• Title/Summary/Keyword: 구조재

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Structural Test Analysis Study for Manufacturing of Flax Fiber Composite Blades for 30kW Wind Turbines (30kW 풍력터빈용 아마섬유 복합재 블레이드 제조를 위한 구조 시험 분석 연구)

  • Hye-Jin Shin;Ji-Hyun Lee;Sung-Young Moon;Jounghwan Lee
    • Composites Research
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    • v.36 no.1
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    • pp.32-36
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    • 2023
  • Recently, as global environmental issues for sustainable development, such as carbon neutrality, have emerged, disposal methods of glass fiber composites, a material of existing wind turbines, have become a problem. To solve this problem, in this study, 30kW wind turbine blades were manufactured using flax fiber-based composites, which are eco-friendly natural fiber composites that can replace existing glass fiber composites, and their suitability was evaluated. First, mechanical strength tests were conducted to verify the feasibility of using eco-friendly natural flax fiber composites as a wind turbine blade material, and as a result, better strength were confirmed compared to previous studies on the properties of flax fiber composites. In addition, the suitability was confirmed through a static strength performance evaluation test to measure the static strength of the flax fiber composite blade using the manufactured 30kW class flax fiber composite blade.

Fatigue Behavior of Reinforced Concrete Beams Externally Strengthened using FRP Tendons (FRP 긴장재로 외부 보강된 철근콘크리트 보의 피로거동)

  • Park, Sang Yeol;Hong, Sung Ryong;Kim, Chang Hoon
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.28 no.6A
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    • pp.809-817
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    • 2008
  • Recently, the external prestressing method is being much frequently used in strengthening reinforced concrete structures because of it's excellent load resistance and serviceability increases comparing to other strengthening methods. However, it is true that the research on fatigue performance of concrete structures strengthened by the external prestressing using FRP tendons is rare. Therefore, the purpose of this study is to evaluate the safety and feasibility of the external prestressing method by analyzing the characteristics of the reinforced concrete beam strengthening using FRP tendons under repeated loads. Test variables adopted in this experimental study are the types of external prestressing material (steel or FRP tendon) and the repeated load ranges. The repeated load range have the minimum 50% of yield load of reinforced concrete beam and the maximum 70-85%. The test beams are loaded by 4 point loadings with 3 Hz sine wave. From this experimental study, it is confirmed that the reinforced concrete beams strengthened using FRP tendons have sufficient safety against fatigue, especially in FRP tendon itself, tendon at deviators and tendon at anchorages.

Numerical Analysis and Verification of Sound Absorbing Properties of Perforated Plate (타공판의 등가 흡음 물성치 유도와 공명기로서의 흡음성능 해석)

  • Yoon, Gil-Ho;Kim, Ki-Hyun;Choi, Jung-Sik;Yun, Su-Hwan
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.28 no.2
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    • pp.139-144
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    • 2015
  • Recently, to realize sound-absorbing structures, we have to insert sound-absorbing materials into wall. These shapes are taken limitations because sound-absorbing materials should be fixed. Therefore, the sound absorption is changed by environment that used the sound-absorbing materials. On the other hand, we will take same effect without sound-absorbing material, if we change the shape of wall to sound absorbing structure. If we use this sound absorbing structure, we can get benefits by removing limitation of materials. Therefore we suggest perforated plate for effective sound-absorbing structure. We confirmed the function of sound-absorption of this structure using equivalent property. Then, we found the similarity between perforated plate and resonator. Also, we verify these theories through computer simulation by FEM(Finite Element Method). Finally, we validated that perforated plate has function of sound absorption without sound-absorbing material. This perforated plate is used for sound-absorbing material of buildings and transportations such as vehicle, train etc. Also, these results could be further used basic tool for design of sound-absorption structure.

A Study on the Ultimate Strength Behavior according to Modeling Range of the Stiffened Plate (선체보강판의 모델링범위에 따른 최종강도거동에 관한 연구)

  • Park, Joo-Shin;Ko, Jae-Yong;Park, Sung-Hyeon
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.10 no.2 s.21
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    • pp.35-39
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    • 2004
  • Ship structures are basically an assembly of plate elements and the load-carrying capacity or the ultimate strength is one of the most important criteria for safety assessment and economic design. Also, Structural elements making up ship plated structures do not work separately, resulting in high degree of redundancy and complexity, in contrast to those of steel framed structures. To enable the behavior of such structures to be analyzed simplifications or idealizations must essentially be made considering the accuracy needed and the degree of complexity of the analysis to be used On this study, to investigate effect of modeling range, the finite element method are used and their results are compared varying the analysis ranges. The model has been selected from bottom panels of merchant ship structures. For FHA, three types of structural modeling are adopted in terms of the extent of the analysis. The purpose of the present study is to numerically calculate the characteristics of ultimate strength behavior according to the analysis ranges of stiffened panels subject to uniaxial compressive loads.

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Low Temperature Structural Tests of a Composite Wing with Room Temperature-Curing Adhesive Bond (상온접합 본딩이 있는 복합재 날개의 저온 구조시험)

  • Ha, Jae Seok;Park, Chan Yik;Lee, Kee Bhum
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.10
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    • pp.928-935
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    • 2015
  • This paper presents low temperature structural tests of a UAV wing which has room temperature-curing adhesive bond. The wing structure is made of carbon fiber reinforced composites, and the skins are bonded to the inner structures (such as ribs and spars) using room temperature-curing adhesive bond. Also, to verify damage tolerance design of the wing structure, barely visible impact damages are intentionally created in the critical areas. The attachment fittings of the wing are fixed in a specially designed chamber which can simulate the low temperature environments of the operating altitudes. The test load is applied by hydraulic actuators which are placed outside the chamber. The structural tests consist of strain survey tests and a durability test for 1-life fatigue load spectrum. During the tests, strains of major parts are measured by strain gauges and FBG sensors. The change of the initial impact damages is also monitored using piezoelectric sensors. The 1-life damage tolerance of the composite structure is verified by the structural tests under the simulated environments.

Compressive Behavior of H-section Brace Strengthened by Non-welded Cold-Formed Element (무용접 냉간성형 조립재로 보강한 H형강 가새의 압축거동)

  • Kim, Sun Hee;Kim, Do Bum;Choi, Sung Mo
    • Journal of Korean Society of Steel Construction
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    • v.27 no.2
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    • pp.169-180
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    • 2015
  • Recently, Seismic performance of the building built in the past is required to review, because the code for seismic design have been reinforced. In 2009, if the revised latest criteria of seismic design is applied, the majority the steel structure of the low-rise concentrically braced system is short of the seismic performance. Also, when the steel braces are subject to compressive load, which causes unstable behavior of the structure. In order to verify the compressive behavior of the reinforced braces, structural performance test was conducted with variables of slenderness ratio and the amount of reinforcement. Therefore, this study suggests restraining the bending buckling of slender H-shaped braces to resist compressive force. In order to verify the compressive behavior of the reinforced braces, structural performance test was conducted with variables of slenderness ratio and the amount of reinforcement.

Compression Test of Subelement and Tension Test of Hoop Ring for Stiffness Evaluation of Conical Composite Lattice Structures (콘형 복합재 격자 구조의 강성 평가를 위한 Subelement의 압축 시험 및 후프 링의 인장 시험)

  • Jeon, Min-Hyeok;Kong, Seung-Taek;No, Hae-Ri;Kim, In-Gul;Lee, Sang-Woo
    • Composites Research
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    • v.33 no.3
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    • pp.169-175
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    • 2020
  • The compression and tension test were performed to evaluate the stiffnesses of the conical composite lattice structures and results of test were compared with finite element analysis results. Because of difficulty to perform simple tension and compression test due to conical shape, suitable specimens and jig for test were made. Subelements extracted from the structure were prepared for compression test. Compression test of subelement was performed and compressive strains in fiber direction were measured. Compressive stiffness of the helical rib was verified by finite element analysis results. For stiffness of hoop rib, hoop ring specimens were extracted from the structure. Tension test of hoop ring specimen was performed to apply bending deformation to hoop rib. Stiffness of hoop rib was verified by finite element model considering various fiber volume fraction in thickness direction.

하중방향에 따른 직물구조 CFRP의 손상에 대한 AE특성

  • 윤유성;이승현;권오현
    • Proceedings of the Korean Institute of Industrial Safety Conference
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    • 2003.05a
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    • pp.360-365
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    • 2003
  • 최근 선진국에서 차세대전투기와 고속철도차량 및 자동차 동체 등 경량화를 위해 복합재료의 사용범위가 증가되고 있다. 특히 강화재로서 섬유를 직물구조의 형태를 이용한 직물구조 CFRP 복합재료는 일방향 섬유에 비해 변형능력이나 기계적 특성이 우수하여 철근 콘크리트 구조물의 보강제와 같은 구조물 등에까지 그 사용이 확대되고 있다. 하지만 직물구조 CFRP 복합재료는 내부의 손상형태나 위치를 파악하기가 어렵고 직물구조의 복잡한 강화구조를 가지기 때문에 그 역학적 손상거동과 명확한 파괴거동 해석수법은 확립되어 있지 않다.(중략)

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Design Pattern Base4 Component Classification and Retrieval using E-SARM (설계 패턴 기반 컴포넌트 분류와 E-SARM을 이용한 검색)

  • Kim, Gui-Jung;Han, Jung-Soo;Song, Young-Jae
    • The KIPS Transactions:PartD
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    • v.11D no.5
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    • pp.1133-1142
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    • 2004
  • This paper proposes a method to classify and retrieve components in repository using the idea of domain orientation for the successful reuse of components. A design pattern was applied to existing systems and a component classification method is suggested here to compare the structural similarity between each component in relevant domain and criterion patterns. Classifying reusable components by their functionality and then depicting their structures with a diagram can increase component reusability and portability between platforms. Efficiency of component reuse can be raised because the most appropriate component to query and similar candidate components are provided in priority by use of-SARM algorithm.

Manufacturing of All Composite Unmanned Aerial Vehicle (전기체 복합재 무인항공기 제작)

  • 김동민;허명규
    • Composites Research
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    • v.15 no.6
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    • pp.24-29
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    • 2002
  • For the development of all composite unmanned aerial vehicle(UAV), the consideration for manufacturing in design phase and events in composite parts fabrication, subassembly and final assembly are summarized. In design phase, to maximize the advantages of composite material such as cocuring, cobonding and secondary bonding for manufacturing, the advanced structural concept is introduced. For the curing of designed parts, the manufacturing tools for composite parts are designed and manufactured. The assembly jigs are designed to meet dimensional tolerance requirements of the vehicle structure. And the inspection criteria are established and applied for the manufacturing. Technical data for inspection items and methodologies are summarized to utilize for the exclusive specifications of the manufacturing sequence.