• 한국소음진동공학회논문집
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• 제27권2호
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• pp.204-212
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• 2017

The rotor dynamics and balancing technic for rotating equipment during engineering and manufacture stage are to be carefully considered in order to minimize the operation troubles regarding vibration during commissioning stage. In this paper, the test rig, which includes the disks as balancing plane, is designed and manufactured, so that the characteristic of rotor dynamics can be analyzed such as critical speed and mode shape. The critical speed predicted through natural frequency analysis is verified by the actual measurement on bearing housing vibration during start-up condition of test rig. The low speed balancing and the operating speed balancing test are performed respectively with consideration of first critical speed, and the residual unbalance amounts are estimated in accordance with the relevant method described in API standard. In addition, the single and dual plane balancing are carried out on main disk and trim disk depended on phase information at each balancing step.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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• pp.25.3-26
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• 2008

The direct way to the moon is to start from the parking orbit by using impulsive thruster In previous domestic research, the direct way has been studied by using a single impulsive shot. However, when a single impulsive shot occurs to go into a Translunar orbit, gravity losses occur because thruster is not impulsive shot but the finite burns and it causes the gravity losses. To make up for the weak point of a single impulsive shot, this paper divides TLI (Trans Lunar Injection) into several small burns. Therefore, departure loop trajectory and the Translunar trajectory. This method is useful not only to reduce the gravity losses but also to check the condition of satellite. By using this method, this paper demostrates the optimized trajectory from Earth parking orbit to lunar mission orbit which minimizes the fuel, and the SNOPT (Sparse Nonlinear OPTimizer software) is used to find optimal solution. Also, this paper provides lunar mission profile which includes the mission schedule when TLI, LOI (Lunar Orbit Insertion) maneuvers occur, a mount of fuel when thruster is used and other mission parameters.

• Asian Pacific Journal of Cancer Prevention
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• 제16권2호
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• pp.507-512
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• 2015

Background: This pilot study looked into the physical, social, psychological and economic issues of Indian adult cancer survivors. Materials and Methods: Assumed cancer free patients, after cancer directed therapy (CDT), were assessed on the basis of a questionnaire developed by the investigators. The mental status of the survivors was elicited by modified MINI international neuro-psychiatric interview. This cross sectional assessment was conducted as a direct interaction with each patient for 30 to 45 minutes at a cancer hospital in 2012. Results: Thirty one adult cancer survivors participated in this study. Median age was 53 years with a median follow up duration of 21.8 months (Range 2.3-194.1 months). The majority (68%) did not receive financial support for treatment. Median interval after CDT to start of activity of daily living was 1.5 months (range: 0-24 months). Fatigue and loss of appetite were reported by 52% and 29% respectively. The cancer diagnosis and its treatment adversely impacted the financial condition in 42% of patients. Nineteen percent each showed social anxiety and post-traumatic stress disorder and another 13% patients reported depression. Conclusions: This prospective assessment highlights survivorship issues and the need to address those issues particularly in the context of developing countries where resources and manpower are limited.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 춘계학술대회 논문집
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• pp.219-222
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• 2009

파이로스타터는 터보펌프 터빈의 초기 구동을 위해 터빈에 고압의 가스를 공급함으로써 액체추진기 관의 터보펌프 시동기 역할을 수행한다. 파이로스타터는 일종의 가스발생기로써, 내부에 충전된 저온고체추진제의 연소가스를 통해 시동에 필요한 에너지를 터빈에 공급하게 된다. 파이로스타터 내부에 충전되는 고체추진제의 외부와의 환경적인 격리뿐만 아니라, 연소 초기 연소실 내부의 충분한 압력 증가를 통해 저온 고체추진제의 점화특성을 향상시킬 수 있는 파이로스타터용 럽쳐디스크 개발을 위해 럽쳐디스크의 두께, 스코어의 깊이 및 형태, 가압 속도에 따른 파열압력과 파열반경 경향에 대한 시험을 수행하였으며, 설계파열압력 및 요구 파열반경 등 실제 운영 조건을 만족하는 파이로스타터용 럽쳐 디스크의 성능을 시험결과를 통해 확인하였다.

• 한국추진공학회지
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• 제15권1호
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• pp.35-44
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• 2011

액체로켓엔진 시스템의 시동 및 정지 또는 추력 제어와 같은 천이 작동 시 동특성을 예측하기 위한 선행 연구로서 추진제 공급 시스템의 구성품에 대한 동특성 모델링을 수행하였다. 연료 공급 계통과 산화제 공급 계통의 구성품들은 재생냉각채널을 제외하고 같은 것으로 가정하였다. 동특성 모델링의 대상 구성품은 펌프, 관로, 오리피스, 제어 밸브, 재생냉각채널, 인젝터 등이며 실제 엔진 시스템의 축소 모형에 대한 수류시험을 통해 각 구성품의 동특성 모델링을 검증하였다. 수치적인 방법을 바탕으로 구성품에 대한 동특성 모델링을 통합하였으며 축소 모형으로 연결된 수류시스템을 사용한 수류시험을 통해 통합 동특성 예측프로그램을 검증하였다.

• 한국소음진동공학회논문집
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• 제16권9호
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• pp.964-970
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• 2006

Micro gas turbine(MGT) has received attention recently as small-scale distributed power sources. With characteristics such as their small size, lightweight, low maintenance cost and minimal vibrations during operation, they are expected to become widespread in a wide range of ' applications, including residential and small-scale industrial use. It is very easier to start-up and stop the MGT system which is the friendly environmental power system has just below the 9ppm NOx emmission and good quality of noise level. The exhaust heat emitted by the MGT is in the form of about $300^{\circ}C$ clean exhaust gas. The exhaust gas is suitable for absorption chiller/heater system. 1 has researched performance characteristics of the 60 kW class MGT-absorption chiller-heater system in the local condition. Variations of heat recovery from exhaust gas has measured according to micro gas turbine output of 15, 30, 45, 60kW. From those results, the performance of the MGT-absorption chiller/heater system has been evaluated.

• 한국지열·수열에너지학회논문집
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• 제12권4호
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• pp.15-20
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• 2016

Even though the control device of the heating system works well, insufficient water flow rates can degrade control performance and thermal comfort. The water flow rate should be adjusted appropriately to cope with the heating load of each zone. In order to solve these problems, a new balancing concept 'dynamic balancing' was proposed where a balancing valve opening can be automatically modulated according to the heating condition of the room. This study analyzed the effects of dynamic balancing upon indoor thermal environment and energy consumption in a radiant floor heating system through field measurement. Under part-load conditions, the use of a dynamic balancing is a more effective method to reduce energy consumption and to prevent a cavitation. Dynamic balancing is able to help boost the temperature of a room in the start-up period.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.886-891
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• 2000

One of the domestic co-generation plants have undergone excessive vibration problems of turbine attributed to external force for years. The root cause of turbine vibration may be shan alignment problem which sometimes is changed by thermal expansion and external farce, even if turbine technicians perfectly performed it. To evaluate the alignment condition from plant start-up to full load, a strain measurement of turbine and main steam piping subjected to thermal loading is monitored by using strain gages. The strain gages are bonded on both bearing housing adjusting bolts and pipe stoppers which. installed in the x-direction of left-side main steam piping near the turbine inlet in order to monitor closely the effect of turbine under thermal deformation of turbine casing and main steam piping during plant full load. Also in situ load of constant support hangers in main steam piping system is measured by strain gages and its results are used to rebalance the hanger rod load. Consequently, the experimental stress analysis by using strain gages turns out to be very useful tool to diagnose the trouble and failures of not only to stationary components but to rotating machinery in power plants.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.331-334
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• 2010

두산중공업(주)에서 개발 중인 발전용 가스터빈 DGT-5 엔진의 작동 특성을 평가하였다. 다양한 연료 스케쥴과 여러 가지 조합의 bleed valve 개폐 제어에 대한 영향을 분석하기 위한 시험을 통해 시동 특성을 개선하였고, 시동부터 부하운전 전체 작동 영역에서 압축기에서의 불안정 현상 없이 엔진이 안정적으로 작동됨을 확인하였다. 순간적인 부하 변동과 load rejection에 대한 엔진의 동적 거동 분석을 통해 실제 계통 병입 조건에서 급격한 부하변동 시 엔진이 안정적으로 제어될 수 있음을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.339-342
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• 2010

두산중공업(주)은 개발 중인 5MW급 발전용 가스터빈의 작동 특성과 설계 인자들을 검증하기 위한 엔진 시험설비를 구축하였으며, 개발 엔진의 모든 성능 인자들을 안전하고 신뢰성 있게 평가하기 위해서 요구 조건을 충족시킬 수 있도록 엔진 테스트 셀을 설계하였다. 구축된 테스트 셀은 엔진의 시동에서 최대 출력조건까지 엔진의 전체 운전 상태를 효과적으로 재현할 수 있기 때문에 다양한 조건에서의 엔진시험 결과를 활용하여 지속적인 설계 개선을 위한 기반시설로 활용 가능하다. 더욱이 개발 엔진의 파생형 모델 개발과 상업모델 출고시험에 활용함으로써 엔진 제작사로서의 개발 경쟁력 제고에 기여할 수 있을 것으로 기대된다.