• Journal of Aerospace System Engineering
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• v.12 no.3
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• pp.70-78
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• 2018

This research was carried out to develop an integrated folding wing made from carbon composite materials. Design requirements were reviewed and composite wing sizing was conducted using design optimization with commercial software. Three composite manufacturing processes including hot-press, pultrusion, and autoclave were evaluated and the most suitable processes for the integrated wing fabrication were selected, with consideration given to performance and cost. The determined manufacturing process was verified by two design development tests for selecting the design concept. Stiffness and strength of the composite wing were estimated through structural analyses. The test loads were calculated and static tests about design limit load and design ultimate load were performed using both wings. As a result, the evaluation criterions of the tests were satisfied and structural safety was verified through the series of structural analyses and testing.

• Composites Research
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• v.25 no.2
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• pp.54-61
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• 2012

In this study, a specific structural design procedure for 2 MW class glass/epoxy composite wind turbine system towers is newly proposed through load case study, trade-off study, optimal structural design and structural analysis. Optimal tower design is very important because its cost is about 20% of the wind turbine system's cost. In the structural design of the tower, three kinds of loads such as wind load, blades, nacelle and tower weight and blade aerodynamic drag load should be considered. Initial structural design is carried out using the netting rule and the rule of mixture. Then the structural safety and stability are confirmed using a commercial finite element code, MSC NASTRAN/PATRAN. The finally proposed tower configuration meets the tower design requirements.

• Proceedings of the Korean Society of Computer Information Conference
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• 2012.01a
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• pp.117-118
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• 2012

본 논문에서는 전자산업공정에서 발생하는 복합오염물질을 측정하고, 분석 관리하는 복합오염물질 분석 관리시스템을 설계하고 구현한다. 이 시스템은 측정기와 분석 및 관리 소프트웨어로 구성된다. 측정기는 복합오염물질을 검출하여 각 오염물질의 수치를 컴퓨터에 전송하는 기능을 제공한다. 분석 및 관리 소프트웨어는 검사, 데이터 관리, 뷰어 등의 모듈로 구성한다. 검사 모듈은 측정기에서 전송된 측정 데이터를 화면에 출력하고, 그 측정 데이터의 정상 기준치 초과 여부를 결정한다. 데이터 관리 모듈은 측정기에서 측정된 방대한 데이터를 데이터베이스에 저장하고 관리하는 기능을 제공한다. 뷰어 모듈은 데이터베이스에 저장된 측정데이터를 그래프 또는 차트 양식으로 출력하는 기능을 제공한다. 본 논문에서 구현한 복합오염물질 분석 관리 시스템은 실제 복합오염물질을 측정하는데 그치지 않고, 그 측정 데이터를 분석하고, 데이터베이스화하여 지속적으로 관리할 수 있는 장점이 있다.

• 한국정보통신설비학회:학술대회논문집
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• 2002.08a
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• pp.137-139
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• 2002

본 논문은 FTTC용 공유급전시스템을 구성하기 위한 광동복합케이블 연구에 관련한 것이다. 광섬유 및 구리 도체를 하나의 케이블에 포함한 복합케이블은 공유급전 시스템에서 포설 비용 절감 및 서비스의 운용 및 유지 보수의 효율 향상을 가능하게 한다. KT 운용시스템연구소의 공유급전 시스템 구성에 따라서 세 가지 type의 광동복합 케이블을 설계하였다. 구리 도체로는 200Vdc 출력 전력을 최대 500m까지 급전을 지원하는 0.65mm 직경의 구리 도체가 선정되었으며 KT 규격을 만족하는 일반 단일모드 광섬유가 적용되었다. 케이블 구조는 다심화에 유리하고 중간분기가 용이한 loose tube형 구조를 채택하였으며, 다심 케이블에서는 stranding된 3층의 집합 코아를 가지도록 설계하였다. 다심의 광동복합케이블은 32심 광섬유와 18페어(pair)의 동선을 실장하여, 두 조의 케이블로 32개의 ONU의 광신호전송 및 전력 공급이 가능하도록 하였다. 또한 포설 및 중간 분기 작업시 광섬유로의 접근이 용이하게 하기 위해 광섬유 튜브를 최외층에 배치하였다. 복합케이블은 상용 loose tube형 광케이블과 동일한 공정으로 제작되었으며, 기계적 및 환경적 특성에서 KT 규격을 만족하는 것을 확인하였다.

• Composites Research
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• v.14 no.3
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• pp.77-89
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• 2001

Since the critical whirling vibration frequency of high speed built-in type motor spindle systems is dependent on the rotor mass of the built-in motor and the spindle specific bending modulus, the rotor and the shaft were designed using magnetic powder containing epoxy and high modulus carbon fiber epoxy composite, respectively. In order to increase the amount of the magnetic flux of the composite squirrel cage rotor of an AC induction motor, a steel core was inserted into the composite rotor. From the magnetic analysis, the optimal configurations of steel core and conductor bars for the dynamic characteristics of the rotor system were determined and proposed. The temperature dependence of composite squirrel cage rotor materials was investigated by various experiments such as TMA, DMA and VSM.

• Journal of Aerospace System Engineering
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• v.11 no.6
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• pp.64-67
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• 2017

This work dealt with structural safety analysis about sandwich composite structure of automotive floor board. In this work, structural design and analysis of sandwich composite structure for automobile floor board were performed. Firstly, structural design requirement of automobile floor board was investigated. After structural design, the structural analysis of the automobile floor board were performed by the finite element analysis method. It was performed that the stress and displacement analysis at the applied load condition. After structural test of target structure, structural test results were compared with analysis results. Through the structural analysis, it was confirmed that the designed floor board structure is safety.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.25 no.3
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• pp.259-266
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• 2012

In this paper the seismic performance of a flat plate wall system structure was evaluated based on the ATC-63 approach, and the results were compared with those of a wall slab structure having the same size. As analysis model structures, a twelve story flat plate wall structure and a wall slab structure were designed based on the KBC-2009, and their seismic performances and collapse behaviors were evaluated by nonlinear static and incremental dynamic analyses(IDA). It was observed that the flat plate wall structure was designed with smaller amount of reinforced concrete, and showed slightly larger displacement response compared with those of the wall slab structure. The collapse margin ratios of the two structures obtained from the incremental dynamic analyses satisfied the limit states specified in the ATC-63, and the structures turned out to have enough capacity to resist the design level seismic load.

• Plant Journal
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• v.8 no.3
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• pp.55-63
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• 2012

This study aims to suggest the improved business process by analyzing the current design process on work flow of the 3D design of power plant, drawing a problems and setting the improving direction through the integration method of the business process reengineering(BPR). In order to realize the improved business process, the integrated design performance system focused on the 3D design was established and accordingly the study analyzed cases of project performances through the integration system and drew the improved effects quantitatively. In the result of the project performance applied with the 3D design integration system, it showed 20.4% design cost saving effect for appropriate rated cost and the integration of design information from each design parts, sub contracters and vendors reduced overlapped works and improved the consistency of repeated design alteration.

• Journal of Aerospace System Engineering
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• v.11 no.4
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• pp.1-7
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• 2017

The development of effective design allowable values for unmanned composite aircraft is an issue of paramount concern for the industry. The application of conventional manned aircraft structural certification methods to unmanned aircraft such as prototype and technology demonstrators, can lead to excessively long development time and costs. In this paper, the determining method of composite structure design allowable values for light composite unmanned aircraft is presented to reduce to the structural weight. This paper seeks to show the applicability of composite B-basis material values as a design allowable of light composite unmanned aircraft structures. A review of different civil and UAV targets failure probability is given. From the results, the researchers can know that the requirements of light composite unmanned aircraft design allowable should be alleviated, compared to manned composite aircrafts.

• The Journal of the Korea Contents Association
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• v.15 no.5
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• pp.18-26
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• 2015

In this paper, we presented a design and control method of multi-stage with wagon and lift stage. Multi-stage system has 4 degree-of-freedom(DOF), i.e., forward/backward/left/right/rotate and up/down motion. Wagon mechanism in the type of two wheel and steering is proposed in order to improve for the maneuverability compared to the existing differential-type wagons. Also, the lift mechanism is designed by interlocking type in order to make the maximum height bigger than 10 times of the original height. We also proposed a path planning algorithm. The performance of the propped system is validated via multi motion experiments, so that the multi-stage system is useful for various performances production.