• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.04a
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• pp.276-281
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• 1995

마모씨일과 발란스디스크에서의 로마킨효과가 3600rpm에서 운전되는 14단 터빈펌프의 동특성에 미치는 영향을 고찰한 결과 다음과 같은 결론을 얻을 수 있었다. 1. 14단 터빈펌프 시제품 해석을 위한 유한요소 모델링 및 해석결과는 실험적 모드해석을 통하여 5% 이내의 오차로 검증되었다. 2. 마모링 및 밸런스 디스크의 로마킨효과를 고려하였을 때 시제품 펌프의 위험속도는 그렇지 않았을 때에 비하여 1차의 경우 약 50% 상승하나 고차의 경우는 그 영향이 미미하였다. 그런데 1차 위험속도가 운전속도와 밀접한 관련이 있으므로 설계시 로마킨효과는 반드시 고려되어야 한다. 3. 마모링 및 밸런스디스크의 설계변경에 의하여 시제품 펌프의 강성을 변화시킬 경우 위험속도가 크게 변화하는 것으로 나타났다. 이를 이용하면 펌프의 심각한 구조변경 없이도 씨일의 적절한 설계에 의하여 임펠러 깃등의 고조화성분을 포함한 유해한 진동을 회피하는 동특성 설계가 가능하다. 향후 계속 연구사업으로서 씨일의 동특성 해석코드 개발 및 Wet Test를 통하여 본 연구결과를 검증하고 그 결과를 다단 터빈 펌프의 동특성 설게에 적용하여 고압 다단 터빈 펌프의 독자적 개발에 활용코자 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.8
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• pp.77-84
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• 2003

Structural analyses of a turbine bladed-disk for a liquid rocket turbopump are peformed to investigate the safety level of strength and vibration at design point. Due to the high rotational speed of the turbopump, effects of centrifugal forces are carefully considered in the structural analysis. Thermal load caused by extreme temperature distribution is also considered as an external force applied to turbine bladed-disk. A three dimensional finite element method (FEM) is used for cyclic symmetry structural analyses with the MSC/NASTRAN DMAP Alter. Interblade phase angles are considered to investigate structural dynamic characteristics as a function of rotational speed. Through the numerical analysis, effects of centrifugal and thermal loads on the turbine bladed-disk are examined.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.219-222
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• 2009

Pyrostarters play a role as a turbopump starter in liquid propellant propulsion systems by supplying pressurized gas to power turbines for engine start. A rupture disk in pyrostarters, which is usually installed behind a nozzle throat, not only isolates the charged solid propellants from the external environment but also improves the ignitability of the solid propellants by increasing a chamber pressure at the beginning of combustion. Experimental tests have been performed to study the effects of rupture disk thickness, depth and shape of scores, and pressure build-up rates on burst pressures and burst diameters. The experimental results show that the developed rupture disk fulfills the performance requirements expected in a real operational condition.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.22-25
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• 2009

Development of a curvic-coupling was presented in this paper. The research covers design, structural analysis, hot-temperature-torsion-test, curvic-coupling applied proto-type turbine disk manufacturing, and assembly test of a curvic-coupling rotor system for the turbopump application. Curvic-coupling was designed based on the Gleason-standard-tooth shape. The load capability of the designed curvic coupling was validated by the structural analysis and hot-temperature-torsion-test. A proto-type turbine disk which had adopted designed curvic-coupling was manufactured, assembled and tested to reveal that shaft-disk assembly run-outs in axial and radial directions were much smaller than the design requirements. The development will be finalized after spin test of shaft-disk assembly in near future.

• The KSFM Journal of Fluid Machinery
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• v.7 no.3 s.24
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• pp.80-83
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• 2004

• Journal of Power System Engineering
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• v.11 no.2
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• pp.38-43
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• 2007

전자기적으로 지지되는 임펠러를 가진 원심 혈액 펌프는 기존의 심장 펌프에 비해 많은 장점을 가지고 있지만, BVAD의 틈새에서 발생하는 유체 동역학적인 문제는 여전히 규명이 되지 않은 상태이다. 본 연구에서는 BVAD의 틈새에서 발생하는 혈액외상(blood trauma)의 예측에 대한 연구에 중점을 두고 있다. 일반적으로 원심 혈액 펌프의 설계를 위해 전자기적으로 지지되는 원심 혈액 펌프의 디스크 틈새에서 발생하는 혈액의 손상을 평가하는 방법으로 CFD를 이용한 방법이 널리 이용되고 있다. 따라서, 본 연구에서는 초기 원심 혈액 펌프의 설계 단계에서 펌프의 특성을 평가하기 위하여, 축 방향 틈새의 영향과 회전수 변화에 따른 누수경로의 전단 응력의 크기 평가를 CFD를 사용하여 해석하여 보았다.

• Aerospace Engineering and Technology
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• v.9 no.2
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• pp.204-209
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• 2010

The current status of the development of pyrostarters, which play a role as a turbo pump starter in liquid propellant propulsion systems by supplying pressurized gas to power turbines for engine start, has been introduced. Firstly, the development history is briefly summarized, and secondly the current technical status in core parts for the development of pryrostarters such as solid propellants, internal ballistics, rupture discs, and igniters are presented. The current technical achievements could make it feasible to fulfill the development requirements for pyrostarters.

• Proceedings of the KIEE Conference
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• 2004.07c
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• pp.2093-2095
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• 2004

본 논문은 압전소자를 구동장치로 사용한 마이크로 펌프의 제작과 실험에 관한 논문이다. 마이크로 펌프의 상부기판은 polydimethyl siloxane(PDMS)을 소재로 미세유로에 상시 닫힌 밸브가 일체화된 구조로 제작되었고, 하부기판은 polymethyl methacrylate(PMMA)를 소재로 3개의 압전 디스크가 구동기로 부착되었다. 최종적으로 상, 하부 기판은 액상 PUMS로 접합하여 제작했다. 구동기의 입력신호는 6상으로 구형파를 인가하여 연동구동하며 주파수와 전압을 가변하면서 유량을 측정하였다. 구동 주파수가 0.167 Hz이고 전압이 20 V일 때, 마이크로펌프의 1회 토출량은 104 nl이고, 유량은 1.04${\mu}{\el}$/min이다.

• The KSFM Journal of Fluid Machinery
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• v.14 no.6
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• pp.18-25
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• 2011

A boundary-layer pump with a single disk has been experimented to obtain its characteristic curve by changing the impeller of a centrifugal pump to a single disk. The primary objective to use of these types of pumps is to avoid hurting water life during transportation unnecessarily. The change of impeller should degrade the performance of pump, so we used the method to increase the roughness on the disk with sandpaper and mesh. The enhancement of shear force from the rotation of disk to the internal flow brought an augmentation of momentum transport, and the characteristics were far improved from the original single-disk pump without decreasing the survival rate of water life in the case of Pseudobagrus fulvidraco (bullhead fish). However, in the case of Artemia cyst (zooplankton), the survival rate was very degraded due to the micro scale smaller than turbulent eddy size. The result of this study could be used for the design of transportation and bio-filtering of water lying on a specific bandwidth of its scale of size.

• Journal of the Korean Society of Manufacturing Technology Engineers
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• v.21 no.3
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• pp.355-361
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• 2012

Though a micro pump is a crucial element in miniaturized bio-fluidic systems or drug delivery systems, it has some intrinsic disadvantages such as backward flow, pulsation of flow, low repeatability and producibility, and high cost. To overcome these limitation, a PZT disc actuated micro pump including a novel ring-shaped multi-flap check valve is introduced. To enhance the performance of the micro pump, the static behaviour of flap valve module and the micro fluidic behavior of fluids are numerically modelled and analyzed. As results of the numerical analysis, the optimal dimension and configuration of the ring-shaped multi flap valve are $1{\times}0.05$ mm and 2 (inlet side)${\times}1$ (outlet side) type. The obtained maximum flow rates and flow resolution are about 90 ml/min and 30 ${\mu}l$/stroke respectively.