• Title/Summary/Keyword: Hydraulic Rotor Block

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Design of the Hydraulic Rotor Block Curvature for a Knuckle Crane According to the Contact Angle (접촉각에 따른 너클 크레인용 유압로터블록의 만곡부 설계)

  • Lee J.M.;Han G.J.;Han D.S.;Lee S.W.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2006.05a
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    • pp.377-378
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    • 2006
  • The knuckle crane mainly consists of six parts such as swing, main boom, outer boom, extension boom, hydraulic rotor and knuckle. And the hydraulic rotor is connected at the end of extension boom has rotor block, rotor body, rotor vane. In this study, we carried out kinematics analysis of the hydraulic rotor block curvature for a knuckle crane. Then, we showed the formula to establish the radius of a circumscribed circle to form the rotor block curvature. Third, we analyzed the stress at each point of the rotor block curvature according to the contact angle. From the result of this study, we designed the rotor block curvature with a proper contact angle for a knuckle crane to guarantee the stability of hydraulic rotor.

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Unsteady Simulations of the Flow in a Swirl Generator, Using OpenFOAM

  • Petit, Olivier;Bosioc, Alin I.;Nilsson, Hakan;Muntean, Sebastian;Susan-Resiga, Romeo F.
    • International Journal of Fluid Machinery and Systems
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    • v.4 no.1
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    • pp.199-208
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    • 2011
  • This work presents numerical results, using OpenFOAM, of the flow in the swirl flow generator test rig developed at Politehnica University of Timisoara, Romania. The work shows results computed by solving the unsteady Reynolds Averaged Navier Stokes equations. The unsteady method couples the rotating and stationary parts using a sliding grid interface based on a GGI formulation. Turbulence is modeled using the standard k-${\varepsilon}$ model, and block structured wall function ICEM-Hexa meshes are used. The numerical results are validated against experimental LDV results, and against design velocity profiles. The investigation shows that OpenFOAM gives results that are comparable to the experimental and design profiles. The unsteady pressure fluctuations at four different positions in the draft tube is recorded. A Fourier analysis of the numerical results is compared whit that of the experimental values. The amplitude and frequency predicted by the numerical simulation are comparable to those given by the experimental results, though slightly over estimated.