• Title/Summary/Keyword: 체결 해석

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The Assessment for Coupling Integrity of Pressurizer Support Bolting (가압기 지지대 볼트 연결부의 건전성 평가에 관한 연구)

  • Cho, Nam-Jin;Kim, Woo-Chang;Kim, Hak-Joong
    • Fire Science and Engineering
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    • v.27 no.5
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    • pp.26-31
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    • 2013
  • In nuclear power plant, anchor bolts for pressurizer supports are sufficiently used in terms of safety reason, but field inspections have reported that some bolts exceed the limit of their allowable hardness. Because the high level of hardness may lead to failures due to the stress corrosion or fracture toughness, a regular inspection is required for the bolts in nuclear power plant. Thus, this research measures the hardness of bolts currently used in pressurizer supports and then estimates maximum allowable stresses preventing failures by stress corrosion and fracture toughness. Using the ANSYS program, the stresses of the bolts in the regular condition and accidental condition have been calculated, and the possible maximum stress has been compared with the estimated allowable stresses. From the results, the stresses of bolts in the accidental condition satisfy the allowable safety stress from the stress corrosion failure. However, in the future, it shall be needed to consider the reflection of the structure assembling method on the assembling procedure to ensure the pressurizer integrity during maintenance period time.

Suggestion of an experimental method for optimization of flange point of a bolt-clamped Langevin-type ultrasonic transducer (볼트 체결형 란주반 초음파 트랜스듀서의 프렌지 포인트 최적화를 위한 실험적 방법 제안)

  • Kim, Jungsoon;Kim, Haeun;Kim, Moojoon
    • The Journal of the Acoustical Society of Korea
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    • v.40 no.4
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    • pp.270-277
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    • 2021
  • In the power ultrasound fields, the flange position for fixing the transducer is an important factor influencing on electro-mechanical efficiency of the transducer. We suggested a practical method that can determine the installation position of the flange for different resonance modes of the bolt-clamped type Langevin ultrasonic transducer. A semicircular wedge-shaped jig was manufactured and moved along the lateral surface of the transducer. The vibration characteristics were examined after a constant pressure was applied to the semicircular wedge-shaped jig. By observing the change of the input admittance of the transducer depending on the position of the pressure application, the optimum position for the flange installation could be determined. The resonant modes of the transducer were calculated by a Mason's equivalent circuit, and the particle velocity distribution for each resonance mode was calculated by a transmission line model. Since the optimum positions determined from an experimental result show a good correspondence with the node positions of the vibration modes calculated by the transmission line model, the validity of the suggested method was verified.

Geometric Modeling of the Skin-Stringer Integrated Panel with Three-Dimensional Woven Composite (3차원 직조 복합재료 스킨-스트링거 일체형 패널의 기하학적 모델링)

  • Yeonhi, Kim;Hiyeop, Kim;Jungsun, Park;Joonhyung, Byun
    • Journal of Aerospace System Engineering
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    • v.16 no.6
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    • pp.8-17
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    • 2022
  • This paper presents a novel geometric modeling technique to predict the mechanical properties of an aircraft wing's skin-stringer integrated panel. Due to mechanical and adhesive fastening, this panel is vulnerable to stress concentration and debonding, so we designed it to integrate the skin and stringer using three-dimensional woven composites. Geometric modeling was conducted by measuring the geometric parameters of the specimen and defining the pattern of the yarns as functions. We used a weighted average model with iso-strain and iso-stress assumptions to predict the mechanical properties of the panel parts. We then compared the results of a finite element analysis with a compression test to verify the accuracy of our model. Our proposed technique proved to be more efficient than the traditional experimental method for predicting the mechanical properties of skin-stringer integrated panels.

A Study of Static Behavior of FRP Bridge Deck Concerning Connection Condition (FRP바닥판의 연결조건에 따른 정적거동 분석)

  • Yong, Hwan Sun;Hwang, Yoon Koog;Kyung, Kab Su;Park, Yong Chan
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.26 no.4A
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    • pp.597-604
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    • 2006
  • Fiber Reinforced Polymer (FRP) is a relatively new material in the bridge construction. With high strength to weight ratios, excellent durability, and low life-cycle costs of FRP, FRP bridge decks can offer a low dead load, reduced maintenance, and long service life. Due to the lightweight of FRP, if existing concrete decks can be replaced with the FRP decks, the load carrying capacity of superstructure can be increased without strengthening of girders. In this study, we have conducted an experiment on 7 cases of connection conditions with steel girder by using bolts considering a rational and economical method of connection and compared with the results of FEM analysis. From the experimental result, if the bolts are strong enough to resist shear force between the FRP bridge deck and the steel girder, it will be structurally secure to use the zigzag method.

A Study Of the Safety Analysis of Titanium Sprockets by Using Finite Element Method (유한요소법을 이용한 티타늄 스프라켓의 안전성 해석에 관한 연구)

  • Song, Byeong-Uk;Cho, Ji-Hyun;Seo, Keum-Hee;Seo, Tae-Il;Bae, Jong-Suk;Park, Jin-Sung
    • Proceedings of the KAIS Fall Conference
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    • 2011.12b
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    • pp.417-420
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    • 2011
  • 본 논문에서는 자전거의 구동 및 변속 창치인 스프라켓에 관한 연구이다. FEM을 이용하여 티타늄 소재 스프라켓의 구조해석을 수행하기 위해 10단 Cassette를 설계하였고, 사용자가 가장 많이 사용하는 단수인 4, 5, 6단을 티타늄 소재로 선정하였다. 티타늄 재료의 물성치를 실험을 통해 확보하였으며, 이를 이용하여 티타늄 스프라켓의 각 치형에 걸리는 Equivalent Stress를 구하였고 스프라켓 고정장치인 스파이더와의 체결 후의 Equivalent Stress를 구하여 티타늄 스프라켓의 안정성을 확보한다.

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Structural Analysis on the Heavy Duty Diesel Engine and Optimization for Bearing Cap (대형 디젤엔진의 구조응력해석 및 베어링 캡의 최적설계)

  • Lee, Jae-Ok;Lee, Young-Shin;Lee, Hyun-Seung;Kim, Jae-Hoon;Jun, Joon-Tak;Kim, Chul-Goo
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.32 no.5
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    • pp.402-410
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    • 2008
  • The heavy duty diesel engine must have a large output for maintaining excellent mobility. In this study, a three dimensional finite element model of a heavy-duty diesel engine was developed to conduct the stress analysis. The FE model of the heavy duty diesel engine main parts consisting with four half cylinder was selected. The heavy duty diesel engine parts includes with cylinder block, cylinder head, gasket, liner, bearing cap, bearing and bolts. The loading conditions of engine were pre-fit load, assembly load, and gas load. As the results of structural analysis, because the stress values of cylinder block and bearing cap did not exceed the basic design can be satisfied. But on the part which contacts with cylinder block and bearing cap the stress value exceeds the allowable strength of material. In order to decrease the stress at that part, it was optimized with parametric study.

Finite Element Analysis of Re-Cold Expansion in Order to Improve the Fatigue Life of Fastener Hole that has been Cold Expanded Before (홀확장법을 적용한 체결홀의 피로수명 개선을 위한 재 홀확장 효과에 대한 유한요소 해석)

  • Jang, Jae-Soon;Yang, Won-Ho;Cho, Myoung-Rea
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.30 no.9 s.252
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    • pp.1110-1115
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    • 2006
  • Cold expansion of fastener holes has been successfully used for many years to impart beneficial compressive residual stresses. Beneficial compressive residual stress of fastener hole that has been cold expanded before is reduced by using of materials for a long time. As a result, fatigue life of material is reduced. So, compressive residual stresses of material have to regenerate by re-cold expansion method. In this paper, it was carried out a finite element analysis about variation of residual stress due to tensile stress and residual stress distribution that was regenerated by re-cold expansion method in the fastener hole. Here, a diversity tensile stress was used. Also, it was performed a finite element analysis according to cold expansion rate of re cold expansion in order to obtain a beneficial compressive residual stress.

The Causes of Bolt Breakage During the Tightening of Impellers in Water Jet Propulsion Systems (워터제트 추진기 임펠러 체결용 볼트파손 원인 분석 연구)

  • Jung, Sang-Jin;Oh, Shini Il;Hur, Jang-Wook
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.18 no.10
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    • pp.48-53
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    • 2019
  • A water jet propeller is a key component that generates propulsion during the start of a naval vessel. When failure or breakage occurs, the vessel cannot operate. Recently, a flow analysis and structural analysis were conducted to understand the cause of damage to a bolt on a water jet. In particular, the stress and strain acting on the fastening bolt (impeller shaft and tail shaft) were examined to determine the extent of misalignment between the impeller shaft and the tail shaft of the water jet propeller. The study determined that stress and strain were concentrated on the impeller shaft and the tail shaft bolt. The alignment of the propeller impeller shaft and the tail shaft increased significantly in response to the tail shaft bolt. Failure of the tail shaft bolt fastening can lead to misalignment between the impeller shaft and the tail shaft.

Functional Verification of Nylon Wire Cutting-Type Holding & Release Mechanism for 6U CubeSat's Solar Panel (나일론선 절단방식 6U 큐브위성용 태양전지판 구속분리장치의 기능검증)

  • Park, Yeon-Hyeok;Go, Ji-Seong;Chae, Bong-Geon;Lee, Seong-Ho;Oh, Hyun-Ung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.10
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    • pp.867-875
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    • 2018
  • Conventional nylon wire cutting-type holding and release mechanisms (HRMs) are limited to securely hold the solar panel under launch environment as the size of the panel increases because the nylon wire is tightened directly on the surface of the solar panel. In this study, we proposed a nylon wire cutting-type HRM for 6U CubeSat's solar panel applying elliptic-shaped bracket with a Ball & Socket interface. The proposed HRM has the advantage of higher holding capability along in-plane and out-of plane directions of solar panel and simplicity in tightening process of nylon wire. The design drivers of structural design of CubeSat's solar panel with the proposed HRM were defined by structural analysis under launch loads. In addition, The design effectiveness of the proposed HRM was verified through the functional tests according to the thickness of nylon wire and the number of wire winding under various temperature conditions.

Evaluation of the Optimal Vertical Stiffness of a Fastener Along a High-speed Ballast Track (고속철도 자갈궤도 체결구 최적 수직강성 평가)

  • Yang, Sin-Choo;Kim, Eun
    • Journal of the Korean Society for Railway
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    • v.18 no.2
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    • pp.139-148
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    • 2015
  • By increasing the vertical stiffness of the rail fastening system, the dynamic wheel load of the vehicle can be increased on the ballast track, though this increases the cost of track maintenance. On the other hand, the resistance acting on the wheel is decreased, which lowers the cost of the electric power to run the train. For this reason, the determination of the optimal fastener stiffness is important when attempting to minimize the economic costs associated with both track maintenance and energy to operate the train. In this study, a numerical method for evaluating the optimal vertical stiffness of the fasteners used on ballast track is presented on the basis of the process proposed by L$\acute{o}$pez-Pita et al. They used an approximation formula while calculating the dynamic wheel load. The evaluated fastener stiffness is mainly affected by the calculated dynamic wheel load. In this study, the dynamic wheel load is more precisely evaluated with an advanced vehicle-track interaction model. An appropriate range of the stiffness of the fastener applicable to the design of ballast track along domestic high-speed lines is proposed.