• 제목/요약/키워드: Small test chamber

검색결과 150건 처리시간 0.032초

핀틀 형상 및 위치에 따른 추력 성능 (Thrust performance at the various pintle shapes and positions)

  • 김중근;이지형;장홍빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제31회 추계학술대회논문집
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    • pp.89-93
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    • 2008
  • 핀틀 형상과 위치가 고체 추진기관의 추력 성능에 미치는 영향을 공압 시험과 수치해석 기법으로 평가하였다. Fluent 해석 결과, Spalart-Allmaras 모델이 공압 시험에 얻은 노즐벽면 압력을 잘 모사하는 것으로 나타났다. 핀틀로 노즐목 크기를 감소시키면 추력은 증가하였으며, 핀틀 직경이 커질수록 핀틀 팁에 나타나는 재순환 영역의 압력에 의한 추력은 증가하지만 노즐 및 연소실 압력에 의한 추력은 감소하여 총 추력은 핀틀 직경이 작은 것 보다 감소하였다.

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재활용재료를 이용한 지하매설물용 뒤채움재 - 모형챔버실험 및 유한요소해석 (Backfill Materials for Underground Facility with Recycling Materials - Small-Scaled Laboratory Chamber Test and FEM Analysis)

  • 이관호;이경중
    • 한국방재학회 논문집
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    • 제11권3호
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    • pp.97-103
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    • 2011
  • 본 연구에서는 현장발생토사, 정수장슬러지 및 폐타이어분말 등 재활용 재료를 이용한 유동성 뒤채움재의 현장적용성 평가를 위해 실내모형실험 및 유한요소해석을 수행하였다. 실내모형실험은 교통하중을 모사한 정하중을 이용하였고, 현장에서의 시공과정을 고려하여 터파기, 베딩재시공 및 관부설, 유동성뒤채움재 타설 및 양생, 교통하중재하 순으로 평가하였다. 모형실험에는 관의 내공변위측정계, 토압계, 변형률게이지, LFWD등이 적용되었다. 유동성뒤채움재를 타설하는 시공과정중 관에서 발생한 최대 수직 및 수평변위는 0.83% 및 1.09%로 측정되었다. 양생 후 교통하중 재하시 최대수직 및 수평변위는 2.54 mm 및 3.15 mm이다. 하중제거시 회복되는 수직 및 수평 변형량은 0.603 mm 및 0.676 mm이다. 측정된 수평 및 수직토압으로부터 토압경감효과가 큼을 알 수 있었다. 모형실험에 이용된 재료물성을 이용하여 유한요소해석을 수행하였다. 유한요소해석을 통해 다양한 유동성뒤채움재 시공시 PVC관에서 발생하는 변위, 토압, 변형률 등을 평가하였다.

Designing Passive-Type Radar Reflector for Small Ship

  • Yim, Jeong-Bin;Kim, Woo-Suk;Ahn, Yoeng-Sub;Park, Sung-Hyeon;Jung, Jung-Sik;Lee, Kyu-Dong
    • 해양환경안전학회:학술대회논문집
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    • 해양환경안전학회 2003년도 춘계학술발표회
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    • pp.125-134
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    • 2003
  • 이 논문에서는 새로 개정된 2000 SOLAS 규정에 근거하여 소형선박용 수동식 레이더 리프렉터(PRR-S) 설계에 관해서 기술했다. 이 연구의 설계개념은 PRR-S이 선박요동에 의해서 레이더 반사면적(RCS)이 변동하는 것을 방지하기 위하여 ‘catch rain’ 위치를 유지하도록 한 것이다. PRR-S은 원형판으로 구성한 옥타헤더럴 레이더 리프렉터와 요동방지를 위한 짐발장치로 구성하였다. 설계한 PRR-S는 전파흡수실에서 성능실험을 하였다. 실험결과, 기준으로 정한 Davis Echomaster사의 리프렉터 보다 설계한 PRR-S이 높은 RCS를 나타냈다.

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산사태 모형실험에서의 Scale Effect에 관한 연구 (A Study on The Scale Effect of Landslide Model Tests)

  • 정지수;지영환;김유태;이승호
    • 한국지반환경공학회 논문집
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    • 제12권8호
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    • pp.5-12
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    • 2011
  • 본 연구는 강우로 인한 산사태 발생 시 강우강도, 강우지속시간, 비탈면 경사, 지반조건등에 따른 파괴 원인을 분석하여 산사태를 사전에 예측하기 위해 산사태 붕괴특성을 알아보고자 인공강우장치를 이용한 실제사면 크기에 근접한 대대형모형토조와 소형모형토조로 실험을 실시하였다. 육안상의 붕괴 형태 및 간극수압, 토압, 함수비, 지중변위 등의 계측결과에 대한 비교연구를 통해 모형토조연구에 있어 크기에 따른 산사태 메커니즘 분석과 소형모형토조 실험에 대한 산사태 모형실험으로서의 검증 실험을 수행하였다.

Dry-Air 중의 동일 연면거리를 가진 고체절연물의 형상 변화에 따른 수직연면방전 특성 연구 (A Study Vertical Surface Discharge Characteristics of the Shape Change of the Solid Insulation with the Same Creepage Distance of Dry-Air)

  • 전종철;최병주;배성우;이광식;박원주
    • 조명전기설비학회논문지
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    • 제30권1호
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    • pp.72-78
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    • 2016
  • In terms of power components which use environmentally-friendly dry air that can substitute SF6, there have been studies on the electrical properties of the solid insulation "spacer" for the purpose of securing dielectric strength as they become smaller. This study laminated solid insulation to keep the creeping distance the same in the dry air and investigated vertical surface discharge characteristics by shape. The three sheets of disk-type solid insulation(Bakelite) were laminated in a manner to keep the creeping distance the same. The lamination was categorized as follows: "Type A" in which the insulations with the same disk diameter were laminated; "Type B" in which the insulations whose middle disk diameter was large were laminated; and "Type C" in which the ones whose middle disk diameter was small were laminated. For a vertical surface discharge experiment, dry air was injected into the test chamber depending on the shape of the laminated solid insulation, and chamber pressure was adjusted in a range of 0.1-0.6MPa. As volume decreased, surface discharging voltage by unit volume increased. This was because of dielectric polarization according to the structural characteristics of the shape of lamination. The highest surface discharging voltage was found in "Type C."

마이크로웨이브 음극을 이용한 소형 인공위성의 홀 추력기용 음극전원 개발 (Cathode Power Development of Hall Thruster for Small Satellite using Microwave cathode)

  • 강석현;추원교;최준구;정연황;김연호;강성민;쿠니나카 히토시;차한주
    • 한국항공우주학회지
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    • 제42권11호
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    • pp.974-980
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    • 2014
  • 소형 인공위성에 적용하기 위해 홀 추력기의 음극 전원공급기가 개발되었다. 이 전기추력기에는 마이크로웨이브 음극을 적용하였고 음극전원은 안정적인 동작을 위해서 필수적이다. 유량을 조절함에 따라 양극전류는 변하게 되고 이때 음극전류는 양극전류에 비례하여 제어되어야 한다. 그래서 양극전류에 비례하여 음극전류를 공급하도록 음극전원을 설계하였다. 또한 음극전원은 음극의 안정성을 위해 음극전류가 약 0.03A 이내에서 양극전류보다 더 흐르도록 세부 조정되었다. 음극전원에 대한 기능시험은 양극과 음극을 등가적인 부하로 구성하여 수행되었다. 안정적인 추력기 동작을 확인하기 위해서 진공 챔버에서 검증되었고 발사 이후에 우주환경에서도 정상적으로 동작하는 것을 확인하였다.

엔진 내구시험 시 실린더 보아의 마모에 관한 연구 (A Study on Cylinder Bore Wear during Engine Durability Test)

  • 전상명
    • Tribology and Lubricants
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    • 제22권3호
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    • pp.131-136
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    • 2006
  • Cylinder bore wear may not be a problem in most current automotive engines. However, a small change in cylinder bore diameter can significantly affect the lubrication characteristics and ring axial motion. This in turn can cause to change inter-ring pressure, blow-by and oil consumption in an engine. Therefore, by predicting the wear of piston ring face, ring groove and cylinder bore altogether, the changed ring end gap and the changed volume of gas reservoir can be calculated. Then the excessive oil consumption can be predicted. Being based on the calculation of gas flow amount by the theory of piston ring dynamics and gas flow, and the calculation of oil film thickness and friction force by the analysis of piston ring lubrication, the calculation theory of oil amount through top ring gap into combustion chamber will be set. This is estimated as engine oil consumption. Furthermore, the wear theories of ring, groove and cylinder bore are included. Then the each amount of wear is to be obtained. The changed oil consumption caused by the new end gap and the new volume of oil reservoir around second land, can be calculated at some engine running interval. Meanwhile, the wear amount and oil consumption occurred during engine durability cycle are compared with the calculated values. Next, the calculated amount of oil consumption and wear are compared with the guideline of each pare0s wear and oil consumption. So, the timing of part repair and engine life cycle can be predicted in advance without performing engine durability test. The wear data of cylinder bore diameter are obtained from three engines before and after engine durability test. The calculated wear data of cylinder bore diameter are turn out to be twice of the lower bound of averaged test values at TDC and the lower bound at BDC.

취성/연성 파괴에 대한 수명예측 모델 및 신뢰성 설계 (Development of Reliability Design Technique and Life Prediction Model for Electronic Components)

  • 김일호;이순복
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.1740-1743
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    • 2007
  • In this study, two types of fatigue tests were conducted. First, cyclic bending tests were performed using the micro-bending tester. A four-point bending test method was adopted, because it induces uniform stress fields within a loading span. Second, thermal fatigue tests were conducted using a pseudo power cycling machine which was newly developed for a realistic testing condition. The pseudo-power cycling method makes up for the weak points in a power cycling and a chamber cycling method. Two compositions of solder are tested in all test condition, one is lead-free solder (95.5Sn4.0Ag0.5Cu) and the other is eutectic lead-contained solder (63Sn37Pb). In the cyclic bending test, the solder that exhibits a good reliability can be reversed depending on the load conditions. The lead-contained solders have a longer fatigue life in the region where the applied load is high. On the contrary, the lead-free solder sustained more cyclic loads in the small load region. A similar trend was detected at the thermal cycling test. A three-dimensional finite element analysis model was constructed. A finite element analysis using ABAQUS was performed to extract the applied stress and strain in the solder joints. A constitutive model which includes both creep and plasticity was employed. Thermal fatigue was occurred due to the creep. And plastic deformation is main damage for bending failure. From the inelastic energy dissipation per cycle versus fatigue life curve, it can be found that the bending fatigue life is longer than the thermal fatigue life.

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수음실 잔향시간 변화에 따른 중량 충격음 레벨 특성 - 실험실 환경을 중심으로 - (Floor Impact Sound Pressure Level Characteristics by the Change of Reverberation Time in Mock-up Test Rooms)

  • 정정호;이병권;연준오;전진용
    • 한국소음진동공학회논문집
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    • 제24권4호
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    • pp.339-347
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    • 2014
  • Floor impact sound in high-rise apartment building became one of social problems. A lot of civil complaints on floor impact sound occur continuously and the number of disputes between neighbors in small and aged apartment buildings is increasing. Interests on heavy-weight impact sound pressure level measurement and evaluation method is increased. Previous study reported that heavy-weight impact sound level was changed by the sound field condition of receiving reverberation chamber. In this study, heavy-weight impact sound pressure level change by the receiving sound field condition was measured in standard test facility and mock-up test room. These two experimental conditions were designed to simulate averaged living room of common apartment units. By the change of sound absorption power in receiving room, heavy-weight impact sound pressure level in most of frequency bands were changed in standard test facility and mock-up room. Normalized maximum sound pressure level regulated in ISO 16032 showed wider range of heavy/soft impact sound pressure level. Heavy/soft impact sound pressure level change was became smaller by the application of standardized maximum sound pressure level and ISO/CD 10140-3 Amd 2 method. In the case of standardized maximum sound pressure level, absolute sound pressure level changed. From these results, receiving sound field correction method regulated in ISO/CD 10140-3 Amd 2 is needed for the precision measurement and evaluation of heavy-weight impact sound.

엔진 내구시험 시 링 외주면 및 그루브 마모에 관한 연구 (A Study on Ring Face and Groove Wear during Engine Durability Test)

  • 전상명
    • Tribology and Lubricants
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    • 제22권4호
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    • pp.211-217
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    • 2006
  • Ring and groove wear may not be a problem in most current automotive engines. However, a small change in ring face and groove geometry can significantly affect the lubrication characteristics and ring axial motion. This in turn can cause to change inter-ring pressure, blow-by and oil consumption in an engine. Therefore, by predicting the wear of piston ring face, ring groove and cylinder bore altogether, the changed ring end gap and the changed volume of gas reservoir can be calculated. Then the excessive oil consumption can be predicted. Being based on the calculation of gas flow amount by the theory of piston ring dynamics and gas flow, and the calculation of oil film thickness and friction force by the analysis of piston ring lubrication, the calculation theory of oil amount through top ring gap into combustion chamber will be set. This is estimated as engine oil consumption. Furthermore, the wear theories of ring, groove and cylinder bore are included. Then the each amount of wear is to be obtained. The changed oil consumption caused by the new end gap and the new volume of oil reservoir around second land, can be calculated at some engine running interval. Meanwhile, the wear amount and oil consumption occurred during engine durability cycle are compared with the calculated values. Next, the calculated amount of oil consumption and wear are compared with the guideline of each part's wear and oil consumption. So, the timing of part repair and engine life cycle can be predicted in advance without performing engine durability test. The wear data of rings and grooves are obtained from three engines before and after engine durability test. The calculated wear data of each part are turn out to be at the lower bound of aver-aged test values or a little below.