• 한국지능정보시스템학회:학술대회논문집
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• 한국지능정보시스템학회 2001년도 The Pacific Aisan Confrence On Intelligent Systems 2001
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• pp.249-255
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• 2001

Different kinds of information are used when solving tasks that arise in the life cycle of an applied knowledge based system (KBS). Many of these tasks are still under investigation. Their solving methods are often researched independently of each other due to complexity of the tasks. As a result, systems that realize these methods turn out to be incompatible and therefore could not be used together in the lifecycle of a KBS. The following problem arises here: how to support the full life cycle of a KBS. This paper introduces a class of computer knowledge banks that are intended to support the full life cycle of KBSs. Primary tasks that arise in the full life cycle of a KBS are analyzed. The architecture of a knowledge bank of the introduced class is presented, including an Information Content, a Shell of the Information Content and a Software Content. General requirements on these components are formulated on the basis of the analysis. These requirements depend on the current state of understanding in the life cycle of KBSs.

• 전기전자학회논문지
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• 제23권4호
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• pp.1208-1217
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• 2019

풀-브리지 서브모듈은 MMC의 단위 시스템으로서 서브모듈에 대한 수명예측은 HVDC 시스템의 유지 보수와 경제성 확보 관점에서 매우 중요하다. 그러나 일반적으로 부품의 종류, 개수, 결합 상태만을 고려하는 수명 예측은 대상 시스템의 구동상태를 고려하지 않는 일반화 된 결과로 실제 시스템의 수명과 크게 차이가 발생할 수 있다. 따라서 본 논문에서는 풀-브리지 서브모듈의 동작 특성을 반영하기 위한 목적으로 고장나무를 설계하고 기본 사상의 고장률에 MIL-HDBK-217F를 적용하여 풀-브리지 서브모듈의 수명을 예측한다. 기존의 부품고장률 분석과 제안된 고장나무 분석에 의한 기대 수명을 비교하고, 풀-브리지 서브모듈의 여유율 적용 여부에 따른 수명을 비교한다.

• 대한전자공학회논문지
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• 제15권3호
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• pp.7-10
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• 1978

이 논문은 single transistor를 사용하여 정현파를 전파정류하는 한 방법을 검토한다. switching으로 동작되는 inverter에 R-feed back을 하고 최적 parameter를 설정하므로써 도통상태의 반파와 cut-off 상태에서 feed back을 통한 반파를 합성하여 전파정류의 출력을 얻는다. cassette deck의 code재생 system에 이용한 바 효과적이었고, AGC 등에 이용 가능하다.

• 대한전자공학회논문지SD
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• 제47권5호
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• pp.1-9
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• 2010

이 논문에서는, 풀 HD 영상을 실시간에 처리가능한 새로운 화면 내 예측 및 DCTQ 하드웨어구조를 제안한다. 화면내 예측,.$4{\times}4$ 을 처리하기 위한 예측과 변환, 양자화, 역양자화, 역변환및 복원의 전체 cycle 을 줄일 수 있는 방법을 제안한다. $4{\times}4$ 예측 부호화 cycle을 줄이기 위해, 양자화과정을 예측 사이클에서 적용할 수 있도록 하였으며, 회로의 크기를 줄이기 위하여 9가지 모드 중 2개의 모드를 먼저 선택하는 알고리듬을 사용하였다. 또한 $16{\times}16$ 예측과 $8{\times}8$ 예측 과정를 하나의 코어를 이용하여 설계하므로 크기를 줄였다. 제안된 구조는 108Mhz 클럭에서 full HD영상을 30frame/sec에서 동작하며, 한 매크로블록의 처리 cycle 은 425 cycle이다.

• Nuclear Engineering and Technology
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• 제29권4호
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• pp.299-309
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• 1997

The neutronic feasibility of typical Korean three-loop 900MWe class PWR core loaded with mixed oxide fuels for both annual and 18-month cycle strategies has been investigated as a means for spent fuel management. For this study, a method of determining equivalent plutonium content was developed under the equivalence concept which gives the same cycle length as uranium fuel. Optimal plutonium zoning within the MOX assembly was also designed with the aim of minimizing the peak md power. Conceptual core designs hate hen developed for equilibrium cycle with the following variations: annual and 18-month cycle, 1/3 and full MOX loading schemes, and typical and high moderation lattice. The analysis of key core physics parameters shows that in all cases considered satisfactory core designs seem to be feasible, though addition of control rod system and change in Technical Specification for soluble boron concentration are required for full MOX loading in order to meet the current design requirements.

• 한국추진공학회지
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• 제25권5호
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• pp.53-64
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• 2021

SpaceX사는 Falcon 9으로 발사체 비용을 혁신적으로 낮추었으며 로켓의 1단 재사용을 실용화하였다. 현재는 완전 재사용이 가능하고 탑재량이 가장 큰 Starship 시스템을 개발 중이며 이로 인해 더욱 저렴한 비용의 발사와 임무의 다양화가 가능하다. 이를 위해 최초로 메탄 연료를 사용하는 전유동 다단 연소 싸이클을 사용하는 Raptor 엔진을 완성하였다. 그리고 완전 재사용을 위해 스테인리스강 탱크, 하강 중 배면낙하 및 역추진과 같은 거의 사용되지 않는 기술들을 함께 적용하여 다수의 시제기를 제작 및 시험하고 있다. 여기서는 Starship 시스템의 제원, 임무, 설계 특징에 대해 알아보았다. 또한 Raptor 엔진과 매우 빠르게 제작된 초기 13 기의 Starship 시제기 개발 과정에 대해서도 알아보았다.

• 시스템엔지니어링워크숍
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• 통권4호
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• pp.17-22
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• 2004

This paper present the brief generation process of system requirements or mart UAV from a development obejective. The current Snart UAV requirements deal with the restricted life cycle from development to test and verification exclusive of full life cycle beacuse of the new technology demonstration research program funded by goverments. The Smart UAV system consists of flight vechicle, avionics, communication link, payload, ground control stationand ground supporting system. In thus paper, top-down flown requirememts are intoduced how to allocate to each sub-system.

• 한국경영과학회:학술대회논문집
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• 한국경영과학회 2006년도 추계학술대회
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• pp.618-629
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• 2006

This Paper is about optimizing preventive maintenance period of connected (r,s) out of(m,n) : F lattice system that one of multi-component system, (m,n) matrix failure of whole system is occurrence when parts that belong in (r,s) matrix part procession of parts arranged with procession are breakdown all. The preventive maintenance about system is very important viewing from system reliability and operational expense viewpoint. Preventive maintenance that misses a time calls big loss by system failure and expense of frequent full equipment is paid excessively in preventive maintenance itself but expense is paid much in preventive maintenance itself and whole expense escalation can be achieved preferably. Through this research, reliability model is constructed that do expense by smallest under full equipment policy chosen through comparison of each full equipment policy and preventive maintenance expense full equipment cycle and r ,s value are made using simulated annealing algorithm and simulated annealing algorithm that converge fast in multi-component system certified most suitable to optimization decision

• International Journal of Automotive Technology
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• 제6권5호
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• pp.513-517
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• 2005

A full-bead of multi-layer-steel engine head gasket, taking charge of the dynamic sealing of combustion chamber, is susceptible to fatigue failure. The fatigue durability of full-bead was assessed with the finite element analysis results and the high-cycle multi-axial fatigue theory. The assessment aimed to reveal the effects of the forming parameters and dimensions of full-bead. The results show that the selection of embossing parameters producing less deformation of bead plate is beneficial for the improvement of durability while the flatting has marginal influence. The fatigue durability also improves with the increase in the width of full-bead and the radial length of bore-side flat region. However, the dimensional effects are limited due to the occurrence of snap-through.

• 한국초전도ㆍ저온공학회논문지
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• 제5권2호
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• pp.58-65
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• 2003

The high temperature superconductivity(HTS) cable must be cooled below the nitrogen liquefaction temperature to applicate the cable in power generation and transmi-ssion system under the superconducting state. To obtain superconducting state. a reliable cryocooler system is required. Structural and thermal design have been performed to design cryocooler system operated with reverse Brayton cycle using gas neon as refrigerant. This cryocooler system consists of compressor. recuperator. coldbox. control valves and has 1 kW cooling capacity. Heat loss calculation was conducted for the given cryocooler system by considering the conduction and radiation through the multi-layer insulation(MLI) and high vacuum. The results can be summarized as: conduction heat loss is 7 W in valves and access port and radiation heat loss is 18 W through the surface of cryocooler. The full design specifications were discussed and the results were applied to construct in house HTS cable cooling system.