• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.66-66
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• 2004

중량은 항공기의 성능을 좌우하는 주요 변수로써, 최소의 중량 달성이 100여 년 전 라이트 형제가 최초의 비행을 성공한 후, 항공기 개발자들의 주요 관심사였다. 일반 구조물의 최적화를 통한 설계는 구조물의 강도를 유지하면서 중량절감, 비용절감을 위해 널리 사용되고 있다. 하지만, 현재 항공기 구조물에 대해서는 아직 최적화론 통한 설계가 널리 적용되지 않고 있다. 그래서, 항공기에서는 중량절감을 위해 가벼우면서 강도를 큰 알루미늄이 주재료로 사용되고 있다.(중략)

• The Hankook-Saengyark Bo
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• no.229
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• pp.5-5
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• 1998

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.1
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• pp.13-20
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• 2022

Aircraft weight is an important factor affecting performance and fuel efficiency. In the conceptual design stage of the aircraft, the process of balancing cost and weight is performed using empirical formulas such as fuel consumption cost per weight in estimating element weight. In addition, when an airline operates an aircraft, it promotes fuel efficiency improvement, fuel saving and carbon reduction through weight management activities. The relationship between changes in aircraft weight and changes in fuel consumption is called the cost of weight, and the cost of weight is used to evaluate the effect of adding or reducing weight to an aircraft on fuel consumption. In this study, the problems of the existing cost of weight calculation method are identified, and a new cost of weight calculation method is introduced to solve the problem. Using Breguet's Range Formula and actual flight data of the A350-900 aircraft, two weight costs are calculated based on take-off weight and landing weight. In conclusion, it was suggested that it is reasonable to use the cost of weight based on the take-off weight and the landing weight for other purposes. In particular, the cost of weight based on the landing weight can be used as an empirical formula for estimating element weight and optimizing cost and weight in the conceptual design stage of similar aircraft.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.26 no.4
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• pp.142-148
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• 2018

In recent years, Korea's aviation industry has been developing rapidly due to the emergence of low-cost airlines. In order to survive in such competition, airlines are making various efforts to save the operation cost as much as possible. Fuel costs account for more than 25% of operating costs. For airlines, reducing aircraft fuel costs is an important part of improving profitability. In this study, analyzing the difference weight between flightplan and W&B Manifest for calculated the fuel that was unnecessarily loaded. As a method to calculate the unnecessary fuel was used by Airbus company flight planning program.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.6
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• pp.389-394
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• 2017

In a conventional ship structure, stiffeners with an asymmetric section, such as inverted angles, are used widely despite the disadvantage of strength compared to the stiffeners with a symmetric section, such as a built-up T. On the other hand, T-type built-up members are attracting more attention than L-type inverted angles due to the increased size of ships. The purpose of this study was to develop an optimal design program for a built-up T, and apply an evolution strategy as an optimization technique. In the optimization process, the gross thickness concept was adopted for the design variables and objective function, and the constraints are set up based on HCSR (Harmonized Common Structural Rules). Using the developed program in this study, the optimal stiffener design was carried out for 300K VLCC and 158K COT of which the orders were obtained lately. The optimal results revealed the weight reduction effect of 144 tons and 60 tons, respectively.

• Journal of the Society of Naval Architects of Korea
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• v.53 no.4
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• pp.336-342
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• 2016

H-CSR(Harmonized Common Structural Rules) integrating CSR-BC(Common Structural Rules for Bulk Carriers) and CSR-OT(Common Structural Rules for Double Hull Oil Tankers) came into effect in July of 2015, so that bulk carrier and double hull oil tanker should comply with this rules. So far, several studies for trend analysis of requirements of structure scantling based on H-CSR have been carried out briskly. However, those studies are rare to apply H-CSR in actual structural design of ships, especially bulk carriers. In this study, an automated system for compartment arrangement is used to search the design case that minimizes still water bending moment(S.W.B.M) in 38k bulk carrier designed by Far East Ship Design & Engineering Co. Ltd. Also, various structural design cases are considered by changing arrangement of structural members to reduce ship weight. The SeaTrust-Hullscan software developed by Korean Register is used to perform structural design of ships based on mother ship and proper design cases are selected by user. The DSA(Direct Strength Analysis) is performed to evaluate structural safety for the yielding and buckling analysis by using MSC Nastran software. The effect of weight reduction is verified by comparison of ship weight between mother ship and the selected design cases.

• Proceedings of the KWS Conference
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• 2010.05a
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• pp.47-47
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• 2010

지구온난화의 심화로 사회적으로 환경의 중요성에 대한 인식이 확산되면서 $CO_2$ 배기가스 및 연비와 직결되어 있는 자동차 중량 절감의 중요성이 강조됨에 따라 차체 경량화 기술은 환경 친화적인 자동차 개발의 핵심기술로 연구되고 있다. 그러나 충돌보호 장치 및 편의장치의 증가로 차체 중량은 지속적으로 증가하고 있어 차체 중량을 혁신적으로 절감할 수 있는 초경량 차체기술이 요구된다. 차체 경량화 방법으로 기존 강재를 알루미늄재로 대체하는 방안이 연구되고 있으며, 일부 해외 고급 차종에서 알루미늄재를 이용한 스페이스 프레임 및 부품 개발을 검토 적용 중이다. 그러나 알루미늄 단일재 사용은 안전성등에서 요구 성능을 만족시키기 어렵기 때문에 강재와 알루미늄재의 적절한 사용이 필요하다. 이를 위하여 강재와 알루미늄간 이종접합부가 발생하며 이를 위한 적정 공정 개발이 필요하다. 전자기 펄스 용접(MPW)은 고상접합의 한 종류로서 고전류를 순간적으로 방전하여 발생된 고에너지를 통하여 접합이 이루어진다. 이러한 고에너지는 외부재의 전 자기적 성질에 의하여 에너지량이 결정되므로 외부재의 전도도(conductivity)는 매우 중요하며 이러한 이유로 Aluminum 1xxx계 중심의 전자기 펄스 용접 공정이 연구되었다. 그러나 자동차 스페이스 프레임 및 드라이브 샤프트등과 같은 부품에 알루미늄재를 적용하기 위해서는 일정 강도를 확보할 수 있는 6xxx계의 관련 연구가 필요하다. 따라서 본 연구에서는 고품질의 접합부 확보를 위한 1xxx계와 6xxx의 최적의 공정변수(충전전압, 외부재와 내부재 사이의 간격, 외부재 두께)를 도출하였다. 이를 위하여 전자기 펄스 용접 장치는 한국생산기술연구원과 웰메이트(주)에서 공동으로 개발한 $120{\mu}F$의 캐패시터 6개로 구성된 'W-MPW36'을 사용하였으며 접합 후 누수시험을 통하여 접합부의 품질을 검토하였다.

• Journal of the Society of Naval Architects of Korea
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• v.54 no.4
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• pp.352-359
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• 2017

Because the Energy Efficiency Design Index(EEDI) came into effect in 2013, it is necessary to develop a new technology to overcome $CO_2$ emission regulations. In structural design viewpoint, lots of researches are carried out to develop eco-friendly and high fuel efficiency ships by weight reduction. By using the automated compartment arrangement system and automated structural design algorithm which were developed by the authors, new researches are performing to combine the above two systems. However, the effect of weight reduction was not significant because structural designs by using these systems for the midship part was carried out only focused on the minimum still water bending moment. In this paper, at first, good compartment arrangements which give the minimum still water bending moment and(or) shear force were chosen by using the automated compartment system. And then, influence of shear force on weight reduction was investigated by using the automated structural design algorithm considering longitudinal strength, local strength and shear strength of longitudinal members in cargo holds. Conclusively, it is necessary to consider the minimum still water bending moment and shear force simultaneously to reduce the weight of mid-sized bulk carrier. Also, good compartment arrangement which gives much more weight reduction compared with existing ship was proposed.

• Bulletin of the Society of Naval Architects of Korea
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• v.26 no.3
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• pp.62-70
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• 1989

For the conduct of optimum design for such complicated and large structures as ship structure by direct structural analysis such as finite element method, it is very important problem that the process needs much computational efforts due to the repeated structural analysis. In this study, the reanalysis technique based on the modified reduced basis method is applied in the process to reduce the computing time required in repeated structural analysis. Numerical examples to simple grillage and actual ship structure are performed and applicability of reanalysis technique to structural optimization process is discussed.

• Proceedings of the KIPE Conference
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• 2012.07a
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• pp.174-175
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• 2012

철도 분야에서도 환경 보호 및 에너지 절감을 위한 경량화 연구가 활발히 진행 되고 있다. 본 논문에서는 철도차량의 보조전원장치 경량화에 대해 설명 한다. 기존의 철도차량의 보조전원 장치는 내부 필터 리액터, 변압기 등이 중량의 상당한 부분을 차지 하고 있고, 이는 시스템 중량 저감을 위한 고민에서 가장 큰 위치를 차지 한다. 본 논문에서는 공진형 컨버터를 사용하고 스위칭 주파수를 높여 필터 리액터, 변압기 등을 경량화 하였다. 150kW급 시제품에 대한 모의해석과 실험을 통해 입증 하였다.