• Title/Summary/Keyword: swept surface

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Parametric Modelling of Cutter Swept Surface for Z-Map Based Cutting Simulation (Z-Map기반 모의가공을 위한 공구 이동 궤적면의 매개변수형 모델링)

  • Park, Bae-Yong;An, Jeong-Ho
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.26 no.9
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    • pp.1814-1821
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    • 2002
  • NC cutting simulation is an important factor in the development of products. The geometric modelling of cutter swept surface should be done in NC cutting simulation. A part of cutter swept surface is a ruled surface blended with silhouette curve and cutter path. Finding an intersection point between cutter swept surface and a line is one of major problems in Z-map based cutting simulation. In this paper, cutter swept surface is defined parametrically and it's intersection point with Z-map is found in an exact form. Triangular grid Z-map based 3-axis NC cutting simulation is performed.

Non-parametric Modeling of Cutter Swept Surfaces for Cutting Simulation (모의가공을 위한 공구 이동 궤적면의 비매개변수형 모델링)

  • 정연찬;최병규
    • Korean Journal of Computational Design and Engineering
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    • v.1 no.1
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    • pp.45-55
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    • 1996
  • This paper presents a new approach to non-parametric modeling of cutter swept surface (CSS) for cutting simulation. Instead of explicitly modeling cutter swept volumes, silhouette curves of the cutter surface are utilized in computing the z-value of the CSS at a grid point on the x,y-plane. The non-parametric evaluation of the CSS constitutes the integral part of 3-axis cutting simulation. The proposed method is more efficient than the existing ones in the case of conventional cutters (i.e., ball-end mills and flat-end mills), and more importantly, it enables the non-parametric modeling of the CSS for the round-end mills which was not possible with the existing methods.

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Finding an Intersection Point between Cutter Swept Surface with a Z-Direction Vector (공구 이동 궤적면과 Z-direction 벡터의 교차점 계산)

  • Park, Pae-Yong;Ahn, Jeong-Ho
    • Proceedings of the KSME Conference
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    • 2001.06c
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    • pp.235-239
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    • 2001
  • Finding intersection point between a surface and a line is one of major problem in CAD/CAM. The intersection point could be found in an exact form or with numerical method. In this paper, the exact solution of the intersection point between a ruled surface which is generated by the movement of an endmill and the z-direction vector is presented. The cutter swept surface which is a ruled surface and the Z-direction vector are represented with parametric equations. With the nature of parametric equations, the geometric properties at the intersection point are easily acquired.

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Five-axis CL Data Generation by Considering Tool Swept Surface Model in Face Milling of Sculptured Surface (공구이동궤적 모델을 이용한 5축 페이스밀링 가공데이터 생성)

  • 이정근;박정환
    • Korean Journal of Computational Design and Engineering
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    • v.9 no.1
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    • pp.35-43
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    • 2004
  • It is well known that the five-axis machining has advantages of tool accessibility and machined surface quality when compared with conventional three-axis machining. Traditional researches on the five-axis tool-path generation have addressed interferences such as cutter gouging, collision, machine kinematics and optimization of a CL(cutter location) or a cutter position. In the paper it is presented that optimal CL data for a face-milling cutter moving on a tool-path are obtained by incorporating TSS(tool swept surface) model. The TSS model from current CL position to the next CL position is constructed based on machine kinematics as well as cutter geometry, with which the deviation from the design surface can be computed. Then the next CC(cutter-contact) point should be adjusted such that the deviation conforms to given machining tolerance value. The proposed algorithm was implemented and applied to a marine propeller machining, which proved effective from a quantitative point of view. In addition, the algorithm using the TSS can also be applied to avoid cutter convex interferences in general three-axis NC machining.

Application of the Scaling Law for Swept Shock/Boundary-Layer Interactions

  • Lee, Yeol
    • Journal of Mechanical Science and Technology
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    • v.17 no.12
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    • pp.2116-2124
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    • 2003
  • An experimental study providing additional knowledge of quasi-conical symmetry in swept shock wave/turbulent boundary-layer interactions is described. When a turbulent boundary layer on the flat plate is subjected to interact with a swept planar shock wave, the interaction flowfield far from fin leading edge has a nature of conical symmetry, which topological features of the interaction flow appear to emanate from a virtual conical origin. Surface streakline patterns obtained from the kerosene-lampblack tracings have been utilized to obtain representative surface features of the flow, including the location of the virtual conical origin. The scaling law for the sharp-fin interactions suggested by previous investigators has been reexamined for different freestream Mach numbers. It is noticed that the scaling law reasonably agrees with the present experimental data, however, that the law is not appropriate to estimate the location of the virtual conical origin. Further knowledge of the correlation for the virtual conical origin has thus been proposed.

Comb-spacing-swept Source Using Differential Polarization Delay Line for Interferometric 3-dimensional Imaging

  • Park, Sang Min;Park, So Young;Kim, Chang-Seok
    • Current Optics and Photonics
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    • v.3 no.1
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    • pp.16-21
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    • 2019
  • We present a broad-bandwidth comb-spacing-swept source (CSWS) based on a differential polarization delay line (DPDL) for interferometric three-dimensional (3D) imaging. The comb spacing of the CSWS is repeatedly swept by the tunable DPDL in the multiwavelength source to provide depth-scanning optical coherence tomography (OCT). As the polarization differential delay of the DPDL is tuned from 5 to 15 ps, the comb spacing along the wavelength continuously varies from 1.6 to 0.53 nm, respectively. The wavelength range of various semiconductor optical amplifiers and the cavity feedback ratio of the tunable fiber coupler are experimentally selected to obtain optimal conditions for a broader 3-dB bandwidth of the multiwavelength spectrum and thus provide a higher axial resolution of $35{\mu}m$ in interferometric OCT imaging. The proposed CSWS-OCT has a simple imaging interferometer configuration without reference-path scanning and a simple imaging process without the complex Fourier transform. 3D surface images of a via-hole structure on a printed circuit board and the top surface of a coin were acquired.

Reconstruction of Canal Surfaces (캐널곡면의 복원)

  • Lee In-Kwon;Kim Ku-Jin
    • Journal of KIISE:Computer Systems and Theory
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    • v.32 no.8
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    • pp.411-417
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    • 2005
  • We present a method to reconstruct a canal surface from a point cloud (a set of unorganized points). A canal surface is defined as a swept surface of a moving sphere with varying radii. By using the shrinking and moving least-squares methods, we reduce a point cloud to a thin curve-like point set which can be approximated to the spine curve of a canal surface. The distance between a point in the thin point cloud and a corresponding point in the original point set represents the radius of the canal surface.

Swept Source-Optical Coherence Tomography Using New Recalibration Method for Nonlinear Sweeping Laser (광원의 비선형 파장스위핑이 보정된 SS-OCT)

  • Eom, Jin-Seob
    • Journal of Sensor Science and Technology
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    • v.21 no.1
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    • pp.68-74
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    • 2012
  • In this paper, Frequency Domain Mode Locked(FDML) wavelength swept laser with 55.027 kHz sweeping speed and 125 nm sweeping range has realized, and also a new method for recalibrating a nonlinear frequency sweeping of a swept laser has proposed. The Swept Source-Optical Coherence Tomography system using the proposed method has performed. For a mirror surface, the system showed the very clean 2-dimensional image and the advanced image speed of 7 frames per sec compared to the previous recalibration method.

Wind Tunnel Test to Enhance Aerodynamic Characteristics of Forward Swept Wing Airplane (전진익형 항공기 공력특성 증진을 위한 풍동시험)

  • Chung, Jin-Deog;Lee, Jang-Yeon;Sung, Bong-Zoo;Lee, Jong-Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.7
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    • pp.800-808
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    • 2004
  • Wind tunnel test of an airplane model with forward swept wing was done in KARI LSWT to evaluate and measure the aerodynamic characteristics of initially designed configuration. Since the given wing planform did not fully satisfy the design requirements, local flow control devices such as vortilon, vortex generator and flow fence were used to delay separation and to enhance aerodynamic characteristics. Also decision making processes of design parameters such as vertical tail boom length, the location, size and the incidence angle of horizontal tail were discussed. The general aerodynamic characteristics of forward swept wing for various control surface deflection conditions of flap, aileron and elevator were also given.

Pipe Surface Reconstruction Using Shrinking (수축을 이용한 파이프 곡면의 복원)

  • Lee, In-Kwon
    • Journal of the Korea Computer Graphics Society
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    • v.5 no.2
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    • pp.1-7
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    • 1999
  • We present an algorithm to reconstruct a pipe surface from a set of unorganized points. A pipe surface is defined by a spine curve and a radius of a swept sphere. In this paper, by using the shrinking and moving least-squares methods, a point cloud is reduced to a thin curve-like point set that can be easily approximated with a spine curve of a pipe surface. The distance between a point in the thin point cloud and a corresponding point in the original point set represents the radius of a swept sphere of a pipe surface.

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