• Proceedings of the Korean Vacuum Society Conference
• /
• 2015.08a
• /
• pp.103.2-103.2
• /
• 2015

10-3 Pa 이하의 고진공 환경과 $180^{\circ}C$ 이하의 극저온 환경에서 대형정지궤도위성의 고온 열평형 환경구현을 위한 열제어패널이 설계되었다. 열제어패널은 가로 2.2 m, 세로 2.6 m, 두께 2 mm의 구리판에 구리 튜브가 브레이징되어 있는 형태로 설계되었으며, 지상에서 6 m 이상의 높이에 설치되고 위성의 위치에 따라 이동이 가능해야 하기 때문에, 별도의 지지 구조물이 함께 설계되었다. 따라서, 열제어패널 설치 및 고정을 위한 지지구조물의 경우 160 kg의 무게를 견뎌내야 하며 이동 및 설치에 있어 구조적인 안전성이 확보 되어야 한다. 이에 본 연구에서는 상용유한요소해석 프로그램을 사용하여 열평형시험 시 위성체 상단부의 고온 환경모사를 위한 열제어패널 지지구조물에 대한 구조 안전성을 확인 하였다.

• Proceedings of the Korean Vacuum Society Conference
• /
• 2013.08a
• /
• pp.114.2-114.2
• /
• 2013

위성체가 임무를 수행하는 우주환경은 지상 환경과 달리 고진공, 고온 및 극저온의 가혹한 환경 이다. 이에 $10^{-5}$ Torr 이하의 고진공과 $-180^{\circ}C$ 이하의 극저온 및 고온의 환경조건을 지상에서 모사하기 위해서는 열진공챔버와 같은 우주환경모사장비가 사용된다. 위성체를 열진공챔버에 설치하고 우주환경모사 시험의 월할한 진행을 위하여 열진공챔버 내 레일을 설치하여 열진공시험 준비 및 열진공시험이 수행되어진다. 현재 위성체 연구개발의 발전으로 다양한 기능 및 장비의 추가로 인하여 위성체가 대형화 되어지고 있다. 이에 보다 안전한 시험 준비 및 수행을 위하여 현재 운용되어지고 있는 열진공챔버의 개선이 필요하다. 이에 본 연구에서는 상용유한요소해석 프로그램 MSC.PATRAN/NASTRAN을 사용하여 대형 위성체의 우주환경모사 시험을 위한 열진공챔버 내 레일에 대한 구조 안선성을 평가 하고자 한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2008.11a
• /
• pp.181-184
• /
• 2008

Austenitic stainless steel is used as high temperature components such as gas turbine blade and disk because of its good thermal resistance. In the present investigation, tensile and low cycle fatigue behavior of 316 stainless steel was studied at wide temperature range $20^{\circ}C{\sim}750^{\circ}C$. In the tensile tests, it was shown that elastic modulus, yield strength, ultimate tensile strength decreases when temperature increased. The effect on fatigue failure of the parameters such as plastic strain amplitude and plastic strain energy density was also investigated. With the experimental results, a structural analysis of turbine blades of 316 stainless steel were carried out.

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

• Proceedings of the Korean Nuclear Society Conference
• /
• 2001.05a
• /
• pp.497.1-497
• /
• 2001

• Proceedings of the Korean Nuclear Society Conference
• /
• 2003.05a
• /
• pp.406.1-406.1
• /
• 2003

• Proceedings of the KIEE Conference
• /
• 2007.04c
• /
• pp.41-42
• /
• 2007

초전도 변압기의 권선에서 발생하는 교류손실은 시스템의 효율과 안정성에 큰 영향을 미친다. 본 논문에서는 고온 초전도 변압기의 권선 구조에 따른 교류손실과 % 임피던스 특성을 살펴보았다. 변압기 철심의 형태가 내철형과 의철형인 경우에 대하여 설계를 하였으며 각 형태에 따른 교류손실과 % 임피던스를 계산하였다. 154 kV/5 MVA 고온 초전도 변압기의 두 가지 철심 형태의 해석을 통해 각각의 특성을 비교하였다.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.10 no.4
• /
• pp.69-76
• /
• 2006

Elastic-viscoplastic structural analysis has been performed for regenerative cooling chamber of liquid rocket thrust chamber using Bodner-Partom visco-plastic model. Strain rate test was conducted for a copper alloy at various temperatures in order to get material constants of visco-plastic model used in the structural analysis. Material constants of visco-plastic model were obtained from strain rate test results and visco-plastic model was incorporated into finite element program, Marc, by means of a user subroutine. The structural analysis results indicated that the deformation of cooling channel is mostly caused by thermal loading rather than pressure loading and confirmed structural stability of the cooling channel under the operating condition.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.36 no.7
• /
• pp.759-768
• /
• 2012

This paper proposes a method to determine the elastic follow-up factors for the $C(t)$-integral under secondary stress. The rate of creep crack growth for transient creep is correlated with the $C(t)$-integral. Elastic follow-up behavior, which occurs in structures under secondary loading, prevents a relaxation of stress during transient creep. Thus, both the values of $C(t)$ and creep crack growth increase as increasing elastic follow-up. An estimation solution for $C(t)$ was proposed by Ainsworth and Dean based on the reference stress method. To predict the value of $C(t)$ using this solution, an independent method to determine the elastic follow-up factors for cracked bodies is needed. This paper proposed that the elastic follow-up factors for $C(t)$ can be determined by elastic-plastic analyses using the plastic-creep analogy. Finite element analyses were performed to verify this method.

• Aerospace Engineering and Technology
• /
• v.5 no.2
• /
• pp.174-180
• /
• 2006

The present paper describes transient thermal and mechanical analyses of a lox/kerosene type turbopump in a LRE(Liquid Rocket Engine). Turbopumps are used to pressurize propellants to achieve higher specific impulse of LRE. The turbopump under development has been designed and verified by structural analyses using finite element methods. Some parts of the turbopump operate under cryogenic environments, while the others work under ambient and high temperature environments. Therefore, numerical analysis at a turbopump system level is essential. In this study, casing assemblies of lox pump and fuel pump were analyzed to determine strength test and air-tightness test conditions. Also, some operational stress and strains of fuel pump casings were measured and analyzed. Based on these results, stress concentration of fuel pump casings during the operation could be successfully predicted.