• Title/Summary/Keyword: Edge radius

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Investigation of the Influence of Radius and Corner Position on the Residual Stress Distribution in the Vicinity of the Repaired Region via Directed Energy Deposition by using Finite Element Analysis (유한 요소 해석을 이용한 DED 공정의 코너 반경 및 위치에 따른 보수 영역 부근 잔류응력 분포 영향성 조사)

  • Alissultan, Aliyev;Lee, Kwang-Kyu;Ahn, Dong-Gyu
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.20 no.7
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    • pp.33-40
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    • 2021
  • Current industrial flow is directed toward reducing the usage of raw materials by reusing parts, which is referred to as a circular economy (CE). Repair is one of the most value-added approaches in CE, which can be efficiently accomplished via additive manufacturing. The repair technology of metallic parts via the directed energy deposition process, which includes the selective removal and redeposition of damaged regions of metallic parts. Residual stress characteristics depend on the shape of the part and the shape of the redeposition region. The objective of this study is to investigate the effects of the radius and corner position of the substrate on the residual stresses for repair by using finite element analysis (FEA). The residual stress distribution of the 45° angle groove at the edge of the circular shape models on the outer and inner radii was analytically investigated. The analysis was accomplished using SYSWELD software by applying a moving heat source with defined material properties and cooling conditions integrated into the FEA model. The results showed a similar pattern of concentrated stress distribution for all models except the 40-mm and 60-mm radii, for which the maximum stress locations were different. The maximum residual stresses are high but lower than the yield strength, suggesting the absence of cracks and fractures due to residual stresses.

Thermal Shock Resistance Property of TaC Added Ti(C,N)-Ni Cermets (TaC 첨가 Ti(C,N)-Ni 서멧의 내열충격 특성)

  • Shin, Soon-Gi
    • Korean Journal of Materials Research
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    • v.24 no.10
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    • pp.526-531
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    • 2014
  • Thermal shock resistance property has recently been considered to be one of the most important basic properties, in the same way that the transverse-rupture property is important for sintered hard materials such as ceramics, cemented carbides, and cermets. Attempts were made to evaluate the thermal shock resistance property of 10 vol% TaC added Ti(C,N)-Ni cermets using the infrared radiation heating method. The method uses a thin circular disk that is heated by infrared rays in the central area with a constant heat flux. The technique makes it possible to evaluate the thermal shock strength (Tss) and thermal shock fracture toughness (Tsf) directly from the electric powder charge and the time of fracture, despite the fact that Tss and Tsf consist of the thermal properties of the material tested. Tsf can be measured for a specimen with an edge notch, while Tss cannot be measured for specimens without such a notch. It was thought, however, that Tsf might depend on the radius of curvature of the edge notch. Using the Tsf data, Tss was calculated using a consideration of the stress concentration. The thermal shock resistance property of 10 vol% TaC added Ti(C,N)-Ni cermet increased with increases in the content of nitrogen and Ni. As a result, it was considered that Tss could be applied to an evaluation of the thermal shock resistance of cermets.

A Study on the Natural Frequencies of the Sound Emitted by Thin Conical Shell (圓통形셸 의 音響調節 에 관한 實驗的 硏究)

  • 염영하;곽재경;정석주
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.6 no.4
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    • pp.353-360
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    • 1982
  • The determination of the natural frequencies and mode shapes for thin conical shell is an important step not only in the investigation of the dynamic response of the composite structures such as missile cone, mose firings, but also in the analysis of the acoustic behavior of bells. A Rayleigh-Ritz procedure was used to determine the natural frequencies for a certain class of mode shapes of a thin conical shell built in on the edge with the smaller radius and free on the other edge. Both bending and extensional energy are included in the analysis. This paper described the experiments on the two natural frequencies which are present in association with two preferential modal directions, as a result of imperfection of the thin conical shell. Experimental work was conducted on two different bronze conical shells. One of these was specially designed to the effects of the adding distributed mass to the end of the conical shell. The other shells were identical in all dimensions except that of the thickness to the end of the conical shell. In this paper, the effect of a adding mass to a conical shell was investigated. Experimental result was that the magnitude of the natural frequency rate and the increase of depth of beat frequency depend upon the location of adding lumped mass on the surface of the conical shell.

Study of Reverse Design for an Axial Turbine Blade Profile and Design Parameters for Designing Blade Geometry (축류형 터빈 익형의 역설계 및 형상설계를 위한 설계변수에 관한 연구)

  • Cho, Soo-Yong;Oh, Koon-Sup;Choi, Bum-Seog
    • The KSFM Journal of Fluid Machinery
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    • v.3 no.2 s.7
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    • pp.7-14
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    • 2000
  • For a given axial turbine blade, reverse design method is developed to improve blade efficiency, optimize blade profile, or repair parts etc. In this process, design parameters for designing axial turbine blade are induced. The induced design parameters are as follows; ellipse at leading edge, radios of trailing edge, axial chord, tangential chord, wedge angle at the inlet, and unguided turning angle. Suction and pressure surfaces of turbine blade are described by cubic polynomials. Two sample blades we chosen and their blade profiles are measured at the mean radius. Values of design parameters for sample blades are obtained by the reverse design method. Re-designed blade profiles using calculated design parameters are compared with the measured data, and they show good agreement. So, the developed design method could be applied to design general turbine blades. Various blade shapes are designed, and they show that designed blade profiles can be adjusted by controlling design parameters.

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A Study on Fatigue Crack Growth and Stress Intensity Factors of Notch Materials (노치재의 피로균열진전과 응력확대계수 평가에 관한 연구)

  • Lee, Jong-Hyung;Lee, Sang-Young;Yi, Chang-Heon;Kim, Yun-Gon;Lim, Chun-Kyoo;Lee, Chun-Kon;Kwon, Yung-Shin
    • Journal of the Korean Society of Industry Convergence
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    • v.10 no.3
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    • pp.165-169
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    • 2007
  • Prediction of fatigue duration is attainable from the analysis of the growth rate of the fatigue crack, and the property of the fatigue crack growth is determined by the calculation of the stress intensity factor. And the evaluation of the stress intensity factor, K comes from the stress analysis of the vicinity of crack tip of the continuum. This study describes a simple method to decide the stress intensity factor for the small crack at the sharp edge notches. The proposed method is based on the similarities between elastic stress fields of the notch tip described by two parameters, the stress concentration factor K, the radius of arc of the notch. And it is applicable to the analysis of the semi-elliptical penetration cracks and the edge notches.

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Averaged strain energy density to assess mixed mode I/III fracture of U-notched GPPS samples

  • Saboori, Behnam;Torabi, A.R.;Berto, F.;Razavi, S.M.J.
    • Structural Engineering and Mechanics
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    • v.65 no.6
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    • pp.699-706
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    • 2018
  • In the present contribution, fracture resistance of U-notched GPPS members under mixed mode I/III loading conditions is assessed by using the Averaged Strain Energy Density (ASED) criterion. This criterion has been founded based on the ASED parameter averaged over a well-defined control volume embracing the notch edge. The validation of the theoretical criterion predictions is evaluated through comparing with the results of a series of mixed mode I/III fracture tests conducted on rectangular-shaped GPPS specimens weakened by a single edge U-notch. A recently developed apparatus for mixed mode I/III fracture experiments is employed for measuring the fracture loads of the specimens. The test samples are fabricated with different notch tip radii with the aim of evaluating the influence of this major feature of the U-notched components on the mixed mode I/III fracture behavior. It is shown that the onset of brittle fracture in U-notched GPPS specimens under various combinations of tension and out-of-plane shear can well be predicted by means of the ASED criterion.

A New line Matching Technique for Solving Correspondence Problem in Stereo Method (스테레오 방식에서 일치성 문제를 해결하기 위한 새로운 선소 정합법)

  • Kang, Dae-Kap;Kwon, Jung-Jang;Kim, Seong-Dae
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.27 no.3
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    • pp.116-123
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    • 1990
  • Most algorithms utilized the horizontal epipolar lines for solving the correspondence problem in 3-D computer vision. However, the requirement is very difficult to be satisfied in real situations. In this paper, we propose a binocular-stereo matching algorithm, based on line matching method, which does not require the horizontal epipolar lines of the extreme pixels of a given line segment and two circles whose radius is equal to the maximum disparity. And we use the features including the direction of line segments, edge strength and cross-correlation for line matching. The experimental results show that the proposed algorithm can be a useful tool for solving the correspondence problem in 3-D computer vision.

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Structural Effects of Geometric Parameters on Liquid Rocket Turbopump Turbine Blades (터보펌프 터빈 블레이드 형상 요소의 구조적 영향)

  • Yoon, Suk-Hwan;Jeon, Seong-Min;Kim, Jin-Han
    • Aerospace Engineering and Technology
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    • v.10 no.1
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    • pp.30-38
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    • 2011
  • Structural effects of several geometric parameters such as shroud thickness, edge roundness and fillet radius of turbopump turbine blade were investigated throughout transient finite element analyses. Usually shroud is inserted to increase aerodynamic efficiency, but blocks deformation of blades. Therefore it can increase stress level in a structural point of view. Likewise, edge roundness and fillet between blades are also parameters where aerodynamics and structural mechanics should compromise. In this study, overall stress levels according to the geometric parameters were thoroughly investigated and the results could be utilized to determine optimal geometries.

THE WARPED DISK OF INTEGRAL-SIGN GALAXY PGC 20348

  • Ann, H.B.
    • Journal of The Korean Astronomical Society
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    • v.40 no.1
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    • pp.9-16
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    • 2007
  • We examine the morphology and luminosity distribution of a strongly warped spiral galaxy PGC 20348 by conducting a detailed BVI CCD surface photometry using BOAO 1.8m telescope. The radial surface brightness shows a break at warp radius $(r_{\omega})$ with a shallow gradient in the inner disk and a steeper gradient in the outer disk. The luminosity of east side of the disk is ${\sim}0.5$ mag fainter than the west side at r > $r_{\omega}$. The reason for the asymmetric luminosity distribution is thought to be the asymmetric flarings that result in the formation of a large diffuse region at the edge of the east disk and a smaller diffuse region at the west disk. The vertical luminosity profiles show a thick disk component whose scale heights increase with increasing galactocentric distances. The warp of PGC 20348 seems to be made by the tidal interactions with the two massive companion galaxies since the flarings and radial increase of disk scale heights are thought to be general properties of tidally perturbed disks. According to the colors of the two clumps inside the diffuse region at the edge of the east disk, they seem to be sites of active star formation triggered by tidal forces from the companion galaxies.

Optimization Study of a Helicopter Rotor Blade Section Using EDISON Ksec2D and Grid Search Method (EDISON Ksec2D와 Grid Search 법을 이용한 헬리콥터 블레이드 단면의 형상 최적화)

  • Na, Deok-Hwan;Hahm, Jae-Joon;Bae, Jae-Seong
    • Proceeding of EDISON Challenge
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    • 2016.03a
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    • pp.183-189
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    • 2016
  • In this paper, an optimization study on a helicopter rotor blade cross-section was made. Generalization was made to the baseline cross-section to simplify the analysis. To have better performance in aeroelastic response, with the aerodynamic center being the origin of the baseline, the distance between aerodynamic center and shear center, and the distance between mass center and shear center of the blade were minimized. For efficient searching of optimum solutions over the design space, grid search method, which is a method of graphical search was used. Two design variables, radius of balancing weight at leading edge, and offset of the spar from leading edge were selected for the study. Cubic spline interpolation method was used to accommodate searching of the optimum solution. 2-Leveled searching system was devised in accordance with the interpolation method. Optimum solution was found to show 6% decrease in both distance between aerodynamic center and shear center, and mass center and shear center to the baseline.

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