• 제목/요약/키워드: swept surface

검색결과 57건 처리시간 0.024초

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

  • 박배용;안정호
    • 대한기계학회논문집A
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    • 제26권9호
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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.

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

  • 정연찬;최병규
    • 한국CDE학회논문집
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    • 제1권1호
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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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공구 이동 궤적면과 Z-direction 벡터의 교차점 계산 (Finding an Intersection Point between Cutter Swept Surface with a Z-Direction Vector)

  • 박배용;안정호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집C
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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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공구이동궤적 모델을 이용한 5축 페이스밀링 가공데이터 생성 (Five-axis CL Data Generation by Considering Tool Swept Surface Model in Face Milling of Sculptured Surface)

  • 이정근;박정환
    • 한국CDE학회논문집
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    • 제9권1호
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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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    • 제17권12호
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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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    • 제3권1호
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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.

캐널곡면의 복원 (Reconstruction of Canal Surfaces)

  • 이인권;김구진
    • 한국정보과학회논문지:시스템및이론
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    • 제32권8호
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    • pp.411-417
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    • 2005
  • 본 논문에서는 입력으로 주어진 점집차 (point cloud)으로부터 캐널곡면을 복원 (reconstruction)하는 알고리즘을 제시한다. 캐널곡면은 반경이 변화하며 중심점이 기준곡선(spine curve)을 따라 이동하는 구(moving sphere)의 스웹트곡면(swept surface)이다. 이 논문에서는 수축기법(shrinking method)과 moving least-square 방법을 이용하여 주어진 점집합을 세곡선(thin-curve)형태의 점집합으로 수축시킴으로써 캐널곡면의 기준곡선을 근사한다. 근사된 기준곡선과 입력으로 주어진 점집합에 포함된 점들 사이의 거리를 이용하여, 캐널곡면을 구성하는 이동 구의 반경을 계산한다.

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

  • 엄진섭
    • 센서학회지
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    • 제21권1호
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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.

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

  • 정진덕;이장연;성봉주;이종원
    • 대한기계학회논문집B
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    • 제28권7호
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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.

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

  • 이인권
    • 한국컴퓨터그래픽스학회논문지
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    • 제5권2호
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    • pp.1-7
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    • 1999
  • 구조화되어있지 않은 점 집합으로부터 파이프 곡면을 복원해 내는 알고리즘을 기술한다. 파이프 곡면은 척추 곡선과 스위핑 구의 반지름으로 정의된다. 수축과 동적 최소자승법에 의해 점 집합은 얇은 곡선 형태로 변환된다. 이 얇은 곡선 형태의 점 집합은 쉽게 척추곡선으로 근사될 수 있다. 얇은 점 집합과 원래 주어진 점 집합의 대응하는 두 점간의 거리로 파이프 곡면을 정의하는 스위핑 구의 반지름을 구할 수 있다.

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