• Title/Summary/Keyword: 터보팽창기

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An Optimization Study on the NGL Recovery Process Using Turbo-expander (터보 팽창기를 활용한 NGL 회수공정 최적화에 대한 연구)

  • Kim, Yu-Mi;Cho, Jung-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.12 no.3
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    • pp.1473-1478
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    • 2011
  • In this study, simulation and optimization works for a demethanizer column have been performed to obtain ethane and heavier products from a pretreated natural gas stream. Pretreated natural gas feed stream is partially condensed after being precooled by exchanging heat with demethanizer top vapor stream and by using an external refrigeration cycle with a propane refrigerant. Vapor stream is furtherly cooled and partially condensed through a turbo-expander and the power generated from the expansion of turbo-expander was delivered to the compressor for the residue gas compression. Liquid stream is being cooled by Joule-Thomson expansion valve and is fed to the middle section of the demethanizer. Ethane recovery percent for feed natural gas was set to 75% and methane to ethane molar ratio was fixed as 0.015. Propane refrigeration heat duty was reduced by splitting the feed stream and to exchange heat with side reboiler.

A Study on the Minimization of the Refrigeration Power Consumptions Through the Determination of Demethanizer Top Pressure in the NGL Recovery Process Using Turbo-expander (터보 팽창기를 활용한 NGL 회수공정에서 최적의 탈메탄탑의 운전압력 결정을 통한 냉동 소요동력 최소화에 대한 연구)

  • Kim, Yu-Mi;Cho, Jung-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.12 no.2
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    • pp.1032-1037
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    • 2011
  • In this study, simulation and optimization works for a demethanizer column have been performed to obtain ethane and heavier products from a pretreated natural gas stream. Pretreated natural gas feed stream was partially condensed after being precooled by exchanging heat with demethanizer top vapor stream and by using an external refrigeration cycle with a propane refrigerant. Vapor stream was cooled further and partially condensed through a turbo-expander. The power generated from the expansion of turbo-expander was delivered to the compressor for the residue gas compression. Liquid stream was cooled by Joule-Thomson expansion valve and was fed to the middle section of the demethanizer. Recovery percent of ethane for feed natural was set to 80% and methane to ethane molar ratio was fixed as 0.0119. On the other hand, some of the cold heat could be recovered by splitting the feed stream and by exchanging heat with side reboiler in order to reduce the heat duty in the propane refrigeration cycle.

Development of Turbo Expanders with Hydrostatic Bearings for Hydrogen Liquefaction Plants (정압 베어링을 적용한 수소 액화 공정용 터보 팽창기 개발)

  • Lee, Donghyun;Kim, Byungock;Park, Mooryong;Lim, Hyungsoo
    • Tribology and Lubricants
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    • v.37 no.3
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    • pp.91-98
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    • 2021
  • This paper presents a hydrostatic bearing design and rotordynamic analysis of a turbo expander for a hydrogen liquefaction plant. Th~e turbo expander includes the turbine and compressor wheel assembled to a shaft supported by two hydrostatic radial and thrust bearings. The rated speed is 75,000 rpm and the rated power is 6 kW. For the bearing operation, we use pressurized air at 8.5 bar as the lubricant that is supplied to the bearing through the orifice restrictor. We calculate the bearing stiffness and flow rate for various gauge pressure ratios and select the orifice diameter providing the maximum bearing stiffness. Additionally, we conduct a rotordynamic analysis based on the calculated bearing stiffness and damping considering design parameters of the turbo expander. The predicted Cambell diagram indicates that there are two critical speeds under the rated speed and there exists a sufficient separation margin for the rated speed. In addition, the predicted rotor vibration is under 1 ㎛ at the rated speed. We conduct the operating test of the turbo expander in the test rig. For the operation, we supply pressurized air to the turbine and monitor the shaft vibration during the test. The test results show that there are two critical speeds under the rated speed, and the shaft vibration is controlled under 2.5 ㎛.

Technical trend of supercharger for automobile (자동차용 기계구동 과급기의 기술동향)

  • 오박균;김향우;박동규
    • Journal of the korean Society of Automotive Engineers
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    • v.15 no.2
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    • pp.11-22
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    • 1993
  • 오늘날 자동차용 엔진에 대한 사용자의 요구는 여러가지가 있지만 그 중에서도 손쉬운 운전, 고 출력화, 응답(response)의 향상 등의 요구는 지금 이후로도 계속되리라 생각된다. 슈퍼차저도 이러한 요구에 의하여 사용되고 있으며 이제는 엔진의 보조적 향상책으로 뿐만 아니라 엔진에 있어서 필요 불가결한 것으로써 확실히 정착되리라 생각된다. 본 고에서 살펴본 바에 의하면 스크류식 슈퍼차저가 테스트된 4종류의 슈퍼차저중에서 가장 나은 성능, 과급압, 토르크를 주고 있으며, 또한 가장 소형이며 경량이다. 또한 스크류로타는 팽창기로써 효율 높게 작용할 수 있어, 이의 채용으로 기존의 터보콤파운드시스템 보다 8-10% 에너지 효율이 높게됨이 알려지고 있다. 그러므로 스크류로타를 이용한 터보콤파운드시스템은 기존의 어떤 시스템보다도 효율이 높은 시스템으로 발전할 수 있는 가능성이 높아 이의 연구가 적극 추진되어야 하겠다.

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Turbine Efficiency Analysis of Steady Flow in a Twin Scroll Turbocharger (트윈 스크롤 터보과급기에서 정상유동의 터빈 효율 분석)

  • Chung, Jin-Eun;Jeon, Se-Hun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.11
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    • pp.765-770
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    • 2020
  • The turbochargers used widely in diesel and gasoline engines are effective devices to reduce fuel consumption and emissions. In this study, the isentropic turbine efficiency of the steady flow in a twin-scroll turbocharger for the passenger vehicle gasoline engine was analyzed. The cold gas test bench was designed and made. The pressure and temperature of the inlet and exit of the turbine were measured at 60,000, 70,000, 90,000, and 100,000rpm under the steady-state flow. The isentropic turbine efficiency was calculated. The efficiency was the range of 0.53 to 0.57. The BSR and expansion ratio were changed from 0.71 to 0.84 and from 1.24 to 1.72, respectively. The isentropic turbine efficiency decreased with increasing BSR and expansion ratio. The operation of only scroll A or B was compared with that of the twin-scroll turbine. The isentropic efficiency of using only scroll B was higher than those of only scroll A at 60,000rpm. The isentropic efficiency of using only scroll A was higher than those of only scroll B at 100,000rpm. Therefore, the twin-scroll turbine used in this study is operating effectively in the wide speed range.

Thermodynamic Analysis on the Feasibility of Turbo Expander Power Generation Using Natural Gas Waste Pressure (천연가스 폐압발전 활성화의 당위성에 대한 열역학적 분석)

  • Ha, Jong Man;Hong, Seongho;Kim, Kyung Chun
    • Journal of the Korean Institute of Gas
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    • v.16 no.6
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    • pp.136-142
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    • 2012
  • Thermodynamic equations for the electric power and temperature in a turbo expander generator (TEG) using pressure energy in a natural gas line are derived. From the equations, it was shown that dominant factor is not the pressure difference but the pressure ratio. The high energy level in the inlet of TEG can be made from nearly no expense of electric energy input, which means TEG can be treated as one of newly available clean energy source. If a post heating method is chosen to heat up expanded natural gas, the usage of cold energy is possible without a refrigeration cycle. The combined TEG and refrigeration system enhances economic benefit much more.

Design and Analysis of Cryogenic Turbo Expander for HTS Power Cable Refrigeration System (초전도 전력 케이블 냉각 시스템 적용을 위한 극저온 터보 팽창기 설계 및 해석)

  • Lee, Changhyeong;Kim, Dongmin;Yang, Hyeongseok;Kim, Seokho
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.14 no.3
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    • pp.141-148
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    • 2015
  • The cryogenic cooling system should maintain the HTS power cable below 77 K. As the length of HTS power cables has increased, there have been many efforts to develop large capacity cryocoolers. Brayton, Joule-Thomson, and Claude refrigerators were considered for the large capacity cryocooler. Among the various cryocoolers, the Brayton refrigerator is the most competitive in terms of the HTS power cable. At present, it is thought that a 10-kW class refrigerator will be able to be used as a unit cooling system for the commercialization of HTS power cables in the near future. The Brayton refrigerator is composed of recuperative heat exchangers, a compressor, and a cryogenic turbo expander. Among the various components, the cryogenic turbo expander is the part that decreases the temperature, and it is the most significant component that is closely related with overall system efficiency. It rotates at high speed using high-pressure helium or neon gas at cryogenic temperatures. This paper describes the design of a 300-W class Brayton refrigeration cycle and the cryogenic turbo expander as a downscale model for the practical 10-kW class cycle. Flow and structural analyses are performed on the rotating impeller and nozzle to verify the efficiency and the design performance.

Design of a Cryogenic Turbo Expander Drive Shaft for 300 W Class Brayton Refrigerators (300 W급 브레이튼 냉동기용 극저온 터보 팽창기 구동축 설계)

  • Kim, Manryeol;Lee, Changhyeong;Kim, Dongmin;Yang, Hyeongseok;Kim, Seokho
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.15 no.6
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    • pp.129-135
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    • 2016
  • There have been many types of development and commercialization efforts for superconducting power applications with the continuous development of High Temperature Superconducting (HTS) conductors. In particular, HTS power cables are going to be commercialized in real power grids. A cryogenic refrigeration system should be used to keep it below 77 K, and its required cooling capacity continuously increases as the unit length of the HTS power cable increases. Among the many kinds of cryogenic refrigerator, a reverse Brayton refrigerator that uses turbo expanders is a promising refrigerator due to its efficiency and reliability. Among the various components in refrigerators, the cryogenic turbo-expander is the most important part for increasing efficiency and assuring reliability. The design of a 300 W class turbo-expander is described in this paper prior to the development of a 10 kW class turbo expander, which is the required capability for the commercialization of a HTS power cable. The impeller shape and rotation speed are determined based on the cycle analysis. The Eigen frequency and harmonic analysis are conducted with gas bearings at cryogenic temperatures to determine the operational stability.

Mass Flow Rate Measurement of Pulsating Flow in a Twin-Scroll Turbocharger (트윈스크롤 터보과급기에서 맥동유동의 질량유량 측정)

  • Chung, Jin-Eun;Jeon, Se-Hun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.12
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    • pp.723-729
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    • 2019
  • Turbochargers are an effective device to reduce the fuel consumption. In this study, the mass flow rate of pulsating flow in the twin-scroll turbocharger for the gasoline engine of passenger vehicles was measured. Pulsating flow was achieved using a pulse generator and the mass flow rate of the unsteady pulsating flow was analyzed by comparing it with those of the steady flow. The pulse generator consisted of a rotating upper plate and a fixed lower plate. To measure the mass flow rate of unsteady flow, the orifice flow meter equipped with the difference pressure transducer was used. To analyze the low speed performance of the turbocharger, the measurement was carried out in the speed of turbocharger from 60,000rpm to 100,000rpm. The mass flow parameters of the unsteady pulsating flow showed a large difference compared to those of the steady flow. Those of the unsteady flow showed the hysteresis loop surrounding the mass flow parameters of the steady flow and the maximum variation of the mass flow parameters were 5.0 times those of the steady flow. This phenomenon is the result of the filling and emptying the turbine volute space due to pulsating flow.

Development of Static Seal for a Liquid Rocket Engine (액체 로켓 엔진 스태틱 실 개발)

  • Jeon, Seong Min;Yoon, Suk-Hwan;Chung, Taegeum
    • Journal of Aerospace System Engineering
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    • v.16 no.4
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    • pp.53-59
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    • 2022
  • Static seals are used to seal high temperature gas and cryogenic fluid under high pressure, at interfaces between liquid rocket engine components such as combustion chamber, turbopump, gas generator, valves, etc. As thermal expansion and contraction at assembly interfaces cause undesirable leakage under cryogenic and high temperature environments, static seals applied for sealing of joint interfaces without relative motion should be designed properly. The additional function of rotation at the sealing face is also required for static seals, when the spherical flange is used for improvement of assembly at misalignment interfaces. In this study, structural analysis and leak tightness test of simulating test rig for several important interfaces are performed, to verify structural integrity of static seals.