• 제목/요약/키워드: spinning mechanism

검색결과 43건 처리시간 0.03초

Computational Study on Unsteady Mechanism of Spinning Detonations

  • Matsuo, Akiko;Sugiyama, Yuta
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.367-373
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    • 2008
  • Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

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Computational Study on Unsteady Mechanism of Spinning Detonations

  • Matsuo, Akiko;Sugiyama, Yuta
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년 추계학술대회논문집
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    • pp.367-373
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    • 2008
  • Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

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용융형 전기방사법에 의한 폴리에스테르섬유의 방사거동과 구조에 관한 연구 (Study on Spinning Behavior and Structure of Polyester Fibers by the Melt-type Electrospinning Method)

  • Lee, Jin-Ah;Lim, Min-Soo;Joo, Chang-Whan
    • 한국섬유공학회:학술대회논문집
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    • 한국섬유공학회 2002년도 봄 학술발표회 논문집
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    • pp.273-276
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    • 2002
  • The fiber formation of conventional melt spinning is extruded by forcing the polymer melt through a spinneret by pumping mechanism usually involving high pressure. This is followed by cooling, solidification and appropriate drawing of the fiber. The spinning process is broadly applicable to polyolefin, polyamide, polyester and indeed the whole range of fibers forming thermoplastic polymers. (omitted)

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전단 스피닝에 의한 원추형상의 성형에 관한 변형 메커니즘 (New Deformation Mechanism in the Forming of Cones by Shear Spinning)

  • 김재훈;김철
    • 소성∙가공
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    • 제14권4호
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    • pp.375-383
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    • 2005
  • The shear spinning process, where the plastic deformation zone is localized in a very small portion of the workpiece, shows a promise for increasingly broader application to the production of axially symmetric parts. In this paper, the three components of the working force are calculated by a newly proposed deformation model in which the spinning process is understood as shearing deformation after uniaxial yielding by bending, and shear stress, $\tau_{rz}$, becomes k, yield limit in pure shear, in the deformation zone. The tangential force are first calculated and the feed force and the normal force are obtained by the assumption of uniform distribution of roller pressure on the contact surface. The optimum contact area is obtained by minimizing the bending energy required to get the assumed deformation of the blank. The calculated forces are compared with experimental results. A comparison shows that theoretical prediction is reasonably in good agreement with experimental results

병렬구조 모션 시뮬레이터 이클립스-II 를 위한 가상현실 시험경로 개발 (Development of the Virtual Test Path for Eclipse-II, A Parallel Mechanism Motion Simulator)

  • 인우성;김종원
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.965-968
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    • 2004
  • This paper describes the development of the test path for Eclipse-II, a parallel mechanism motion simulator. Eclipse-II which can be used as a base for general motion simulators, enables unlimited continuous 360-degree spinning in any rotational axes plus finite X, Y, and Z translation motions. The advantage of enabling continuous 360-degree spinning allows various motions for virtual reality. In this paper, the development of the test path to verify the robustness of the Eclipse-II motion simulator is described. The test motions, which satisfy the requirements of test path, are suggested and washout filter enables these motions reproduced in the limited workspace. The trial run is conducted to verify the robustness of the Eclipse-II motion simulator. Additionally the standard data format of virtual reality for Eclipse-II One Man Ride is suggested.

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Three-Dimensional Numerical Analysis for Detonation Propagating in Circular Tube

  • Sugiyama, Yuta;Matsuo, Akiko
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.364-370
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    • 2008
  • Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable and unstable pitch modes for the lower and higher activation energies, respectively. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of two modes. The maximum pressure history in the stable pitch remained nearly constant, and the single Mach leg existing on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the unstable pitch due to the generation and decay of complex Mach interaction on the shock front shape. The high frequency oscillation was self-induced because the intensity of the transverse wave was changed during propagation in one cycle. The high frequency behavior was not always the same for each cycle, and therefore the low frequency oscillation was also induced in the pressure history.

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전기스피닝 공구의 삼분력 해석 (Analysis of three force components of shear spinning)

  • 최재찬;백남주
    • 대한기계학회논문집
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    • 제5권2호
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    • pp.88-93
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    • 1981
  • The three force components of shear spinning are calculated by a newly proposed deformation model. The spinning process is understooed as shearing deformation arter uniaxial yuelding by ending, and shear stress .tau.$\sub$rz/ becomes .kappa. the yueld limit in pure shear, in the deformation zone. The tangential forces are calculated and then the feed forces and normal foeces are obtained by assuming a nuiform distribution of roller pressure on the contact surface. An optimum contact area is obtaned by minimizing the bending energy required to obtain the assumed deformation mechanism. The calculated forces are compared with experimental data form published literature and present experiments. Good agreement cetween calculated and experimental values for working forces is obtained over a wide range of process variables.

폴리프로필렌 중공사막의 용융방사

  • 김진호;강민수;김성수
    • 한국막학회:학술대회논문집
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    • 한국막학회 1996년도 추계 총회 및 학술발표회
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    • pp.75-76
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    • 1996
  • 다공성 고분자 분리막을 제조하는 방법으로 기존의 용매교환법을 대신하여 내용매성, 내약품성 및 내열성이 매우 뛰어난 고분자를 소재로하여 다공성 고분자막을 만드는 열유도 상분리법(Thermally Induced Phase Separation, TIPS)이 개발되었다. TIPS공정에서는 주로 고분자/희석제 system의 열역학적인 불안정성에 의하여 polymer-rich phase와 polymer-lean phase로 상이 분리되는 liquid-liquid phase separation과 결정성 고분자의 결정화에 의한 solid-liquid phase separation을 주로 상분리 mechanism으로 사용하고 있다. 따라서 위에 언급된 TIPS 이론에 근거한 melt spinning 공정에 의하여 PP 중공사막을 제조하였는데 wet spinning 공정에 의한 용매 교환법에 비해 비교적 공정이 단순하고 다공도를 조건하기가 용이하며 구조 및 성능면에서도 높은 재현성을 가지고 있다. 또한 우수한 소재임에도 불구하고 절절한 용매의 부재로 용매교환법에서 사용할 수 없었던 폴리올레핀계, 나일론계, 방향족출합계 고분자를 사용할 수 있게 되어 소재의 폭이 넓어졌다는데에 가장 큰 장점이 있다. 본 연구에서는 PP중공사막을 제조하기 위하여 먼저 용융 방사장치를 제작하였고 melt spinning 공정에 의해 막을 제조하는데 적합한 방사조건들을 확립한 후 결정된 방사조건에 의해 얻어진 PP 중공사막의 구조 및 성능에 영향을 미치는 인자들에 관하여 조사하였다.

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