• Title/Summary/Keyword: 압축기 일

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Change in compressive strength of lightweight geopolymers after immersion (침지 후 경량 지오폴리머의 압축강도 변화)

  • Kim, Hakmin;Kim, Yootaek
    • Journal of the Korean Crystal Growth and Crystal Technology
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    • v.31 no.4
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    • pp.174-181
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    • 2021
  • Lightweight geopolymers were fabricated by using IGCC (integrated gasification combined cycle) slag and Si sludge which are classified as general wastes (recyclable resources). Three curing methods were tried to investigate the changes in compressive strength and density according to the curing method and immersion time. Immersion period was tried up to 21 days to observe long-term performance in water. Compressive strength of the specimens cured in oven decreased abruptly with an increase in immersion time. Compressive strength of the specimen cured in autoclave was low after 3 and 7 day immersion; however, increased rapidly after 21 day immersion. On the contrary, compressive strength of the specimen cured in autoclave and oven was high but substantially decreased after 21 day immersion. Conclusively, it was speculated that oven curing is effective for the compressive strength development at early age; however, autoclave curing is more desirable for the long-term performance in water.

A Study on Steady-State Performance Analysis and Dynamic Simulation for Medium Scale Civil Aircraft Turbofan Engine (I) (중형항공기용 터보팬엔진의 정상상태 성능해석 및 동적모사에 관한 연구 (I))

  • 공창덕;고광웅;기자영
    • Journal of the Korean Society of Propulsion Engineers
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    • v.2 no.2
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    • pp.47-55
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    • 1998
  • Steady-state and transient performance for the medium scale civil aircraft turbofan engine was analyzed. Steady-state performance was analyzed on maximum take-off condition, maximum climb condition, and cruise condition. At 90%RPM of the low pressure compressor, the partload performance was economized. The transient performance was analyzed with cases of the step increase, the ramp increase, the ramp decrease, and the step increase and ramp decrease for the input fuel flow. For the transient performance analysis, work matching between compressor and turbine was needed. Modified Euler method was used the integration of residual torque in work matching equation. At all flight condition, the overshoot of the high pressure turbine inlet temperature was appeared in the step and ramp increase case, and the surge of high pressure compressor was appeared in the step increase case and the ramp increase case within 5.5 seconds of maximum climb condition.

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Numerical Performance Analysis of the Swing Compressor (스윙 압축기의 수치해석적 성능평가)

  • Moon, Seok-Hwan;Noh, Ki-Youl;Sa, Bum-Dong;Yang, Jang-Sik;Choi, Gyung-Min;Kim, Duck-Jool
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.24 no.1
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    • pp.77-84
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    • 2012
  • Numerical performance analysis of the vane-roller integral type swing compressor was conducted. The swing compressor has been investigated for the highly efficient air conditioning system. Performance analysis results of the swing compressor were compared with those of a conventional rotary compressor. Mechanical and gas losses of a swing compressor were larger than those of a rotary compressor. However in case of mass flow rate from the discharge port, the swing compressor was about 6.68% higher than the rotary compressor. Hence the EER, the cooling capacity and the compressor work of the swing compressor were about 3.71%, 6.69% and 2.90% higher than the rotary compressor respectively.

Theoretical study on the performance improvement of refrigeration system installed with ejector entraining expansion gases after expansion process (이젝터를 적용한 팽창기체 흡입 냉동시스템의 성능향상 해석 연구)

  • Yun, Sangkook
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.7
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    • pp.828-833
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    • 2014
  • In this paper, the performance characteristics for newly developed ejector refrigeration system, which is that the part of saturated vapor from liquid-vapor separator after ejector expansion process is entrained in ejector, and the saturated liquid flows in the evaporator and compressed with the rest of vapor in separator, is studied. The reasons of the performance improvement of refrigeration system are that the refrigeration capacity is increased due to quality reduction after iso-entropic expansion process by ejector and the compression work is reduced because of the relatively high pressure of vapor refrigerant before compression process. The comparison results of the ejector system entraining expansion gases with the present residential freezer show that the COP increases to 27.8% maximum in case of the pressure drop to 65% of high pressure of freezer, and to 40.1% for 75% pressure drop of refrigerant R401A. The COP improvement rate with 20%~60% pressure lift in diffuser of ejector is only 2.6%~3%.

DME 분과 발표회-(DME 연료실증.시험연구 기술개발)

  • Korea LPGas Industry Association
    • LP가스
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    • v.20 no.2
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    • pp.59-67
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    • 2008
  • 지난 4월 2일 GAS KOREA 2008 전시회가 개최된 서울무역전시장에서 '한국DME협회 분과발표회'가 열렸다. 이날 분과발표회에서는 'DME Demo 플랜트 현황소개(한국가스공사 연구 개발원 조원준 박사 "DME 연료실증, 시험연구 사업현황(한국가스공사 연구개발원 백영순 박사)" 커먼레일형 연료공급계를 탑재한 2리터급 DME 차량개발(자동차 부품연구원 정재우 박사) "급속압축장치를 이용한 불균일 예혼합기의 DME HCCI연소 과정에 관한 연구(울산대학교 임옥택 교수) DME의 자착화 측정 및 세탄가의 추정(인하대학교 이대엽교수)" 직접분사식 압축착화기관에서 DME연료의 분무미립화 및 배출물 특성(한양대학교 이창식 교수)' 에 대한 발표도 이뤄졌다.

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A Dynamic Simulation for Small Turbushaft Engine with Free Power Turbine Using the CMF Method (CMF 기법을 이용한 소형 분리축 방식 터보축 엔진의 동적모사)

  • 공창덕;기자영;고광웅
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.04a
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    • pp.11-11
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    • 1998
  • 다목적으로 활용할 수 있는 터보축 엔진의 개발을 위한 정상상태 및 동적모사 프로그램을 개발하였다. 개발비, 개발시간, 개발위험도의 절감을 위해 가스발생기 부분은 성능이 잘 알려진 기존의 터보제트 엔진을 활용하였으며 약 3000hr 이상의 수명을 확보하기 위해 터빈재질을 교체하고, Larson-Miller 곡선을 이용하여 최대회전속도와 최대 터빈 입구온도를 각각 35000 RPM과 1140 K의 결정하였다 추가되는 동력터빈의 구성품 성능선도는 압축기 터빈 성능선도를 축척하여 사용하였다. 정상상태 성능해석에는 유량 및 일평형 방정식을 이용하였으며, 동력터빈이 각각 73%, 80%, 90%, 100% RPM일 때 가스발생기를 75%(24500 RPM)에서 100%(35000 RPM)까지 5% 간격으로 나누어 계산을 수행하였다.

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Effects of Stator Shroud Injection on the Aerodynamic Performance of a Single-Stage Transonic Axial Compressor (정익 슈라우드 공기분사가 단단 천음속 축류압축기의 공력성능에 미치는 영향)

  • Dinh, Cong-Truong;Ma, Sang-Bum;Kim, Kwang Yong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.1
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    • pp.9-19
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    • 2017
  • In this study, stator shroud injection in a single-stage transonic axial compressor is proposed. A parametric study of the effect of stator shroud injection on aerodynamic performances was conducted using the three-dimensional Reynolds-averaged Navier-Stokes equations. The curvature, length, width, and circumferential angle of the stator shroud injector and the air injection mass flow rate were selected as the test parameters. The results of the parametric study show that the aerodynamic performances of the single-stage transonic axial compressor were improved by stator shroud injection. The aerodynamic performances were the most sensitive to the injection mass flow rate. Further, the total pressure ratio and adiabatic efficiency were the maximum when the ratio of circumferential angle was 10%.

Investigation of Transient Performance of An Auxiliary Power Unit Microturbine Engine (보조동력용 마이크로터빈 엔진에 대한 과도성능 해석)

  • Son, Ho-Jae;Kim, Soo-Yong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.3
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    • pp.20-28
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    • 2007
  • The easiest way to see the phenomena of compressor surge is to show the static and dynamic operation characteristic on the map. Its operation zone will be restricted by the surge limit and, static and transient process must have some margin for it. Effect of rotor moment of inertia, air/gas volumes and heat transfer are factors to cause the transition from the static line. In case a large volume such as heat exchanger exists in the system it will exert a substantial influence to dynamic characteristics. In the present paper, influence of air volume bled from the compressor exit on transient process is investigated with an example of an auxiliary power unit micro-turbine engine. Turbine mass, pressure ratio, rotation speed, power and moment are calculated based on mass and work conservation. Result from the present study can give guidance to design the control system. A computer program is developed to calculate the dynamic process using the MathCAD commercial software.

전기안전사고사례 - 발전기 교체 작업중 메탄가스 폭발로 1명 사망, 6명 부상한 사고 발생

  • Ryu, Bo-Hyeok
    • Electric Engineers Magazine
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    • s.358
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    • pp.44-45
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    • 2012
  • 2012년 03월 16일(금) 11:05경, 경기도 고양시 소재 ${\bigcirc}{\bigcirc}$물재생센터의 발전기(3기)를 교체하기 위하여 발전기 및 관련 설비를 해체하는 과정에서 가스 압축기실 내에 있던 누출된 메탄가스가 배관 등의 용단작업 중에 발생된 불꽃에 의해 점화 폭발로 1명 사망, 6명이 부상당한 재해임.

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Performance Analysis of Freezing Desalination System using Seawater Heat Pump (해수 히트펌프를 이용한 냉동법 담수화시스템 개념설계)

  • Lee, Ho-Saeng;Lee, Seung-Won;Yoon, Jung-In;Kim, Hyeon-Ju
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.4
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    • pp.373-378
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    • 2011
  • The freeze desalination cycle with seawater heat pump system is simulated and designed for the basic data for the design of freeze desalination system. The basic model of seawater heat pump system is refrigeration cycle and indirect freeze desalination method is used for seawater desalination. The cycle performance of seawater heat pump such as COP, compressor work, condensing capacity was analyzed and the desalination performance such as fresh water productivity and energy per unit fresh water productivity was compared with respect to the seawater temperature of condenser inlet and ice ratio in the evaporator. The compressor work and condensing capacity decreased with respect to the decrease of seawater inlet temperature. The energy per unit fresh water productivity in case of $8^{\circ}C$ seawater inlet temperature showed 28.9% lower than that of $20^{\circ}C$.