• 제목/요약/키워드: High/Low Temperature Test

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수출형 KT-1 훈련기 고/저온 환경시험절차 적합화 연구 (A Study on the Tailoring of High / Low Temperature Test for KT-1 Trainer Export Version)

  • 김진석
    • 시스템엔지니어링학술지
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    • 제16권2호
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    • pp.78-86
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    • 2020
  • The environmental tests are one of the key branches of the reliability tests. The purpose of the high/low environmental test of KT-1 Export Version Trainer is not only based on meeting the compliance of the reliability, customer satisfaction, but also for the expansion of its export. Amongst many existing environmental tests, the high and low temperature tests are considered as the two most important tests. The tests are considered and tailored to the high and low temperature methods of MIL-STD-810H. This paper proposes the tailoring processes and the results of High/Low temperature conditions, test procedures, and test profiles for the aircraft. Additionally, this paper is described by considering the view of MIL-STD-810H.

FA-50 경공격기 전기체 지상 고/저온시험 (Ground High/Low Temperature Test for FA-50 Aircraft)

  • 안종훈;김태호;우승철;조영균;김도완
    • 시스템엔지니어링학술지
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    • 제6권1호
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    • pp.41-46
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    • 2010
  • The ground high/low temperature test objective is to check the normal ground operation of FA-50 aircraft in the extreme ground ambient conditions. The aircraft was exposed in climatic conditions of the basic climatic category according to the MIL-HDBK-310. For verified normal operation in the extreme high temperature, the high temperature test was performed in the hot regional type conditions and accentuated solar radiation heat. This test was performed at the test chamber in ADD where is in Haemi. This paper was described about the test procedure of FA-50 high/low temperature including preparation, testing and results.

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XKT-1T 항공기 환경 요구사항 적합화 연구 (A study on the Tailoring of Environmental Requirements for XKT-1T Aircraft)

  • 김진석
    • 시스템엔지니어링학술지
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    • 제17권1호
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    • pp.97-106
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    • 2021
  • The purpose of the study on the tailoring of environmental requirements for KT-1 Export Version(XKT-1T) aircraft is not only based on meeting the compliance of the environmental reliability, customer satisfaction, but also for the expansion of its export. This paper proposes the environmental requirements tailoring processes and High/Low temperature conditions, test procedures, and the results of test profiles for the aircraft. Amongst many existing environmental requirements, the temperature requirements are considered as the most basic and the most important environmental requirements. The High/Low temperature tests are considered and tailored to the high and low temperature methods of MIL-STD-810.

고기능성 투습방수 소재의 저온굴곡 시험방법 개선 연구 (A Study on Improvement of the low temperature flex resistance test method about high waterproof materials)

  • 이민희;문선정;고혜지;홍성돈
    • 품질경영학회지
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    • 제46권3호
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    • pp.425-440
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    • 2018
  • Purpose: This study is aimed at developing of the flex resistance testing process at low temperature with the waterproof fabric to suit the military environment, and is designed to fit for the purpose of the waterproof materials in order to optimize the test method by finding out matters to improve from existing the test method and through previous studies. Methods: The test method, which has been applied to flex resistance of existing water-repellent materials, was improved and consequently, differentiated test results could be obtained according to the test temperature, sample size, and flexing method. Results: The testing of the total of 8 samples revealed that performance of the military requirement could hardly be met just by presenting the materials or 2~3 layers when the quality criteria for high functional water repellent fabrics were applied. PTFE(Polytetrafluoroethylene) is preferred to PU(Polyurethane) to be used in the extremely low-temperature environment, but durability under the low-temperature environment may be varied depending on film thickness or laminating technique even if the materials of waterproof films are identical. Therefore, in addition to the material or texture, the test method capable of reflecting durability under the low-temperature environment shall be suggested, and the newly designed test method proposed in this study was shown to suggest differentiated quality criteria by the material. Conclusion: The water resistance measurement and the test method following flex resistance with expanded range of flex will enable the differentiable test of the samples according to the number of repetition. This study is meaningful in that it suggests a differentiable test method capable of establishing a basis of deciding suitable material when selecting military goods made of water repellent material by properly improving the test method.

TiC-Mo 공정복합재료의 고온 변형특성 (Deformation Properties of TiC-Mo Eutectic Composite at High Temperature)

  • 신순기
    • 한국재료학회지
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    • 제23권10호
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    • pp.568-573
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    • 2013
  • The deformation properties of a TiC-Mo eutectic composite were investigated in a compression test at temperatures ranging from room temperature to 2053 K and at strain rates ranging from $3.9{\times}10^{-5}s^{-1}$ to $4.9{\times}10^{-3}s^{-1}$. It was found that this material shows excellent high-temperature strength as well as appreciable room-temperature toughness, suggesting that the material is a good candidate for high-temperature application as a structure material. At a low-temperature, high strength is observed. The deformation behavior is different among the three temperature ranges tested here, i.e., low, intermediate and high. At an intermediate temperature, no yield drop occurs, and from the beginning the work hardening level is high. At a high temperature, a yield drop occurs again, after which deformation proceeds with nearly constant stress. The temperature- and yield-stress-dependence of the strain is the strongest in this case among the three temperature ranges. The observed high-temperature deformation behavior suggests that the excellent high-temperature strength is due to the constraining of the deformation in the Mo phase by the thin TiC components, which is considerably stronger than bulk TiC. It is also concluded that the appreciable room-temperature toughness is ascribed to the frequent branching of crack paths as well as to the plastic deformation of the Mo phase.

15Cr 페라이트계 스테인리스강의 겹침용접부 고온인장 특성에 관한 연구 (A Study on the High Temperature Tensile Characteristics of Lap Weld of 15Cr Ferritic Stainless Steels)

  • 이영기;이경철;김재성;한도석;오승택;이보영
    • Journal of Welding and Joining
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    • 제26권5호
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    • pp.60-65
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    • 2008
  • Ferritic stainless steels of the 400 series have been available for automotive exhaust system, heat exchanger, radiater etc. in various industrial because heat resistance, corrosion resistance and strength are excellent. Especially, automotive exhaust system is required good heat resistance because typical temperature of exhaust system exposed during operation of engine is reach up to $800^{\circ}C$. However, research for effect of high temperature in ferritic stainless steels is not enough. In this study, high temperature tensile properties of lap weld of ferritic stainless steels(STS 429) were investigated. In accordance with heat input, lap welds had been produced and were evaluated at high temperature($800^{\circ}C$) to compare high temperature tensile properties. In addition, room temperature tensile tests were carried out for non-aging and aging specimens. As a result of R.T tensile test, non-aging specimens were fractured in base metal except for low heat input specimen and aging specimens were fractured in weld metal. Also high temperature tensile test were carried out by aging specimen. After high temperature tensile test, fracture of aged specimen was occurred in base metal except for low heat input specimen. Fracture surface of low heat input specimen in weld metal was confirmed as brittle fracture with observation using scanning electron microscope(SEM). Significant decrease in ultimate tensile strength (between 82 and 85%) was observed for aged ferritic stainless steels(STS 429) when tested at high temperature.

XKT-1(수출형 KT-1) 항공기 열 환경시험에 관한 연구 (Study on Thermal Environmental Test for XKT-1 (KT-1 Export Version) Aircraft)

  • 김진석
    • 항공우주시스템공학회지
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    • 제15권3호
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    • pp.105-113
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    • 2021
  • 본 논문은 MIL-STD-810 시험법 501(고온 시험법)과 시험법 502(저온 시험법)를 기반으로 XKT-1(수출형 KT-1) 항공기 고객의 운용 환경과 요구사항에 적합하도록 시험조건과 시험절차를 최적화하여 열 환경시험 프로파일을 제시하였다. 또한, 이렇게 최적화된 고온 및 저온시험 프로파일을 환경시험 종합평가 계획서에 반영하여 국방과학연구소의 기후환경 챔버에서 시험수행 하였다. 본 고온 및 저온 환경시험 프로파일로 XKT-1(수출형 KT-1) 항공기의 고온 및 저온 환경시험수행 결과, 고객 환경 요구사항을 만족하고 혹독한 열 환경에서 신뢰성 있음을 확인하였다. 특히 본 논문에서 제안된 고온 및 저온 환경시험절차와 프로파일은 더 혹독한 환경시험 조건의 수출형 항공기 환경시험에도 응용할 수 있다.

자동차 제동시 나타나는 Anti-Fading현상에 관한 연구 (Study of Anti-Fading Phenomena during Automotive Braking)

  • 이정주;장호
    • Tribology and Lubricants
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    • 제14권1호
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    • pp.70-78
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    • 1998
  • Two different friction materials (organic and low-metallic pads) for automotive brakes were studied to investigate the anti-fading phenomena during stop. The anti-fading phenomena were pronounced more in the case of using low metallic friction materials than organic friction materials. The main cause of the anti-fading phenomena was the high dependence of friction coefficient on a sliding speed. The anti-fading was prominent when the initial brake temperature was high in the case of low-metallic friction materials due to the strong stick-slip event at high temperature. On the other hand, the anti-fading was not severe in organic friction materials and the effect was reduced at high braking temperature due to the thermal decomposition of organic friction materials. The strong stickslip phenomena of low metallic friction materials at high temperature induced high torque oscillations during drag test. During this experiment two different braking control modes (pressure controlled and torque controlled modes) were compared. The type of the control mode used for brake test significantly affected the friction characteristics.

대향류 확산화염의 고온공기 연소특성에 관한 수치해석 (A Numerical Analysis of the Characteristics with High Temperature Air Combustion in Counterflow Diffusion Flame)

  • 조은성;히데아키 코바야시;정석호
    • 한국연소학회지
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    • 제8권4호
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    • pp.9-14
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    • 2003
  • High temperature air combustion technology has been utilized by using preheated air over 1100 K and excessive exhaust gas recirculation. Numerical analysis was performed to investigate the combustion characteristics with high temperature deficient oxygen air combustion by adopting a counterflow as a model problem accounting for detailed chemical kinetics. Methane($CH_4$) was used as a test fuel and calculated oxidizer conditions were low temperature high oxygen (300K, $X_{O2}=0.21$) and high temperature low oxygen (1300K, $X_{O2}=0.04$) conditions. The latter case showed that the flame temperature is lower than the former case and its profile showed monotonic decrease from oxidizer to fuel side, without having local maximum flame temperature at high stretch rate. Also, heat release rate was one order lower and it has one peak profile because of low oxygen concentration and heat release rate integral is almost same for stretch rate. High temperature low oxygen air combustion shows low NO emission characteristics.

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엔진 오일 열화와 피스톤 톱링 그루브 온도가 카본 디포짓 형성에 미치는 영향 Part II-디젤 엔진의 디포짓 형성 특성 (The Effect of Engine Oil Degradation and Piston Top Ring Groove Temperature on Carbon Deposit Formation Part II - The Deposit Formation Characteristics of Diesel Engine)

  • 김중수;민병순;오대윤;최재권
    • Tribology and Lubricants
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    • 제14권4호
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    • pp.108-113
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    • 1998
  • In order to investigate the characteristics of top ring groove deposit formation in diesel engine, engine test and simulation test were performed. From component analysis of used oils sampled from actual running engines, soot content in engine oil was selected as a main parameter for evaluating oil degradation. Deposit formation is highly related to soot content in lubricating oils. And high soot content oil accelerates deposit formation even in low temperature region below 26$0^{\circ}C$. In low temperature region below 26$0^{\circ}C$, deposit formation rate is mainly affected by top ring groove temperature. However, in high temperature region above 26$0^{\circ}C$, deposit formation rate is affected by soot content as well as top ring groove temperature. Therefore, soot content as well as top ring groove temperature should be kept a certain level in order to prevent troubles due to carbon deposit formation.