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复合材料铺层角度对螺旋桨受力特性影响分析
Influence of composite layer angle on the mechanical characteristics of propeller
- DOI:
- 作者:
- 秦天腾, 丁永乐, 郭君, 蔡卫军, 韩新波, 谭坤
QIN Tian-teng, DING Yong-le, GUO Jun, CAI Wei-jun, HAN Xin-bo, TAN Kun
- 作者单位:
- 中国船舶集团有限公司 第七〇五研究所, 陕西 西安 710077
The 705 Research Institute of CSSC, Xi'an 710077, China
- 关键词:
- 复合材料螺旋桨;铺层角度;受力特性;流固耦合
composite propeller; layering angle; mechanical characteristics; fluid-structure interaction
- 摘要:
- 复合材料螺旋桨具有高比强度、高阻尼等特性，可有效提高螺旋桨推进效率，这种特性与制作工艺中的铺层方案存在相关性。针对P4119桨，建立复合材料螺旋桨模型，采用流固耦合数值模拟方法，对复合材料螺旋桨形变、应力分布与推进效率进行计算。结果表明，复合材料铺层角度对螺旋桨的弯扭耦合效应产生明显效果，载荷集中区域局部叶型剖面螺距发生改变，进而影响整个螺旋桨径向范围内的螺距、侧斜与纵倾的分布情况。铺层角度0°～90°时，最大应力值下降41.06%～42.90%，推力系数下降4.12%～5.85%，扭矩系数下降4.49%～7.52%，效率提升0.39%～1.8%。因此，复合材料螺旋桨在大载荷下运行时，工况会发生改变，桨叶会随工况产生较大变形，影响其推进性能。调整复合材料铺层角度，可改善桨叶变形情况。
Composite propellers have the characteristics of high specific strength and high damping, which can effectively improve the propeller propulsion efficiency. This characteristic is related to the layering scheme in the manufacturing process. For P4119 propeller, a composite propeller model was established, and the deformation, stress distribution and propulsion efficiency of the composite propeller were calculated by fluid-structure coupling numerical simulation method. The results show that the composite coating angle has a significant effect on the bending-torsion coupling effect of the propeller, and the pitch of the local profile changes in the load concentration area, which affects the distribution of pitch, lateral tilt and trim in the radial range of the whole propeller. When the layup angle is 0° to 90°, the maximum stress value decreases by 41.06%～42.90%, the thrust coefficient decreases by 4.12%～5.85%, the torque coefficient decreases by 4.49%～7.52%, and the efficiency increases by 0.39%～1.8%. Therefore, when composite propellers operate under large loads, the working conditions will change, and the blades will produce large deformation along with the working conditions, which will affect their propulsion performance. The deformation of blade can be improved by adjusting the coating angle of composite material.
2023,45(8): 20-25 收稿日期：2022-08-29
DOI：10.3404/j.issn.1672-7649.2023.08.005
分类号：TJ630.2;U661.313
作者简介：秦天腾(1995-),男,硕士研究生,助理工程师,研究方向为总体技术
