• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2008.05a
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• pp.77-80
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• 2008

해상통신은 인명 안전을 위한 중요 통신으로 국제적으로 보호되어 왔다. 뿐 만 아니라 지구 전역을 커버하기 위해 전송 특성이 좋은 LF/MF/HF대역의 통신시스템 및 위성 시스템이 이용되고 있다. 최근에는 통신 기술의 발달로 육상이동통신 기술을 해상 및 항공에 확대하려는 시도가 꾸준히 진행되고 있다. 통신 기술의 급속한 발전으로 해상 및 항공 통신망은 기존 음성 위주의 통신망에서 멀티미디어를 처리할 수 있는 디지틀망으로의 전환이 시급히 필요하게 되었다. 대부분의 아날로그 시스템은 디지틀 시스템으로 전환되고 있으며 데이터를 이용해서 보다 정확한 정보를 제공해서 해상 안전을 높이고 있으며 기존 개별 장비를 시스템화하여 주파수를 효율적으로 활용하고 사용을 편리하게 할 수 있도록 하고 있다. DSC, AIS 등 이미 많은 디지틀 장비들이 국제 해상 통신에 이용되고 있으며 해상 통신 시스템을 종합화해서 해상안전을 제고하기 위해 IMO를 중심으로 주진 중에 있다. 그러나 연근해 해상 통신 시스템은 SOLAS조약에서 제외되어 있으므로 나라마다 다양하게 개발되고 있다. 특히 연근해에서 중요한 MF/HF/VHF대역 시스템을 각 국이 경쟁하면서 현대화를 추진하고 있으며 ITU-R을 통해서 표준화를 주도하려고 노력하고 있다. 본 고에서는 연근해 핵심 통신망을 구성할 HF/VHF대역 시스템에 대한 기술을 분석하고 기술하였다.

• Journal of the Institute of Electronics Engineers of Korea TC
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• v.40 no.10
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• pp.59-66
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• 2003

We propose the novel optical burst switching scheme to guarantee a minimum bandwidth for multiple classes. To date, QoS studies on OBS network are capable of differentiating two classes, but have difficulties in providing a minimum bandwidth lot several classes because of lower classes' collision with the highest class bursts in the networks. To solve that problem, in our proposed scheme we assign time zones in a data channel for each class periodically, making one burst have top priority at least its zone. Also, the new burst assembling algorithm, as well as the way of managing data channel, is necessarily proposed to coordinate with the proposed OBS scheme. Through the evaluation, we show that the worst-case end-to-end delay is small enough and the received bandwidth of the lower classes is still assured regardless of the traffic load of the highest class.

• Aerospace Engineering and Technology
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• v.2 no.2
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• pp.33-44
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• 2003

This paper describes the design and analysis technology of composite flexure and composite paddle-type blade which are all key technologies on hingeless rotor system. Through replacing the existing metal or engineering plastic flexure part with composite part, Several required structural analysis were accomplished, which are static analysis by using NASTRAN and dynamic analysis by using FLIGHTLAB. The dynamic characteristics of composite hingeless hub attached with paddle-type blade was also investigated. Further more, small-scaled paddle-type blade was designed using froude scaled properties of existing full size blade. Through this design procedure of composite paddle-type blade, the structural design method was achieved. These results will be applied to accomplishing current project named as "the development of next-generation helicopter rotor system."

• Proceedings of the Korean Society For Composite Materials Conference
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• 2001.10a
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• pp.206-209
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• 2001

This paper contains the development procedure of small-scaled composite rotor blade for helicopter hingeless rotor system. Composite blade design is conducted by using CORDAS program developed by KARI and dynamic analysis is conducted by using Flightlab which is commercial software for helicopter analysis. Also the optimizing procedure of iterative design was described. The designed composite blades were manufactured after establishing the effective curing method. Through this research, the experiences of composite rotor blade development were accumulated and will be applied to the related research field.

• Journal of the Korean Geotechnical Society
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• v.19 no.5
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• pp.327-333
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• 2003

Characteristics of vibration propagation of borehole blasting were analyzed with 578 borehole vibration data obtained from 23 sites which were used in tunnel and underground space design, and 221 tunnel vibration data fron 4 sites of tunnel under construction. Analysis results on the damping of vibration velocity show that site factors in borehole blasting were higher than those in tunnel blasting. And the critical charge calculated from regression equations at large scaled distance was lower in borehole blasting. Dominant frequency was in the range of 30∼60Hz for the borehole blasting and 60∼90Hz for the tunnel blasting. As a conclusion, the borehole blasting data should not be used on the tunnel blasting design without careful statistical analysis.

• Journal of Korean Medical classics
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• v.19 no.2 s.33
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• pp.196-221
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• 2006

자락출혈료법방면(刺絡出血擾法方面), 금원사대가재침구상다사용료자락법(金元四大家在鍼灸上多使用了刺絡法), 류완소재임상상(劉完素在臨皮上), 자락출혈이대자팔관법(刺絡出血以大刺八關法), 진행청열사화(進行淸熱瀉火), 저여사화파사상상일치(這與瀉火派思想相一致). 장종정야수류완소적영향(張從正也受劉完素的影響), 용비침다방면사용자락출혈료법(用排針多方面使用刺絡出血療法), 불근용어와과질환(不僅用於外科疾患), 환용어내과질환적지료(還用於內科疾患的治療), 광대료기사용범위(據大了其使用範圍), 사자락출혈료법갱가득도료발전(使刺絡出血療法更加得到了發展), 이동원야재사음화법상(李東桓也在瀉陰火法上), 광법사용료자락출혈료법(廣範使用了刺絡出血療法). 주진형재침자보사상(朱震亨在針刺補瀉上), 야인위침지유사적공효무보적공효(也認爲針只有瀉的功效無補的功效), 주장재사법상사용자락출혈법(主張在鴻法上使用刺絡出血法). 류완소재취혈방면(劉完素在取穴方面), 주장용통경접기법(主張用通經接氣法), 이급접경삼법(以及接經三法), 재통증상용분경취혈법등(在痛症上用分經取穴法等), 래소통경맥적기혈(來疎通經?的氣血). 재임상상중시료정혈(在臨床上重視了井穴), 원혈화오유혈(原穴和五兪穴). 장종정대경락장부지병(張從正對經絡臟腑之病). 상이순경취혈법취경락지정혈(常以循經取穴法取經絡之井穴), 진행자구치료(進行刺灸治療樓). 이동원위보익비위(李東垣爲補益脾胃), 취복적모혈화하합혈(取腹的募穴和下合穴), 이급이허측보기모적방법진행취혈(以及以虛則補其母的方法進行取六), 병이오난침법화표본치료응용오유혈진행료치료(幷以五亂針法和標本治療應用五兪六進行了治療). 주진형보충증입료십이경견증화합생견증(朱震亨補充增入了十二經見症和合生見症), 병이설명료각경락병증특점(幷以說明了各經絡的病症特点), 지출병증적침구치료방법(指出病症的鍼灸治療方法), 류완소준순료중풍분육경침자법화심병적접경삼법(劉完素遵循了中風分六經針刺法和心痛的接經三法).

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2003.11a
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• pp.310-315
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• 2003

This paper described that rotating test and fatigue test of a small-scale hingeless hub system with composite rectangular blades. Generally Rotating stability and fatigue test technique is one of Key-technology on test and evaluation for helicopter rotor system Rotating test of hingeless rotor system was achieved by means of rotor vibration characteristic and aeroelastic stability test GSRTS, equipped with hydraulic actuator and 6-component rotating balance was used to test hingeless rotor system especially for an observation of blade motion including flawing, lagging and feathering. Rotating test was done in hover and forward flight condition. Small-scaled blade fatigue test condition was determined by blade load analysis with the reference table of composite materials(S-N curve). Fatigue test bench was developed for the estimation of blade fatigue life, and tested its characteristic.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2006.05a
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• pp.187-192
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• 2006

Helicopter noise has been considered as one of major design factors like a performance and safety since the public acceptance, comfortability and stealth aspects were important for customers. According to the airworthiness regulation, the noise levels in throe different flight conditions shall comply with the specific limits. Main and tail rotors noise is most dominant in far field due to the low and mid range frequency characteristics. It is an air-born noise so That the accurate aerodynamic data is necessary for the accurate noise prediction. In KARI, low noise main and tail rotors as well as analysis codes have been developed since 2000. The approach for low noise main rotor is a kind of tip modifications, so called twin vortices tip to reduce the BVI noise. Analysis results show the 9.3dB reduction in terms of pseudo EPNL. The uneven spacing concept is applied for low noise tail rotor. Three or four decibel noise reduction is achieved by new optimized uneven spacing. Rotor noise and aerodynamic prediction codes have been improved also.

• Proceedings of the KAIS Fall Conference
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• 2010.05b
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• pp.1237-1240
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• 2010

본 연구에서는 유동층반응기를 이용하여 왕겨의 탄화반응을 수행하였다. 탄화반응은 내경 40mm, 높이 1.8m의 유동층을 사용하였으며, 분산판은 다공성 스테인레스스틸을 사용하였다. 탄화반응은 질소를 이용하여 수행하였다. 왕겨 주입입자 크기는 직경 2.0mm, 0.715mm, 0.359mm, 0.194mm를 각각 사용하였으며, 유동층의 온도는 $400^{\circ}C$, $500^{\circ}C$, $600^{\circ}C$, $700^{\circ}C$에서 탄화특성을 측정하였다. 또한 유동층의 매질로는 직경 1.0mm의 Co-Mo-Fe/$Al_2O_3$ 촉매를 사용하였으며, 탄화물은 유동층상부에 설치된 사이크론에 의하여 포집분리되었다. 탄화시 유동층 내부의 현상을 압력요동을 이용하여 해석하였으며, 압력신호로부터 평균압력, 압력요동의 표준편차, 주진동수, power spectrum density function을 계산하여 층내현상을 해석하였다. 층내온도, 유동화속도, 공급 입자크기에 따른 층내현상을 압력요동특성치를 이용하여 해석할 수 있었다.

• Aerospace Engineering and Technology
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• v.1 no.1
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• pp.1-7
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• 2002

This paper describes the analysis method about the dynamic characteristics and vibratory load through HDS(Helicopter Design Study). To analyze the dynamic characteristics of helicopter rotor blade, the natural frequencies and modes are calculated according to rotor operational speed(Ω). Generally the proximity of rotor natural frequency and N times of rotor operational speed is a dominant component to determine the helicopter vibration. Also we can predict the airframe vibration by calculating the airload of rotating blade exactly. We expect to establish the design procedure of rotor dynamics by describing the two major analysis methods necessary to rotor design.