• Journal of the Computational Structural Engineering Institute of Korea
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• v.30 no.2
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• pp.179-184
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• 2017

Due to rapid development of infrared guided weapon, survivability of armored vehicle is severely threatened. Hence, reduction of susceptibility by lowering infrared signature level is essential to enhance survivability of the vehicle. For this purpose, numerical analysis is conducted to analyze time and spatial characteristics of infrared signature of the vehicle when surface emissivity changes in this study. The analysis shows that the emissivity which produces minimum contrast radiant intensity is significantly altered by time and detecting position. Based on the result, it is concluded that the controlled structures which have different emissivity should be adopted at different region of the vehicle to effectively decrease infrared signature level.

• 전기의세계
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• v.41 no.10
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• pp.16-23
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• 1992

원적외선의 이용은 에너지절약을 목적으로한 효율이 높은 열전파형태로서 주로 응용되고 있다. 따라서 방사체의 적외선 방사특성과 피가열체의 적외선 흡수특성과의 관계가 먼저 명확하게 규명되어야 한다. 그러면, 그 흡수특성과 정합된 원적외선 방사세라믹스의 제작도 가능하게 되어갈 것이므로 원적외선의 작용효과가 각종 분야에서 이용되어 갈 것이다. 예를들면 의료분야에서 과거에는 인체의 일부를 가온할 필요가 있을 때에는 고주파전류, 마이크로파 또는 환부를 유동 파라핀속에 넣어 환부를 따뜻하게 하는 방법 등이 있지만 만약 어떤파장의 원적외선이 인체의 피부 깊숙이 투과가 가능하다면 마이크로파 방생장치 대신에 원적외선의 발생장치가 값이 저렴하고 기온부를 국소로 제한 할 수 있으므로 널리 사용되어질 것이다. 또 식품분야에서는 에너지절약의 관점에서 뿐만아니라 조리의 관점에서도 원적외선의 이용이 진전되어 갈 것으로 생각된다. 한편 원적외선센서의 진전은 놀랄만하여 앞으로 초전도세라믹스를 이용한 원적외선 검출의 죠셉슨센서는 더욱 진전되어 질것으로 생각된다. 어떻든 각종 원적외선방사 세라믹스의 개발과 원적외선 영역에서의 파장 특성에 대한 측정법이 확립되어짐에 따라서 원적외선 이용은 앞으로 각종방면에 진전되어질 것이다.

• Journal of the Korean Society of Propulsion Engineers
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• v.21 no.1
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• pp.1-7
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• 2017

As a part of studies to lower the infrared (IR) emissivity from the surface of exhaust nozzle in the turbo jet engine, stainless steel plate was coated with copper particle/meta-aramid resin composites and the IR emissivity of the plate were investigated. Binders of filler particles based on synthetic polymers generally undergo thermal decomposition before $300^{\circ}C$. It was found that the meta aramid resin was thermally stable after the test at $320^{\circ}C$, confirming the excellent thermal stability. Contents of copper particles in the composites were varied from 0 to 70% by volume. It was observed that the copper particle/meta aramid resin composites showed good adhesion after the tests at $320^{\circ}C$. The specimen coated with the composite containing 50 vol% of copper particles showed the lowest IR emissivity, 0.6, at $320^{\circ}C$.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.7
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• pp.545-551
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• 2016

Surface temperature of supersonic wind tunnel model was measured using an infrared thermography technique. To measure the temperature quantitatively, various calibration techniques such as blackbody calibration which converts detected camera signal to temperature, distortion correction due to the camera lens and an imbalance of camera pose, and emissivity calibration which considers viewing angles to the model surface, were employed. Throughout the study, for the quantitative as well as qualitative surface temperature measurement, it was verified that the distortion correction must be considered even for the use of two-dimensional model in aerodynamics testing.

• Proceedings of the KIEE Conference
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• 2004.07c
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• pp.1721-1723
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• 2004

우리는 황토 조명등을 제작하여 원 적외선 발생 실험을 하였다. 실험에는 백열전구 200W, 실내온도 21도, 습도 38%의 조건에서 열화상실험과 TF-IR(적외선 분광방사 측정장치)에 의한 원적외선 방사한도를 측정하였으며, 그 결과 방사율 0.914와 방사에너지 $6.23{\times}10^2\;(w/m^2{\cdot}{\mu}m)$ 가 얻어졌다. 이와 같은 결과로 황토조명등에서 원적외선이 발생한 것을 확인하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.3
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• pp.240-245
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• 2013

Each pixel of InfraRed(IR) sensor differently responds to IR light as time elapses or the sensor on/off operation is repeated. As a result, the quality of IR sensor image is deteriorated, and therefore NUC(Non-uniformity Correction) is periodically needed for IR sensor. In this paper, in order to perform NUC in the Satellite, on-board V-grooved blackbody is designed with a baffle so that the emissivity of black body is to be higher than 0.995 as well as the temperature deviation is less than $1^{\circ}C$ in the range of the infrared wave length from 3.3 to $5.2{\mu}m$. To check its performance, the emissivity and the surface temperature of the blackbody by TRT(Transfer Reference Thermometer) and IR Micrometer scanner are measured, respectively. From the results, black body design is verified and the uncertainty of NUC is estimated through the measurement results.

• Journal of The Korean Society For Urban Railway
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• v.6 no.4
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• pp.243-248
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• 2018

The abnormally high temperature of the train part is related to train accidents and monitoring is important for safe operation of trains. In case of KTX an abnormality detecting device that detects the abnormality of the axle and scans the urban railway is installed on the railroad and when there is an abnormal heat generation, a system for automatically informing the control center is installed. The IR sensors module used in this system are depend on quick response. we have conducted a study on the fast response test method through the production of experimental equipments.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.307.2-307.2
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• 2013

창호를 통해 건축물 내부에 유입되는 태양광, 특히 태양열 유입에 큰 영향을 미치는 적외선 파장대역을 차폐할 수 있는 특성을 갖는 근적외선 반사 또는 흡수용 원천소재 개발하였다. 근적외선 반사는 고 굴절률/저 굴절률 다중 코팅막을 이용하여 상대적으로 에너지가 높은 800~1,300 nm 파장 영역의 근적외선만을 효율적으로 반사시킬 수 있 방식으로 적외선 차단 효율을 개선하였다. 근적외선 흡수용 나노박막 유 무기 복합소재를 기반으로 하여 특정 파장대에서 적외선을 흡수하도록 하여 적외선 차단 효율을 증대시켰다. 본 연구개발의 고단열 유리는 기존에 개발된 저방사 유리의 문제점인 높은 근적외선 투과문제를 해결하기 위한 대체/보완기술로서 이를 이용한 대면적 코팅을 통한 고기능성 복층창호 시스템을 구성하였고, 이에 대한 단열 특성 실험을 실시하였다.

• Aerospace Engineering and Technology
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• v.12 no.1
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• pp.40-45
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• 2013

Satellite's infrared detector shall be calibrated under thermal vacuum environment using a reference black body before a launch. The full aperture black body (FABB) as an infrared calibration reference shall be composed of vacuum compatible materials and temperature controlled from $-40^{\circ}C$ to $+40^{\circ}C$ with emissivity higher than 0.95. The temperature homogeneity over the central 80 % area of the FABB front surface shall be better than 2 K. The FABB designed by thermal and flow analysis was $1m{\times}1m{\times}8mm$ copper plate on which black painted aluminum honeycomb core was attached. Copper tubes were welded on the opposite side of the honeycomb core to allow temperature regulated gaseous nitrogen to flow through them. By the FABB validation test, the temperature homogeneity was observed around 1 K using 20 PT100 sensors and modified COTS infrared camera. The emissivity value was 0.975 at $40^{\circ}C$ under atmospheric pressure.

• Polymer Science and Technology
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• v.24 no.6
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• pp.612-617
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• 2013