• 한국식품영양학회지
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• 제15권4호
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• pp.364-369
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• 2002

방선균은 토양 속에 다양하게 존재하는 미생물의 일종으로 그람 양성 진정세균으로 이차대사산물을 생산하는 시기와 포자 착생이 시작되는 세포분화의 시기가 밀접한 관련이 있다. S. griseus는 streptomycin을 비롯한 다양한 종류의 endopeptidase 및 exopeptidase들을 생산한다. 방선균에서의 protease 생산은 많은 경우에 이차대사산물이 형성되거나 형태분화가 유도되는 시기에 동시에 시작된다는 점에서 Pretense가 이차대사물질 생산 및 세포분화에 일정한 기능을 수행할 것이 라는 점을 시사하고 있다. 본 연구에서는 S. griseus IFO 13350에서 클로닝한 SGPD protease가 각 strain에서 형태학적으로나 생리적으로 어떠한 gene dosage 효과를 미치는지 조사하는 것이었다. sprD 유전자가 S.lividans를 숙주로 사용한 시스템에서 대량발현이 성공적으로 되는 것을 확인한 후, 본 유전자를 클로닝한 S. griseus IFO13350 균주와 이의 A-factor 결손주인 S. griseus HH1에 형질전환하였다. S. griseus HH1과 S. griseus IFO13350에서는 protease activity가 벡터만 도입된 대조군과 sprD 유전자가 들어간 형질전환체에서 큰 차이를 보이지 않았다. 또한 S. griseus IFO 13350 및 HH1 모두에서 생리학적·형태학적 분화의 차이를 발견하지 못하였다. Chymotrypsin계열의 pretense를 암호화하는 유전자만이 S. griseus에서 발현이 repression된다는 사실을 본 연구 결과를 통하여 알게 되었다. 이를 바탕으로 sprD유전자와 동일계열의 chymotrypsin 계열의 유전자들이 공통적으로 S. griseus에서 repression 되는 일반적인 기전이 있을 것으로 판단, chymotrypsin계열 유전자들의 promoter부분의 염기 상동성을 조사하였다 번역개시부위 바로 상부 유전자부터 상동성을 조사한 결과 적어도 상당부분의 염기배열이 잘 보존된 지역이 존재함을 알게 되었다. 향후 이들 발현기구의 조절기구를 연구함으로서 protease의 기능을 밝히는데 좋은 단서를 제공할 것으로 판단된다.

• Wind and Structures
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• 제30권4호
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• pp.433-450
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• 2020

The strong turbulence characteristic of typhoon not only will significantly change flow field characteristics surrounding the large-scale wind turbine and aerodynamic force distribution on surface, but also may cause morphological evolution of coast dune and thereby form sand storms. A 5MW horizontal-axis wind turbine in a wind power plant of southeastern coastal areas in China was chosen to investigate the distribution law of additional loads caused by wind-sand coupling movement of coast dune at landing of strong typhoons. Firstly, a mesoscale Weather Research and Forecasting (WRF) mode was introduced in for high spatial resolution simulation of typhoon "Megi". Wind speed profile on the boundary layer of typhoon was gained through fitting based on nonlinear least squares and then it was integrated into the user-defined function (UDF) as an entry condition of small-scaled CFD numerical simulation. On this basis, a synchronous iterative modeling of wind field and sand particle combination was carried out by using a continuous phase and discrete phase. Influencing laws of typhoon and normal wind on moving characteristics of sand particles, equivalent pressure distribution mode of structural surface and characteristics of lift resistance coefficient were compared. Results demonstrated that: Compared with normal wind, mesoscale typhoon intensifies the 3D aerodynamic distribution mode on structural surface of wind turbine significantly. Different from wind loads, sand loads mainly impact on 30° ranges at two sides of the lower windward region on the tower. The ratio between sand loads and wind load reaches 3.937% and the maximum sand pressure coefficient is 0.09. The coupling impact effect of strong typhoon and large sand particles is more significant, in which the resistance coefficient of tower is increased by 9.80% to the maximum extent. The maximum resistance coefficient in typhoon field is 13.79% higher than that in the normal wind field.

• 한국산학기술학회논문지
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• 제12권4호
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• pp.1824-1832
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• 2011

본 논문에서는 스마트 홈 서비스 로봇인 맥봇II(Mess-Cleanup Robot; McBot II)를 설계한다. 그것은 맥봇I에 비하여 더욱 지능적이고 실용적인 시스템으로 개발하였다. 지금까지 진공청소기는 가사 노동의 부담을 덜어주었지만 진공청소기를 운용하는 점에서 노동의 강도는 차이가 없다. 최근에 이 문제의 해결을 위해 상용화된 청소로봇이 나왔지만 큰 시장을 형성하지는 못했다. 왜냐하면 여전히 진공청소 이전에 큰 부피의 쓰레기나 신문, 옷가지 등을 정리정돈 하지 못하는 문제를 가지고 있다. 따라서 우리는 실제 환경에서 이 문제를 해결하기 위해 더 발전된 새로운 정리정돈 로봇 맥봇II를 개발한다. 특히, 본 논문에서는 로봇의 기계적인 설계와 기본적인 제어에 초점을 맞추어 논문을 구성한다. 맥봇II는 인간이 허리 및 손을 이용하여 정리 정돈 작업을 수행하는 메커니즘을 모델로 하여 설계되어 진다. 작업 시 인간의 허리 기능은 변화 범위가 큰 수직형 리프트와 전후진이 가능한 어깨 조인트 구조로 구현한다. 정리정돈 작업을 직접 수행하는 로봇 팔과 핸드는 실용성을 위하여 최소 자유도를 갖는 시스템으로 설계한다. 또한 맥봇II가 좁은 면적의 실내에서 장애물과의 충돌을 방지하면서 고속의 이동 능력을 갖기 위하여 홀로노믹(Holonomic)특성의 이동로봇으로 설계한다. 끝으로 최적화 설계로 구현된 로봇의 몸체/이동/로봇팔/핸드의 동작 제어 실험 결과들을 통하여 맥봇 II의 향상된 성능을 확인한다.

• 한국재료학회지
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• 제7권3호
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• pp.175-179
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• 1997

고밀도 고기능 전자기기의 발전과 고주파 이동통신의 증대에 따라 전자소자의 소형화, 집적화가 요구되고 있으며, 이는 전자소자의 박막화를 필요로 한다. 캐패시터, 인덕터는 전기 회로를 구성하는 기본적인 소자로서 그 응용 범위는 무수히 많으며, 따라서 이들 소자의 박막화는 전자소자의 소형화, 경량화에 큰 영향을 끼치리라 생각된다. 본 연구에서는 강자성 및 강유전 산화물 박막을 이용하여 인덕터, 캐터시터, LC 복합소자를 제조하였다. 고온 산화분위기에서 안정한 Au를 리프트 오프법으로 금속배선 패턴을 향상하였고, 스퍼터링, 화학기상증착법 등을 이용하여 산화물 박막을 증착하였다. 0.5-15GHz에서 network analyzer로 측정하고 Microwave Design System으로 분석한 결과 5nH의 인덕턴스, 10,000pF의 캐패스턴스, $10^{6}-10^{9}Hz$ 정도의 공진 주파수 값을 얻었다.

• 항공우주정책ㆍ법학회지
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• 제5권
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• pp.101-118
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• 1993

Generally there is no law and liability system which applies particulary to commercial space ventures. There are several international treaties and national statutes which deal with space ventures, but their impact on the liability of commercial space ventures has not been significant. Every state law in the United States will impose both tort and contract liability on those responsible for injuries or losses caused by defective products or by services performed negligently. As with the providers of other products and services, those who participate in commercial space ventures have exposure to liability in both tort and contract which is limited to the extent of the resulting damage The manufacturer of a small and cheap component which caused a satellite to fail to reach orbit or to operate nominally has the same exposure to liability as the provider of launch vehicle or the manufacturer of satellite into which the component was incorporaded. Considering the enormity of losses which may result from launch failure or satellite failure, those participated in commercial space ventures will do their best to limit their exposure to liability by contract to the extent permitted by law. In most states of the United States, contracts which limit or disclaim the liability are enforceable with respect to claims for losses or damage to property if they are drafted in compliance with the requirements of the applicable law. In California an attempt to disclaim the liability for one's own negligence will be enforceable only if the contract states explicitly that the parties intend to have the disclaimer apply to negligence claims. Most state laws of the United States will refuse to enforce contracts which attempt to disclaim the liability for gross negligence on public policy grounds. However, the public policy which favoured disclaiming the liability as to gross negligence for providers of launch services was pronounced by the United States Congress in the 1988 Amendments to the 1984 Commercial Space Launch Act. To extend the disclaimer of liability to remote purchasers, the contract of resale should state expressly that the disclaimer applies for the benefit of all contractors and subcontractors who participated in producing the product. This situation may occur when the purchaser of a satellite which has failed to reach orbit has not contracted directly with the provider of launch services. Contracts for launch services usually contain cross-waiver of liability clauses by which each participant in the launch agrees to be responsible for it's own loss and to waive any claims which it may have against other participants. The crosswaiver of liability clause may apply to the participants in the launch who are parties to the launch services agreement, but not apply to their subcontractors. The role of insurance in responding to many risks has been critical in assisting commercial space ventures grow. Today traditional property and liability insurance, such as pre-launch, launch and in-orbit insurance and third party liability insurance, have become mandatory parts of most space projects. The manufacture and pre-launch insurance covers direct physical loss or damage to the satellite, its apogee kick moter and including its related launch equipment from commencement of loading operations at the manufacture's plant until lift off. The launch and early orbit insurance covers the satellite for physical loss or damage from attachment of risk through to commissioning and for some period of initial operation between 180 days and 12 months after launch. The in-orbit insurance covers physical loss of or damage to the satellite occuring during or caused by an event during the policy period. The third party liability insurance covers the satellite owner' s liability exposure at the launch site and liability arising out of the launch and operation in orbit. In conclusion, the liability in commercial space ventures extends to any organization which participates in providing products and services used in the venture. Accordingly, it is essential for any organization participating in commercial space ventures to contractually disclaim its liability to the extent permitted by law. To achieve the effective disclaimers, it is necessary to determine the applicable law and to understand the requirements of the law which will govern the terms of the contract. A great deal of funds have been used in R&D for commercial space ventures to increase reliability, safety and success. However, the historical reliability of launches and success for commercial space ventures have proved to be slightly lower than we would have wished for. Space insurance has played an important role in reducing the high risks present in commercial space ventures.