• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.8
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• pp.111-121
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• 2005

A 100kW class gas turbine combustor was developed and tested for PPU(Primary Power Unit) of ground vehicle. The combustor which employed annular-reverse type and pressure swirl atomizer was designed through 1-D analysis, 3-D thermal flow analysis and combustor performance was experimentally investigated on the combustor test rig. The test result was satisfactory. The developed combustor was also tested for environmental and endurance specification under engine adopted conditions and the application of a state-of-the-art gas turbine combustor to ground vehicle PPU turned out to be successful.

• Aerospace Engineering and Technology
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• v.8 no.1
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• pp.1-9
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• 2009

The ground integration test of Smart UAV has been performed according to the flight test plan. The flight test of full scaled model will be performed followed by 4 DOF ground rig test and a tethered hover test. Smart UAV is the first indigenous tiltrotor aircraft which can fly with fast cruise speed and take off or land vertically. In order to prove the flight control law of Smart UAV, the 40% scaled airplane was developed and have been tested. During flight test of small scaled model, many unique and unexpected problems occurred. After clearing these problems, fully automatic flight test was performed successfully. The experiences about many trouble shooting and resolving the problems would be basic material to avoid the unexpected but similar flight test problems hidden behind of the full scaled Smart UAV. This paper presents the detailed procedures of trouble shootings to solve the unique problems which occurred during the flight test of small scaled tiltrotor UAV.

• The Journal of Korea Institute of Information, Electronics, and Communication Technology
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• v.8 no.6
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• pp.470-477
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• 2015

This paper presents a new technique for generating an optimum synchronizable test sequence that can be applied in the distributed test architecture where both external synchronization and input/output operation costs are taken into consideration. The method defines a set of phases that constructs a tester-related digraph from a given finite state machine representation of a protocol specification such that a minimum cost tour of the digraph with intrinsically synchronizable transfer sequences can be used to generate an optimum synchronizable test sequence using synchronizable state identification sequences as the state recognition sequence for each state of the given finite state machine. This hybrid approach with a heuristic and optimization technique provides a simple and elegant solution to the synchronization problem that arises during the application of a predetermined test sequence in some protocol test architectures that utilize remote testers.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.38 no.3
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• pp.429-438
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• 2018

Cone and T-bar penetrometers have been frequently used to estimate the undrained shear strength of clay. For small-size model tests, miniature penetrometers should be used but their correlation factors have not been well published. In this study, a testing setup was developed to derive empirical factors of the miniature cone and T-bar penetrometers. A 350mm-diameter chamber and kaolin clay were utilized to prepare soil specimens consolidated under four different pre-consolidation pressures controlling undrained shear strength. Two miniature cones with two diameters of 10-mm and 16-mm and a T-bar penetrometer with 10-mm diameter were used to investigate boundary effect, penetration rate effect, and diameter and shape effect. Unconsolidated-undrained triaxial tests were carried out with samples taken from the specimens to measure undrained shear strength. Finally, empirical factors for the penetrometers were constructed to correlate tip resistance to undrained shear strength.

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
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• 2013.04a
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• pp.144-145
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• 2013

국내에서 생산되고 있는 화재감지기는 설치 환경, 위치, 전기적 및 기계적인 요인에 따라 그 성능의 신뢰성이 차이를 나타내고 있다. 본 연구는 국내에서 제조되고 있는 국내 화재감지기 성능 신뢰성 제고를 위한 방안을 제시하고자 열감지기, 연기감지기, 불꽃감지기 등의 성능시험 관한 각 기관별 주요 내용과 차이점을 비교 검토하였다. 이를 위해 국가시험기관의 27종, 방재시험연구원 46종류, 국제 표준화기구 36종류를 대상으로 한바 다양한 환경에서 적응하고 신뢰성 향상에 비중이 많았다. 감지기에서 발생하는 비화재보, 감지지연 및 기타 원인 불명등과 시험기준의 상호관계를 확인하는 연구가 선행되어야 한다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.7 no.1
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• pp.110-121
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• 1983

ASHRAE 표준을 참고로 하여 한국과학기술원(KAIST)에서 수정한 집열기 시험 장치의 주요부품 의 설계도면 및 Specification 등을 제시하였다. 또한 ASHRAE 표준 시험 절차를 재분석하고 KAIST에서 수정한 Test Loop를 시험하기 위한 실험절차의 개요도 설명하였다. ASHRAE 표준 상의 가장 중요한 실험인 (1) 집열기 시간 상수 실험과 (2) 수직에 가까운 입사각에 대한 효율 실 험 및 (3) 입사각 수정 계수 실험 등을 실제 태양 아래에서 실험하여 그 결과도 그림으로 제시하 였다. 본 연구를 통해서 얻은 결과로부터 다음과 같은 결론을 얻을 수 있었다. 한국 과학 기술원 에서 설계한 집열기 시험 장치는 ASHRAE의 표준 절차에 따라 액체 가열식 집열기의 열효율을 측정하기 위한 실용적 장치임을 알 수 있다. 일반적으로 ASHRAE 표준 93-77은 합리적인 절차 라고 할 수 있다. 그러나, 최소일사량 규정(즉 630W/m$^{2}$ 미만이 되어서는 안된다고 하는 ASHRAE 규정) 같은 것은 일사량이 적은 기후 조건하에서는 다소 하향 조정하여도 정확한 효율 곡선을 얻을 수 있다고 하겠다.

• Journal of the Korea Convergence Society
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• v.10 no.1
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• pp.149-154
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• 2019

High pressure valve tester used in industrial fields precise measurement gives inconvenience in precise measurement due to manually regulated pressures. In order to improve this inconvenience, the high pressure valve tester was designed by using CATIA and structural analysis of the designed high pressure valve tester was conducted and water leaking, total deformation, strain and stress were obtained by applying ANSYS. These results will be provided to develop new concepts of high pressure valve tester as initial data.

• Journal of the Korean Society of Propulsion Engineers
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• v.2 no.2
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• pp.99-107
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• 1998

A test on venturi-type premixer of ASE120 engine combustor has been performed to evaluate its mixing performance. Cold air was supplied into the premixer through the fuel nozzle and mixed with the hot air from the compressor exit. The measured temperature of the mixed air was used to evaluate the mixedness. DOE(Design of Experiment) technique was utilized to make a test matrix of variables and to determine the optimum combination of variables, which was verified through a confirmation test.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.107-110
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• 2008

The test range for turbopump and gas generator coupled test was determined considering the engine system test area which cover the qualification and development. Based on the test range, we determined the required loss coefficient for the throttle valves and lines.

• Proceedings of the IEEK Conference
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• 2003.07a
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• pp.330-333
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• 2003

본 논문에서는 조립/제작, 시험과정을 통하여 개발된 통신방송위성용 Ka 대역 통신위성 중계기의 구조 및 성능에 대하여 기술한다. 개발된 중계기는 전체 400MHz 대역 내에 100 MHz 대역폭을 갖는 3 개의 통신채널을 수용하여 광대역 멀티미디어 서비스를 지원할 수 있도록 설계되었으며 국내 기술로 제작되어 우주인증을 거친 IFA, RxDC, IMUX, CH-AMP 등의 부품으로 구성되어 있다. 중계기에 대한 성능시험은 EGSE를 이용해 자동으로 수행되었으며, 성능시험결과 대부분의 성능 항목이 요구사항과 부합됨을 확인하였다. 제작된 Ka 대역 중계기에 적용된 위성 중계기 및 부품의 제작 및 시험 기술은 향후 통신해양기상위성에 탑재될 중계기의 개발에 직접 응용이 가능하다.