共查询到18条相似文献,搜索用时 187 毫秒
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对引起螺旋桨毂帽鳍系统推进性能变化的细节及流动本质问题的研究,有助于对毂帽鳍的节能机理产生新的认识,并为改进该系统的推进性能提供新的思路。通过模型试验和大涡模拟方法对螺旋桨毂帽鳍系统进行了力的测量及精细流场的分析,从能量的角度,分析了毂帽鳍节能机理。数值模拟显示,在毂帽鳍的作用下,在紧邻桨毂后方区域的流速比无毂帽鳍时小且低速区域更广,桨毂后方流体轴向和横向动能均有所减小。由此可知,毂帽鳍通过回收一部分螺旋桨释放在尾流中的动能实现节能;在桨毂后安装一种圆锥形导流帽可避免流动分离,能进一步提高推进系统的整体效率。 相似文献
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桨毂形状对螺旋桨水动力影响仿真 总被引:1,自引:0,他引:1
《船舶工程》2019,(4)
采用全结构化网格对桨毂进行计算流体动力学(CFD)水动力仿真,验证仿真方法的有效性,研究3种典型桨毂形状对螺旋桨敞水特性、截面压力分布和空化的影响。通过对比分析发现:圆弧形桨毂阻力最小,效率最优,桨毂形状主要影响叶根区域的流动;圆柱形桨毂叶根的压力最小,空化面积最大;圆弧形桨毂的抗空化性能最优。 相似文献
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本文通过对30kn排水型侧斜桨的设计研究,解决了在有设计桨存在的叶根面空泡剥蚀问题,同时也使亲的效率提高了约2%(3叶桨)和6.5%。本研究结果可用于最高航速30kn左右的快艇。 相似文献
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研制了调距桨装置半实物加载试验装置,包括机械加载装置、加载液压系统和电控系统.该试验装置可模拟调距桨装置在实际航行时所受的各种静态载荷.通过试验模拟加载,可获得桨毂毂桥、叶根螺栓等主要零件的应力与加载负荷的关系及分布情况,并可验证理论分析、仿真计算,为叶根螺栓等零件的优化设计提供依据. 相似文献
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Numerical simulation is investigated to disclose how propeller boss cap fins (PBCF) operate utilizing Reynolds-averaged Navier-Stokes (RANS) method. In addition, exploration of the influencing mechanism of PBCF on the open water efficiency of one controllable-pitch propeller is analyzed through the open water characteristic curves, blade surface pressure distribution and hub streamline distribution. On this basis, the influence of parameters including airfoil profile, diameter, axial position of installation and circumferential installation angle on the open water efficiency of the controllable-pitch propeller is investigated. Numerical results show: for the controllable-pitch propeller, the thrust generated is at the optimum when the radius of boss cap fins is 1.5 times of propeller hub with an optimal installation position in the axial direction, and its optimal circumferential installation position is the midpoint of the extension line of the front and back ends of two adjacent propeller roots in the front of fin root. Under these optimal parameters, the gain of open water efficiency of the controllable-pitch propeller with different advance velocity coefficients is greater than 0.01, which accounts for approximately an increase of 1%-5% of open water efficiency. 相似文献
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HUANG Sheng WANG Pei-sheng HU Jian 《船舶与海洋工程学报》2007,6(2):6-11
The hydrodynamic performance of a propeller in unsteady inflow was calculated using the surface panel method. The surfaces of blades and hub were discreted by a number of hyperboloidal quadrilateral panels with constant source and doublet distribution. Each panel's corner coordinates were calculated by spline interpolation between the main parameter and the blade geometry of the propeller. The integral equation was derived using the Green Formula. The influence coefficient of the matrix was calculated by the Morino analytic formula. The tangential velocity distribution was calculated with the Yanagizawa method, and the pressure coefficient was calculated using the Bonuli equation. The pressure Kutta condition was satisfied at the trailing edge of the propeller blade using the Newton-Raphson iterative procedure, so as to make the pressure coefficients of the suction and pressure faces of the blade equal at the trailing edge. Calculated results for the propeller in steady inflow were taken as initialization values for the unsteady inflow calculation process. Calculations were carried out from the moment the propeller achieved steady rotation. At each time interval, a linear algebraic equation combined with Kutta condition was established on a key blade and solved numerically. Comparison between calculated results and experimental results indicates that this method is correct and effective. 相似文献
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Jungyong Wang Ayhan Akinturk Neil Bose Stephen J. Jones Yun Young Song Ho Hwan Chun Moon Chan Kim 《Journal of Marine Science and Technology》2008,13(3):244-255
The objective of this study was to investigate the performance of a model azimuthing podded propulsor in ice-covered water.
Model tests were carried out with two different depths of cut into the ice (15 and 35 mm), two different ice conditions (presawn
and pack ice conditions), and four different azimuthing angles. The depth of cut is the maximum penetration depth of the propeller
blade into the ice block. The 0.3-m-diameter model propeller was operated in a continuous ice milling condition. Ice loads
were measured by several sensors which were installed in various positions on the model. Six one-axis pancake-style load cells
on the top of the model measured the global loads and two six-component dynamometers were installed on the shaft to measure
the shaft loads. One six-component dynamometer was attached to the one of the propeller blades inside the hub to measure the
blade loads. The pod unit and propeller performance in ice are presented. Ice-related loads, which were obtained when the
blade was inside the ice block, are introduced and discussed. During the propeller–ice interaction, a blade can experience
the path generated by the previous blade, which is called the shadowing effect. The effects of shadowing, depth of cut, azimuthing
angle, and advance coefficient on propulsor performance are presented and discussed. 相似文献