak back flows which may have deleterious effects upon the anti-cavitation ability. But the adopted inducer showed low head rise with high volume flow rates, which may be caused by the small passage area near the trailing edge. The static pressure distributions at the shroud surface are compared with experimental results showing very good agreements except near the leading edge where strong back flows are present. The overall performance of the inducer such as, efficiency, head rise is also compared with experiments. The computational results are generally in good agreements with experimental ones near the design point, but two results show discrepancy at the high flow rate.

A Study on the Operational Optimization of Turbo-Expander Pressure Reduction System to the Natural Gas Flow Rates (천연가스 유량변화에 따른 터보팽창기 감압시스템 운전 최적화에 관한 연구)

  • Yoo, Han Bit;Kim, Hyo
    • Journal of the Korean Institute of Gas
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    • v.19 no.6
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    • pp.72-79
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    • 2015
  • Electricity can be generated when the natural gas passes through a turbo-expander pressure reduction system at natural gas pressure reduction stations. Efficiency of the turbo-expander depends on the ratio of the natural gas flow rates to the design flow rate of the turbo-expander. Therefore, the optimal conditions for the operation of the pressure reduction system can be determined by controlling the natural gas flow rates. In this study, we have calculated the electric energy generation depending on the natural gas flow rates at the two low-pressure reduction stations when the pressure of the natural gas is reduced from 17.5 bar to 8.5 bar and have found the optimal conditions for the turbo-expander pressure reduction system through the comparison with the calculation results. The turbo-expander generates the electric power efficiently for the high natural gas flow rates which variations are slight. The determined design flow rate of the turbo-expander has the highest coverage of the natural gas flow rates. The electricity generation is calculated as much as 9 MW(B station) and 12 MW(D station) at each pressure reduction station.

Feasibility Study of Pressure Letdown Energy Recovery from the Natural Gas Pressure Reduction Stations in South Korea (한국의 천연가스 도시정압기지에서 감압에너지 회수에 대한 타당성 연구)

  • Yoo, Han Bit;Hong, Seongho;Kim, Hyo
    • Journal of the Korean Institute of Gas
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    • v.19 no.3
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    • pp.9-17
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    • 2015
  • Almost all of the natural gas consumed in South Korea is compressed into very high pressure for the transportation through the underground pipelines, then reduced in pressure regulation stations before delivery to the consumer. For pressure reduction, expansion valves have been used due to the simple and effective installation, but recover none of the energy in the gas during compression. Hence, turbo-expanders are proposed instead of the valves to accomplish the same pressure letdown function and recover some of the compression energy in the form of shaft work converting into electric powers. Here we have theoretically calculated the electric powers at the pressure reduction from 68.7 bar to 23 bar (which are the average values taken at the inlet and outlet points of the expansion valve in medium-pressure regulation stations) according to the inlet conditions of temperature and flow rate. The natural gas is considered as two cases of a pure methane and the mixture of hydrocarbons with a very small amount of nitrogen, and the Peng-Robinson equation of state is employed for the calculation of required thermodynamic properties. The electric energy is recovered as much as 1596 MW(methane) and 1567 MW(mixture) based on the total supply of natural gas in 2013.

Prediction of Maximum Fly Ash Conveying Capacity of Fly Ash System in a Power Plant (발전 보일러용 비회 이송설비에서 최대 비회 이송량 예측)

  • Jin, Kyung-Yong;Moon, Yoon-Jae;Lee, Jae-Heon;Moon, Seung-Jae
    • Plant Journal
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    • v.11 no.1
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    • pp.50-57
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    • 2015
  • This study presents prediction of maximum fly ash conveying capacity of fly ash system in a power plant. The mixture ratio and pressure drop characteristics of air-fly ash flow in piping system are not well understood due to the complexity of particle motion mechanism. In this paper, the researcher investigated the optimum mixture ratio when the pressure drop of fly ash conveying system is equal to maximum static pressure of displacement fly ash transport blower and the capacity of fly ash transport according to the optimum mixture ratio by experimenting the fly ash conveying system of domestic D coal thermal power plants, which is currently in operation. The experiment results showed that the maximum fly ash conveying capacity of fly ash system were founded under the condition of maximum air volume 5,040 m3/h, static pressure of trip condition 1,163 mmH2O. In addition, it was predicted maximum mixture ratio of the air-fly ash was 8.66 and maximum capacity of fly ash conveying was 52,600 kg/h under these conditions.

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