• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
• /
• pp.523-526
• /
• 2006

A series of hydraulic and cavitation tests are performed in water environment in order to verify the hydraulic and cavitation performance of three types of LOX pumps. All the performances of the pumps are found to be satisfied with each design requirement. In the hydraulic tests, the head and efficiency are increased as the gap between floating ring seals and the impeller shoulder is decreased. In the cavitation tests, some pumps show decrease in the cavitation performance as the flowrate of the pump is decreased.

• 대한기계학회논문집B
• /
• 제33권12호
• /
• pp.933-938
• /
• 2009

Hot test of a full-scale turbopump for a 30-ton-thrust liquid rocket engine was carried out. The turbopump is composed of an oxidizer pump, a fuel pump, and a turbine on a single shaft. Model fluid was used in the test, that is, hot air for the turbine and water for the pumps. The turbopump was operated stably at full speed for 120 seconds. In terms of performance characteristics of pumps and turbine, the results from the turbopump assembly test are compared with those from the turbopump component tests which were performed at about half of the design rotational speed.

• 대한기계학회논문집B
• /
• 제32권4호
• /
• pp.249-254
• /
• 2008

Hydrodynamic performance test of a turbopump for a liquid rocket engine is carried out. The turbopump is composed of an oxidizer pump, a fuel pump and a turbine, and the two pumps are driven by the turbine. In the test, water is used for the pumps as working media and air is used for the turbine. Performance parameters of pumps and a turbine are drawn, and a power balance between the pumps and the turbine are calculated. The calculation shows a good power balance, which implies that the pump component tests, the turbine component test and the assembly test are reliably performed. At the starting period of the test, pressure rise-flow rate curve of a pump gradually approaches the ideal curve which could be obtained by very slow starting.

• 한국유체기계학회 논문집
• /
• 제15권1호
• /
• pp.41-45
• /
• 2012

The effects of inducer tip clearance on the suction performance of a pump for turbopumps are investigated. Experiments for the pump with inducer tip clearances of 1.8% and 1.4% of blade height were performed. The experimental results showed that the suction performance of the pump increased as the tip clearance decreased. It seems that the suction performance of the pump becomes better with smaller tip clearances because the strength of the inducer backflow becomes weak with the decreased tip clearance.

• 한국유체기계학회 논문집
• /
• 제15권1호
• /
• pp.36-40
• /
• 2012

The magnitude of the axial thrust acting on pump bearings has a great influence on the operational reliability and service life of a pump for turbopumps. In the present study, radial vanes are introduced to the pump casing to control the axial thrust by changing the cavity pressure between the impeller and the casing. To investigate the effect of the vanes on the axial thrust of the pump, experimental and computational studies were performed with and without the vanes. It is shown that the vanes reduce the cavity pressure by preventing the flow from rotating with the impeller. Experimental and computational results show similar trend for the axial thrust difference between two cases with and without the vanes. The results show that the cavity vanes are very effective in controlling the magnitude of the axial thrust.

• 한국방송∙미디어공학회:학술대회논문집
• /
• 한국방송공학회 1998년도 학술대회
• /
• pp.161-164
• /
• 1998

본 논문은 이동성 추정기를 이용하여 수신체의 이동성 정도 또는 채널의 변화 정도를 추정해 냄으로써 채널 추정에 사용하는 OFDM 심볼의 개수를 결정하여 최적의 채널 추정을 수행하는 알고리즘을 제안하고, 성능 분석을 보여준다. OFDM 시스템의 채널 보상에 다수의 심볼을 사용하면 고정된 수신체에서 우수한 성능을 나타내지만 시간 변화적인 다중 경로환경에서는 오히려 출력 SNR 성능을 저하시킨다. 제안된 이동성 추정기를 이용한 채널 추정 알고리즘은 고정 수신체 및 고속의 이동체 뿐만 아니라 복잡하고 변화 무쌍한 다중 경로 페이딩 채널 환경에 강인한 특성을 나타낸다는 것을 전산 모의 실험을 통하여 확인하였다.

• 한국정보과학회:학술대회논문집
• /
• 한국정보과학회 2007년도 가을 학술발표논문집 Vol.34 No.2 (C)
• /
• pp.433-438
• /
• 2007

This paper presents a distance mapping-based localization method with incomplete data which means partially observed data. We make three contributions. First, we propose the use of Multi Dimensional Scaling (MDS) for multi-robot localization. Second, we formulate the problem to accomodate partial observations common in multi-robot settings. We solve the resulting optimization problem using #Scaling by Majorizing a Complicated function (SMACOF)#, a popular algorithm fur iterative MDS. Third, we not only verify the performance of MDS-based multi-robot localization by computer simulations, but also implement a real world localization of multi-robot team. Using extensive empirical results, we show that the accuracy of the proposed method is almost similar to that of Monte Carlo Localization(MCL).

• 항공우주기술
• /
• 제10권1호
• /
• pp.122-128
• /
• 2011

액체로켓엔진용 산화제펌프의 수류시험을 상온에서 실시하였다. 수력성능시험 결과, 펌프의 양정 계수는 회전수가 커질수록 약간 감소하였고, 효율은 회전수가 커질수록 증가하였다. 흡입성능시험 결과, 유량비 92% 이하의 낮은 유량비에서 흡입성능이 떨어지는 것으로 나타났다. 또한, 시험 중 측정한 고주파 신호를 이용하여 펌프의 진동 특성을 분석하였다.

• 한국방송∙미디어공학회:학술대회논문집
• /
• 한국방송공학회 2015년도 추계학술대회
• /
• pp.23-25
• /
• 2015

최근 디지털 방송의 새로운 서비스에 대한 소비자의 기대와 무선 통신 및 영상 압축 기술의 발전으로 인해 차세대 방송 기술에 대한 관심이 고조되고 있다. 미국 방송 표준화 기구인 ATSC에서는 차세대 국제 방송 표준을 위해 ATSC 3.0을 시작하였고, 고정 방송 및 이동 방송의 동시 서비스 제공을 목표로 하고 있다. TDM을 사용하여 두 방송 서비스를 제공하는 경우 ATSC 3.0 융합형 3DTV 서비스를 제공할 수 있으며, 모바일 방송의 파일럿 심볼을 이용한 채널 추정이 가능하므로 고정 방송만을 제공하는 경우보다 채널 등화 성능 측면에서 더 유리하다. 이에 본 논문에서는 ATSC 3.0 융합형 3DTV를 위한 채널 등화 시뮬레이터를 설계 및 구현하여 고정 방송 환경과 성능을 비교한다.

• 항공우주시스템공학회지
• /
• 제7권4호
• /
• pp.49-54
• /
• 2013

A turbopump for a 75 ton class liquid rocket engine was tested at full speed for 20 seconds using model fluid. Liquid nitrogen is used for the oxidizer pump, water for the fuel pump, and hot gas for the turbine. The non-cavitating head of pump from the turbopump assembly test showed a good agreement with that from the pump component test. The relative difference of turbine efficiency between the turbopump assembly test and the turbine component test was 0.3% only. Suction performance from the turbopump assembly test was higher than that of pump component test, which resulted from the thermodynamic effect of cavitation.