• 한국음향학회:학술대회논문집
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• 한국음향학회 1994년도 FIFTH WESTERN PACIFIC REGIONAL ACOUSTICS CONFERENCE SEOUL KOREA
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• pp.662-667
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• 1994

This paper presents the design and construction details of a soundproof enclosure for housing 20 KVA diesel generator-set. As the generator had to be installed close to the hospital building, it was desirable to reduce the transmission of noise by housing the generator in such an enclosure. The diesel engine being an air cooled one, it was essential to supply fresh air into the enclosure for its cooling. Forced inflow of air is provided through an inlet duct located in such a way that the incoming fresh air is thrown close to the inlet of cooling fan of the engine. The high velocity air stream, which heats up while passing over the engine head, escapes to the atmosphere through a rectangular outlet duct with enlarges inlet that receives hot air from the engine. The air ducts were designed specially and have been provided with acoustic lining for sound absorption. The masonary enclosure has been provided with double glazed fixed windows and double doors. The exhaust pipe of the engine fitted with a muffler has been taken out through the enclosure wall facing away from the hospital. Acoustic performance studies conducted in terms of attenuation provided by the enclosure at different frequencies have also been presented and discussed. The noise control measures adopted for building the sound-proof enclosure have been found to be quite effective as the noise levels inside the hospital building are now within the acceptable limits.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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• pp.129-132
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• 2008

30톤급 액체로켓엔진 가스발생기의 연소 특성에 대한 연구를 수행하였다. 개발 초기 가스발생기는 터빈 매니폴드 출구를 모사하는 노즐을 후단에 장착한 상태에서 연소시험을 진행하였다. 이후 가스발생기와 터빈부의 공진모드를 모사하는 연장배관을 가스발생기와 노즐 사이에 추가하여 시험이 이루어졌으며, 최종적으로 터보펌프의 터빈부를 연결한 상태에서 연소시험을 수행하였다. 본 논문에서는 이와 관련된 온도 분포, 압력섭동 결과들을 분석하였다.

• 한국가스학회지
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• 제10권3호
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• pp.1-6
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• 2006

본 연구는 석탄을 가스화한 저발열량 합성가스 연료의 가스엔진과 소형가스발전기로의 적용가능성을 보여준다. 석탄을 가스화한 저발열량 합성가스를 가스엔진의 연료로 사용하기 위해 상용 LPG엔진을 부분적으로 변경하였다. 석탄가스화 연료에 적합한 연료공급시스템 -공기유량조절 오리피스, 가스믹서, 기화기, 예열히터, 레귤레이터, 연료탱크-이 집중적으로 변경되었다. 엔진 운전 결과에서 비록 석탄가스화 연료의 엔진 출력이 LPG연료에 비해 다소 떨어지지만 석탄가스화 연료를 사용하는 엔진이 공회전 조건에서부터 교축밸브를 완전 개방한 전부하조건까지 잘 운전됨을 보여주었다. 또한 본 연구에서 개발된 가스엔진발전기는 다양한 부하에서도 잘 작동됨을 보여주었다.

• 한국수소및신에너지학회논문집
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• 제27권1호
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• pp.114-120
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• 2016

This paper describes generating efficiency characteristics of the double acting Stirling engine/generator for domestic small-scale CHP (Combined Heat and Power) system. In small distributed generation applications, Stirling engine has competition from fuel cell, microturbine and etc. In order to be economical in the applications, a long life with minimum maintenance is generally required. Free piston Stirling engine (FPSE) has no crank and rotating parts to generate lateral forces and require lubrication. Double acting Stirling engine/generator has one displacer and two power piston which are supported by flexure springs. Two power pistons oscillate with symmetric displacement and are connected with moving magnet type linear generators for power generation from PV work. In experiments, 1 kW class double acting free piston Stirling engine/generator is fabricated and tested. Heat is supplied to hot end of engine by the combustion of natural gas and converted to electric power by linear generators which are assembled with power pistons. The electric parameters such as voltage, current and phase are measured with for variable flow rate of fuel gas. Especially, generating efficiency of FPSE is measured with three different measurement methods. Generating efficiency of the double acting Stirling engine/alternator is about 24%.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 하계종합학술대회 논문집 V
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• pp.2769-2772
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• 2003

This paper presents results of the development of the Turbo-generator system with structure which is HSG(High Speed Generator) installed to high speed gas-turbine engine directly. Turbo-generator with high speed motor-generator directly has many advantages aspects of weight, size, lubrication system and complexity of the system compared of conventional turbo-generator system with gear-box. But because of direct high speed operation of the high speed generator, we have to need stable high speed motor driving algorithm for perfect engine ignition when gas turbine starting. Also we have to need design of the PCU(Power Conditioning Unit) for converting high speed AC output power to conventional AC power or needed DC power.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.648-655
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• 2005

The resilient mounts of a diesel engine installed onboard a ship should be designed for both static and dynamic loads. If possible, the resonance frequencies of the six rigid body modes of the installation and the flexible modes of the engine support structure should not lie within the engine operation range. In this paper a design criterion is proposed to evaluate an isolation system which involves the summation of dynamic forces transmitted through the resilient mounts and elastic potential energy index stored in the mounts. A case study is also presented in which a diesel engine generator, which had an elastic foundation and was mounted in a 5500 TEU container vessel, was studied both theoretically and experimentally. The theoretical analysis of the test model was performed by using a single mass 6 degree of freedom system. Actual measurements of mechanical vibration of the Engine and its foundation onboard were carried out, which showed the importance of including the flexibility of the engine support structure in the mode

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.191-195
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• 2006

우주 발사체의 성공적인 비행을 위해서는 로켓 엔진의 성능 분산 관리가 필수적이다. 양산되는 엔진의 성능편차를 정량적으로 예측하기 위한 해석을 수행하고 성능영향계수를 이용하여 보정에 필요한 차압을 산출하였다. 별도의 추력제어 시스템을 갖추지 않은 엔진의 진공 추력 분산은 +9.1%, -8.7%로 나타났으며 엔진 혼합비 오차는 +9.7%, -9.6%에 달했다. 보정에 필요한 요구차압은 동일한 혼합비 보정에 대해 연소기 배관 산화제 측에서 더 작게 나타났으나 가스발생기 배관의 요구차압은 더 크게 요구된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.135-138
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• 2006

가스발생기 사이클 엔진시스템 설계를 입력값과 기본 요구값으로 나누어 설계 요구값을 만족하기 위한 설계변수 11개를 정의하였다. 이 11가지의 설계변수를 통하여 설계 요구값을 만족하기 위한 압력 유량 파워 균형 관계식 11개를 제시하였으며, Newton 방법을 이용하여 해를 찾는 프로그램을 제작하였다. 고안된 프로그램을 이용하여 가스발생기 사이클 엔진의 시스템설계를 수행하여 그 유효성을 입증하였다.

• 한국추진공학회지
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• 제12권5호
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• pp.18-25
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• 2008

가스발생기 사이클 액체로켓엔진의 성능 해석 프로그램을 개발하였다. 본 프로그램은 구성품의 성능으로부터 시스템의 성능을 예측하는 기능을 가지며 구성품 성능은 별도의 해석이나 실험에 의한 성능결과에 근거한 모델로 평가한다. 프로그램은 기존의 개념설계 연구와 비교하여 검증하였다. 서브시스템의 성능 모델은 MC-1 엔진 설계 및 10톤 추력 엔진에 대한 시스템 해석 결과와 비교하여 적절한 결과를 주는 것으로 확인하였다. 적용 예로서 LOx/Jet-A1을 사용한 30톤급 엔진의 성능을 제시하였다.

• 한국소음진동공학회논문집
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• 제16권4호
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• pp.329-338
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• 2006

The resilient mounts of a diesel engine installed onboard a ship should be designed for both static and dynamic loads. If possible, the resonance frequencies of the six rigid body modes of the installation and the flexible modes of the engine support structure should not lie within the engine operation range. In this paper a design criterion is proposed to evaluate an isolation system which involves the summation of dynamic forces transmitted through the resilient mounts and elastic potential energy index stored in the mounts. A case study is also presented in which a diesel engine generator, which had an elastic foundation and was mounted in a 5500 TEU container vessel, was studied both theoretically and experimentally. The theoretical analysis of the test model was performed by using a single mass 6 degree of freedom system. Actual measurements of mechanical vibration of the engine and its foundation onboard were carried out, which showed the importance of including the flexibility of the engine support structure in the mode.