• Title/Summary/Keyword: Aluminum Sandwich Panel

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A Study on The Load Test Method and Result For AL Car Body of LRT (경량전철차량 알루미늄 구조체 하중시험방법 연구 및 결과고찰)

  • Kim, Won-Kyung;Won, Si-Tae;Jeon, Chang-Sung
    • Proceedings of the KSR Conference
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    • 2008.06a
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    • pp.986-995
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    • 2008
  • This study introduces the testing results of the AL car body which is applied to LRT. The LRT car body is made of aluminum structure materials like a sandwich panel. The static load test was performed to evaluate the structural characteristic and stability of the AL car body. Considering the vertical, compressive, twisting load and 3-point supporting, Bend natural frequency Measurement, Twist natural frequency Measurement type as a testing terms, the structural stability of a car body was evaluated.

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A Study on Comparison Of The load Test Results Of AL Car Body Welding Method For Rolling Stock (철도차량 알루미늄 차체 용접방법에 따른 하중시험결과 비교 고찰)

  • Kim, Weon-Kyong;Won, Si-Tae;Jeon, Chang-Sung
    • Proceedings of the KSR Conference
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    • 2009.05a
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    • pp.1604-1612
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    • 2009
  • This study introduces comparison the testing results of the AL car body which is applied to FSW and GMAW welding method. The car body is made of aluminum structure materials like a sandwich panel. The static load test was performed to evaluate the structural characteristic and stability of the AL car body. Considering the vertical, compressive, twisting load and 3-point supporting, Bend natural frequency Measurement, Twist natural frequency Measurement type as a testing terms, the structural stability of a car body was evaluated.

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Structural Analysis for VVIP Cabin Compartment Modification STC of Commercial Airplane

  • Lee, Sang Hoon;Bang, Dae Han;Choi, Sang Min;Choi, Hang Suk
    • Journal of Aerospace System Engineering
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    • v.15 no.4
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    • pp.30-39
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    • 2021
  • This paper presents a study on the design and structural substantiation of the interior structure of the new VVIP aircraft. In this study, the structural design and analysis of the compartment with aluminum alloy and sandwich composite panel were performed. The structural design requirements from the Federal Aviation Administration were identified. The structural analysis of the compartment was performed by the utilization of the finite element analysis method, for the structural design process. Therefore, the designed cabin compartment secured the structural integrity, and satisfied its certification standards and design requirements via structural analysis.

The Real Scale Fire Tests for Vertical Fire Spread Study of External Finishing Material (외벽 마감재료의 수직화재 확산 연구를 위한 실물화재 실험)

  • Kweon, Oh-Sang;Yoo, Yong-Ho;Kim, Heung-Youl;Kim, Jung-Hyun;Min, Se-Hong
    • Fire Science and Engineering
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    • v.26 no.6
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    • pp.85-91
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    • 2012
  • To reduce human life and property damage at the fire in a building, it is most critical to control flame spread in the early stage. Fire spread prevention measure generally includes fire resistance performance securing of structure member in the arson zone and use limitation based on combustion performance of finishing material. The latter is most fundamental fire safety design to determine flame spread, but domestic combustion test determines combustion performance by specimen sized fire test method. Thus, there are many restrictions in the determination of combustion performance by composite material such as sandwich panel. Especially, outer finishing material uses a variety of composite material such as dry bit, aluminum composite panel, and metal panel compared to inner finishing material. Therefore, this study would determine vertical fire spread features by a full scaled fire experiment through the test method of ISO 13785-2, an international test standard.

A Study on the Minimum Weight Design of Stiffened Cylindrical Shells (보강원통셸의 최소중량화설계 연구)

  • 원종진
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.4
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    • pp.630-648
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    • 1992
  • The minimum weight design for simply-supported isotropic or symmetrically laminated stiffened cylindrical shells subjected to various loads (axial compression or combined loads) is studied by a nonlinear mathematical search algorithm. The minimum weight design in accomplished with the CONMIN optimizer by Vanderplaats. Several types of buckling modes with maximum allowable stresses and strains are included as constraints in the minimum weight design process, such as general buckling, panel buckling with either stingers or rings smeared out, local skin buckling, local crippling of stiffener segments, and general, panel and local skin buckling including stiffener rolling. The approach allows the consideration of various shapes of stiffening members. Rectangular, I, or T type stringers and rectangular rings are used for stiffened cylindrical shells. Several design examples are analyzed and compared with those in the previous literatures. The unstiffened glass/epoxy, graphite/epoxy(T300/5208), and graphite/epoxy aluminum honeycomb cylindrical shells and stiffened graphite/epoxy cyindrical shells under axial compression are analyzed through the present approach.

Study on Weight Reduction of Urban Transit Carbody Based on Material Changes and Structural Optimization (도시철도차량 차체의 경량화를 위한 소재 변경 및 구조체 최적화 연구)

  • Cho, Jeong Gil;Koo, Jeong Seo;Jung, Hyun Seung
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.9
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    • pp.1099-1107
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    • 2013
  • This study proposes a weight reduction design for urban transit, specifically, a Korean EMU carbody made of aluminum extrusion profiles, according to size optimization and useful material changes. First, the thickness of the under-frame, side-panels, and end-panels were optimized by the size optimization process, and then, the weight of the Korean EMU carbody could be reduced to approximately 14.8%. Second, the under-frame of the optimized carbody was substituted with a frame-type structure made of SMA 570, and then, the weight of the hybrid-type carbody was 3.8% lighter than that of the initial K-EMU. Finally, the under-frame and the roof-panel were substituted with a composite material sandwich to obtain an ultralight hybrid-type carbody. The weight of the ultralight hybrid-type carbody was 30% lighter than that of the initial K-EMU. All the resulting carbody models satisfied the design regulations of the domestic Performance Test Standard for Electrical Multiple Unit.

Study on Application of Ultrasonic Propagation Imager for Non-destructive Evaluation of Composite Lattice Structure (복합재 격자 구조 비파괴평가를 위한 초음파전파 영상화 시스템 활용 연구)

  • Park, Jae-Yoon;Shin, Hye-Jin;Lee, Jung-Ryul
    • Composites Research
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    • v.30 no.6
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    • pp.356-364
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    • 2017
  • Composite lattice structures are tried to be used in various fields because of its benefit in physical properties. With increase of demand of the composite lattice structure, nondestructive testing technology is also required to certificate the quality of the manufactured structures. Recently, research on the development of the composite lattice structure in Republic of Korea was started and accordingly, fast and accurate non-destructive evaluation technology was needed to finalize the manufacturing process. This paper studied non-destructive testing methods for composite lattice structure using laser ultrasonic propagation imaging systems. Pulse-echo ultrasonic propagation imaging system was able to inspect a rib structure wrapped with a skin structure. To reduce the time of inspection, a band divider, which can get signal in different frequency bands at once, was developed. Its performance was proved in an aluminum sandwich panel. In addition, to increase a quality of results, curvature compensating algorithm was developed. On the other hand, guided wave ultrasonic propagation imaging system was applied to inspect delamination in a rib structure. To increase an area of inspection, multi-source ultrasonic wave propagation image was applied, and defects were successfully highlighted with variable time window amplitude mapping algorithm. These imply that ultrasonic propagation imaging systems provides fast and accurate non-destructive testing results for composite lattice structure in a stage of the manufacturing process.

An Experimental Study on the Pore Structure and Thermal Properties of Lightweight Foamed Concrete by Foaming Agent Type (기포제 종류에 따른 경량기포콘크리트의 기포구조 및 열적특성에 관한 실험적 연구)

  • Kim, Jin-Man;Choi, Hun-Gug;Park, Sun-Gyu
    • Journal of the Korea Institute of Building Construction
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    • v.9 no.4
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    • pp.63-73
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    • 2009
  • Recently, the use of lightweight panels in building structures has been increasing. Of the various lightweight panel types, styrofoam sandwich panels are inexpensive and are excellent in terms of their insulation capacity and their constructability. However, sandwich panels that include organic material are quite vulnerable to fire, and thus can numerous casualties in the event of a fire due to the lack of time to vacate and their emission of poisonous gas. On the other hand, lightweight foamed concrete is excellent, both in terms of its insulation ability and its fire resistance, due to its Inner pores. The properties of lightweight concrete is influenced by foaming agent type. Accordingly, this study investigates the insulation properties by foaming agent type, to evaluate the possibility of using light-weight foamed concrete instead of styrene foam. Our research found thatnon-heating zone temperature of lightweight foamed concrete using AP (Aluminum Powder) and FP (animal protein foaming agent) are lower than that of light-weight foamed concrete using AES (alkyl ether lactic acid ester). Lightweight foamed concrete using AES and FP satisfied fire performance requirements of two hours at a foam ratio 50, 100. Lightweight foamed concrete using AP satisfied fire performance requirements of two hours at AP ratio 0.1, 0.15. The insulation properties were better in closed pore foamed concrete by made AP, FP than with open pore foamed concrete made using AES.