水空两用螺旋桨设计及其气动-水动力性能数值研究

Design and numerical investigation on aero-hydrodynamic performance of an aerial-aquatic propeller

  • 摘要: 水空两用螺旋桨是无人水空飞行器的核心部件。本文针对水空两用螺旋桨空中和水中效率无法兼顾的问题,提出了一种基于分段设计原则的水空两用螺旋桨设计方法,将桨叶分为了水下推力设计区、水空过渡区和空中拉力设计区。其中水下推力设计区依据水下最优升阻比准则设计,保障水下推进效率;水空过渡区考虑水下推进段过渡到空中拉力段的整体平滑过渡;空中拉力设计区则专为空中拉力需求设计,其在水下巡航工况下不产生有效推力,仅贡献诱导阻力。 这种分区设计显著降低了螺旋桨水下阻力,使其在空气和水两种介质中均能维持高效运行。通过数值模拟,系统对比了本文设计的水空两用螺旋桨与传统空中螺旋桨的性能差异。结果表明:(1)空中悬停工况:优化螺旋桨悬停效率达到57%,优于传统9英寸和10英寸螺旋桨3%,但比传统12英寸螺旋桨低3% ;(2)水下工况:优化螺旋桨的推进效率较传统12英寸螺旋桨显著提升11.5%,达到59.5%,有效延长了无人水空飞行器的水下续航时间。本研究验证了所提出的分段设计策略在解决水空螺旋桨介质适应性矛盾中的有效性,为水空两用推进系统的设计提供了可靠的理论依据与技术参考。

     

    Abstract: The aerial-aquatic propeller is a core component of unmanned aerial-aquatic vehicles. Aiming at the problem that the efficiency of aerial-aquatic propellers in air and water cannot be balanced, this paper proposes a design method for aerial-aquatic propellers based on the principle of segmented design. The blade is divided into an underwater thrust design zone, a water-air transition zone, and an air pulling force design zone. The underwater thrust design zone is designed according to the criterion of the optimal lift-drag ratio underwater to ensure the underwater propulsion efficiency. The water-air transition zone considers the overall smooth transition from the underwater propulsion section to the air pulling force section. The air pulling force design zone is specially designed for air pulling force requirements. It does not generate effective thrust under the underwater cruise condition and only contributes to induced drag. This zonal design significantly reduces the underwater resistance of the propeller, enabling it to maintain efficient operation in both air and water. Through numerical simulation, the performance differences between the aerial-aquatic propeller designed in this paper and traditional air propellers are systematically compared. The results show that: (1) In the air hovering condition: The hovering efficiency of the optimized propeller is 3% better than that of traditional 9-inch and 10-inch propeller, reaching 57%, however 3% lower than that of traditional 12-inch propeller; (2) In the underwater condition: The propulsion efficiency of the optimized propeller is significantly increased by 11.5% compared with that of the traditional 12-inch propellers, reaching 59.5%, effectively extending the underwater endurance of the unmanned aerial-underwater vehicles. This study verifies the effectiveness of the proposed segmented design strategy in solving the medium adaptability contradiction of aerial-aquatic propeller and provides a reliable theoretical basis and technical reference for the design of aerial-aquatic propulsion systems.

     

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