• 제목/요약/키워드: Weight Reduction Design

검색결과 692건 처리시간 0.028초

구조강도 해석 및 민감도 분석을 이용한 멀티하우스 보트 중량저감 설계 (Multi-house boat weight reduction design using structural strength analysis and sensitivity analysis)

  • 최보엽;손준식;이경환;송창용
    • 해양환경안전학회:학술대회논문집
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    • 해양환경안전학회 2018년도 공동국제학술발표회
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    • pp.193-193
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    • 2018
  • 현재 우리나라는 레저선박 및 중소형 선박, 연안소형어선에 대부분 사용되는 재질은 강도가 높고 내양품성이 우수한 FRP를 사용하고 있다. 하지만 FRP선박의 폐선 시 환경문제와 자원재활용, 선체중량에 연비 및 대기오염등에 의해 소형선박 중심으로 알루미늄선 전환이 이루어지고 있다. 본 연구에서는 알루미늄 선체가 적용된 멀티하우스보트에 알루미늄선 구조기준에 따른 슬래밍하중을 적용하여 구조 강도평가를 실시하였으며, 그 결과를 통해 각 부재별 민감도 평가를 수행하여 알루미늄 구조강도기준을 만족함과 동시에 중량 저감을 하여 실제 선박설계에 적용시키고자 한다.

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고속전철 감속기 케이스의 경량화 설계를 위한 구조해석 (Structural Analysis for Light Weight Design of Reduction Gear Box Case of High Speed Train)

  • 김완두;한승우;임영식;권오웅;박순원
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 1999년도 춘계학술대회 논문집
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    • pp.116-123
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    • 1999
  • A case of the axle gear box which was one of tile power transmission components of high speed train was supported by the bearings installed in axle and the reaction arm connected in bogie frame. Structural analyses of this case were executed for investigation the application of aluminum for weight reduction. The evaluations of the material strength, the thermal strength and deformation, and the stability of natural vibration were carried out according to computer simulation. It was found out that the steel case was safe from the structural failure. For the aluminum case, there was no worry about the vibration resonance and the static failure, but some efforts to reduce tile deformation of the bearing mounting part.

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Propulsion System Modeling and Reduction for Conceptual Truss-Braced Wing Aircraft Design

  • Lee, Kyunghoon;Nam, Taewoo;Kang, Shinseong
    • International Journal of Aeronautical and Space Sciences
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    • 제18권4호
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    • pp.651-661
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    • 2017
  • A truss-braced wing (TBW) aircraft has recently received increasing attention due to higher aerodynamic efficiency compared to conventional cantilever wing aircraft. For conceptual TBW aircraft design, we developed a propulsion-and-airframe integrated design environment by replacing a semi-empirical turbofan engine model with a thermodynamic cycle-based one built upon the numerical propulsion system simulation (NPSS). The constructed NPSS model benefitted TBW aircraft design study, as it could handle engine installation effects influencing engine fuel efficiency. The NPSS model also contributed to broadening TBW aircraft design space, for it provided turbofan engine design variables involving a technology factor reflecting progress in propulsion technology. To effectively consolidate the NPSS propulsion model with the TBW airframe model, we devised a rapid, approximate substitute of the NPSS model by reduced-order modeling (ROM) to resolve difficulties in model integration. In addition, we formed an artificial neural network (ANN) that associates engine component attributes evaluated by object-oriented weight analysis of turbine engine (WATE++) with engine design variables to determine engine weight and size, both of which bring together the propulsion and airframe system models. Through propulsion-andairframe design space exploration, we optimized TBW aircraft design for fuel saving and revealed that a simple engine model neglecting engine installation effects may overestimate TBW aircraft performance.

다단 왕복동 공기압축기의 평형추 설계 (Counter Weight Design of Multi-stage Reciprocating Air Compressors)

  • 김영철;김병옥;신현익
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.656-661
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    • 2003
  • Modem reciprocating air compressors have tendency to a multi-stage W-type or V-type cylinder arrangement for the purpose of high outlet pressure, compactness and low vibration and noise. A valid counter weight calculation method using the complex expression is proposed for reducing the inertia forces of the compressor. Counter weight removes only 1st forward whirl component. Counter weight formulations are applied to the six various compressor structures which are (a) 1 cylinder single-throw crank shaft, (b) 2 cylinder single-throw crank shaft (c) 2 cylinder double-throw clank shaft, (d) 3 cylinder single-throw crank shaft, (e) 4 cylinder single-throw crank shaft and (f) 4 cylinder double-throw crank shaft. The improvement of performance is verified through available vibration test.

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VE 대상선정을 위한 평가항목의 가중치결정방법에 관한 연구 (A Study on the Subject Selection of VE Using Decision Weights Techniques)

  • 윤동진;신병윤;정용식;이상범
    • 한국건축시공학회지
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    • 제5권3호
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    • pp.83-90
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    • 2005
  • Was used at step space-time mainly after VE technique sponsors in domestic in the 1960s but have been expanded to design step recently. Possibility of value elevation or cost reduction must choose member that is effectively for active and effective application of VE technique. In this study, when enforce design VE examining for weight decision corrosion protection been using in weight grant composition estimation technique, target choice process wishes to suggest formality and method that can be achieved effectively Main conclusion of this study sorts valuation items step by step for weight appropriation of valuation basis and give point on article of high position point after expert which employer is included estimates article by low rank step and this presented high position method that do union item by item and establishes by item weight. Did these techniques for giving weights so that importance for weight appropriation developed estimation program, and data save of target estimation standard and target estimation standard is possible using straight sit.

초고속 원심분리 회전축계의 최적설계 (An Optimum Design of a Rotor-Bearing Spindle System for a Ultra Centrifuge)

  • 김종립;윤기찬;박종권
    • 한국정밀공학회지
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    • 제15권6호
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    • pp.145-152
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    • 1998
  • This paper presents an optimum design of a rotor-bearing spindle system for a ultra centrifuge (80,000 RPM) supported by ball bearings with nonlinear stiffness characteristics. To obtain the nonlinear bearing stiffnesses, a ball bearing is modeled in five degrees of freedom and is analyzed quasi-statically. The dynamic behaviors of the nonlinear rotor-bearing system are analyzed by using a transfer-matrix method iteratively. For optimization. we use the cost function that simultaneously minimizes the weight of a rotor and maximizes the separation margins to yield the critical speeds as far from the operating speed as possible. Augmented Lagrange Multiplier (ALM) method is employed for the nonlinear optimization problem. The result shows that the rotor-bearing spindle system is optimized to obtain 9.5% weight reduction and 21% separation margin.

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알루미늄 압출재를 적용한 2층 열차 차체의 기초설계 및 구조강도해석 (The Concept Design and Structural Strength Analysis for Double-Deck Train Carbody using Alluminum Extruded Panels)

  • 황원주;김형진;강부병;허현무
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2002년도 춘계학술대회 논문집
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    • pp.364-369
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    • 2002
  • The purpose of this paper is to introduce the concept design and the structural strength of the double-deck rolling stock vehicle. Aluminum is very useful material for the carbody structure due to its characteristic of light weight. Large alumillum extrusion profiles(panels) have toe of merits such as easy production of complicated shapes, reduction of welding and cutting lines, and cutting down the labor cost. AED type is being applied to the standard EMUs and the EMUs Kwangju subway in Korea. Light material recommended the double-deck rolling stock vehicle because the center of gravity of the train is higher and its weight is heavier than those of the normal vehicle. So we applied the technology of the large aluminum extrusion profiles(panels) to the double-deck vehicle. We performed the structural strength analysis and examined its safety.

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스톤마사지 테라피가 복부비만의 감소에 미치는 영향 (The Effects of Stone Massage Therapy on Abdominal Obesity Reduction)

  • 반소정;김정숙;김지현
    • 한국의상디자인학회지
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    • 제15권4호
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    • pp.17-27
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    • 2013
  • This study has the purpose to examine the effects of stone massage therapy on abdominal obesity reduction. 10 sessions for 5 weeks two times a week of stone massage therapy were offered to 43 adult females who were 40s through 70s with 27% or more of body fat and the results were analyzed. The body composition like body fat mass, fat free mass, weight and skeletal muscular mass etc and the degrees of obesity like body fat ratio abdominal fat ratio were measured and analyzed before and after stone massage therapy. The results are as follows: First, the subjects were obese body type and stone massage therapy produced positive effects with body fat mass, fat free mass, weight and BMI value slightly less than before the therapy. Second, as the average values of body fat ratio and waist hip ratio of subject were significantly different statistically before and after the therapy, stone massage therapy was found to be effective in reducing abdominal obesity. Third, as for the change of waist hip ratio, the therapy was found to be effective in reducing waist hip ratio that 40s decreased insignificantly after the therapy, and 50s and 60s significantly at p<0.05 level respectively from 0.92 to 0.90 and from 0.93 to 0.92. In conclusion, the results of this study indicated that stone massage therapy has positive effects on abdominal obesity reduction, and can contribute to healthy life and well-being culture.

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차량성능을 고려한 최대종단경사 합리화 연구 (Theoretical Review of Highway Grades Considering Vehicle Performances)

  • 김상엽;이승용;한형관;최재성
    • 대한교통학회지
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    • 제25권5호
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    • pp.79-90
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    • 2007
  • 도로의 최대종단경사는 차량의 등판능력에 좌우된다. 과거에 비해 차량의 성능이 좋아질수록 도로의 최대종단경사는 조정될 수 있다. 하지만, 미국(AASHTO, 1990, 2004)에서는 설계기준트럭이 300lb/hp에서 200lb/hp로 성능이 상승했음에도 불구하고, 적용되는 최대 종단경사는 거의 변화가 없다. 따라서, 현재 차량의 성능을 고려한 최대종단경사의 검토 및 조정의 검토가 필요한 실정이다. 특히 국내의 지형은 산악지가 많고, 험준한 지역이 많으므로 실정에 맞도록 최대종단경사의 검토가 필요하다. 본 연구에서는 차량의 성능의 개선과 도로 설계자가 당면한 결정의 문제를 인식하고 세계 각국의 지형과 최대종단경사 적용기준을 비교하여 우리나라의 최대종단경사의 적정성을 확인한다. 또한, 교통시뮬레이션 프로그램을 이용하여 차량의 성능향상에 따른 새로운 트럭 성능곡선을 토대로 최대종단경사를 판단한 결과 $1{\sim}2%$ 정도 종단경사 완화가 가능한 것으로 판단한다.

고고도 장기체공 무인기 구조 설계 및 해석 (Structural Design and Analysis for High Altitude Long Endurance UAV)

  • 김성준;이승규;김성찬;김태욱;김승호
    • 한국항공운항학회지
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    • 제22권3호
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    • pp.68-73
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    • 2014
  • Research is being carried out at Korea Aerospace Research Institute with aim of design a HALE UAV(High Altitude Long Endurance Unmanned Air Vehicle). HALE UAVs are ideally suited to provide surveillance, remote sensing and communication relay capabilities for both military and civilian applications. HALE UAVs typically cruise at an altitude between 15 km and 20 km, travelling at low speed and circling specific area of interest. Airframe structural point of view, weight reduction of the airframe structure is the most important method to improve the flight efficiency. High modulus CFRP(Carbon Fiber Reinforced Polymer) has been used in designing the structure in order to minimize the airframe weight. With respect to structural design and analysis, the key question is to decide an adequate airworthiness certification base to define suitable load cases for sizing of various structural components. In this study, FAR(Federal Aviation Regulation) 23 have constituted the guidance and benchmark throughout all structural studies. And the MSC/FlightLoads was introduced to analyze the flight loads for the HALE UAV. The MSC/FlightLoads can compute the flexible air load and analyzed loads are distributed on structural model directly. A preliminary structural concept was defined in accordance with the estimated inertial and aerodynamic loads. A FEM analysis was carried out using the MSC/Nastran code to predict the static and dynamic behaviour of UAV structure.