吴浩, 杨子烨, 曹建鑫, 等. 大尺度自航模气层减阻试验研究[J]. 中国舰船研究, 2024, 19(X): 1–6. DOI: 10.19693/j.issn.1673-3185.03360
引用本文: 吴浩, 杨子烨, 曹建鑫, 等. 大尺度自航模气层减阻试验研究[J]. 中国舰船研究, 2024, 19(X): 1–6. DOI: 10.19693/j.issn.1673-3185.03360
WU H, YANG Z Y, CAO J X, et al. Experimental research of air layer drag reduction on self-propelled model[J]. Chinese Journal of Ship Research, 2024, 19(X): 1–6 (in Chinese). DOI: 10.19693/j.issn.1673-3185.03360
Citation: WU H, YANG Z Y, CAO J X, et al. Experimental research of air layer drag reduction on self-propelled model[J]. Chinese Journal of Ship Research, 2024, 19(X): 1–6 (in Chinese). DOI: 10.19693/j.issn.1673-3185.03360

大尺度自航模气层减阻试验研究

Experimental research of air layer drag reduction on self-propelled model

  • 摘要:
    目的 旨在研究气流量、航行倾角对船底凹槽内气层保持和节能效果的影响。
    方法 以一艘肥大型散货船的较大尺度缩比模型为研究对象,通过设计气层减阻自航模系统和船底凹槽方案,开展开阔水域条件下自航模气层减阻试验,研究模型正浮状态下喷气减阻效果,以及模型一定纵倾角状态下对航速和轴功率的影响。
    结果 在主机转速一定时,喷气可以明显提高自航模的航速,停止喷气后,船底凹槽内的气体仍能维持较长时间;船体尾倾角为0°~0.25°时的气层减阻效果较好,较大尾倾角时气体从自航模艏部两侧溢出,气层无法对船底实现有效覆盖,减阻效果不佳。
    结论 通过试验,可对气层减阻技术在肥大型船舶上的工程应用提供一定参考。

     

    Abstract:
    Objectives The effects of air flow rate, sailing angle within the groove bottom of the air layer retention and energy efficiency were studied.
    Methods The study focuses on a large-scale scale model of a bulk carrier. By designing a air layer drag reduction self-propelled model system and a hull cavity scheme, drag reduction experiments were conducted under open water conditions using the self-propelled model. The research examines the jet drag reduction effect on the model in a positive floating attitude of ship, as well as the impact of a certain trim angle on the speed and shaft power of the model..
    Results When the host speed is in certain, it can significantly improve the model speed with air injection, and after stopping the jet the air layer within the air cavity of ship bottom can be maintained for a long time; it will get better drag reduction efficiency when the ship in the upright state and the trimming is within 0.25 degrees. When the trimming angle is too larger, the gas will overflows from both sides of the model head, and the air layer cannot effectively cover the bottom of the ship, so it will decrease the efficiency of the drag reduction.
    Conclusions Through experiments, some meaningful conclusions have been obtained, which can provide a certain reference for the engineering application of air layer drag reduction technology on full-formed ships.

     

/

返回文章
返回