高空风能捕获伞梯系统空气动力学原理及建模

Aerodynamic principles and modeling of high-altitude wind harvesting parachute systems

  • 摘要: 高空风能具有功率密度大、风向风速平稳等优势,对其进行大规模开发并利用的潜力大。现有伞梯式陆基高空风电系统已被证实是一种可行的高空风能利用方案,其通过做功伞串联形成的捕风伞梯 “兜风”捕获风能产生阻力,经系留缆绳牵引地面发电机转化为电能。目前伞梯系统的空气动力学原理尚不清晰,缺乏分析模型,为明晰其受力特性、掌握运行姿态以实现稳定高效运行,本文对其开展力学原理建模研究。首先针对伞梯倾斜往复运动的特点,结合做功伞与降落伞的气动相似性,厘清了捕风伞梯系统空气动力学原理。然后结合环境参数,构建了兼顾设计参数及运行参数的伞梯系统力学模型。进一步通过极值分析推导出系统输出功率最大时,放绳速度满足风速三分之一的匹配关系,功率误差小于1.7%。最后,基于力学模型与最优绳速匹配关系实现了伞梯系统最大输出功率测算及运行姿态安全性评估,以及特定目标功率、稳定性与工程实现等约束条件下的伞梯快速设计。

     

    Abstract: High-altitude wind energy exhibits significant advantages, such as high power density and stable wind direction and speed, thereby demonstrating great potential for large-scale development and utilization. A ground-based airborne wind energy system utilizing a parachute-ladder configuration offers a feasible solution, with its core component being the energy-harvesting parachute system composed of a series of working parachutes. The system captures wind energy primarily through drag-based "wind-catching" by the parachutes, which pull a ground-based generator via a tether to convert energy into electricity. First, considering the inclined reciprocating motion of the ladder and the aerodynamic similarity between working parachutes and deceleration parachutes, the aerodynamics of the energy-harvesting parachute system are clarified. Then, incorporating environmental parameters, a mechanical model of the system is developed that accounts for both design and operational parameters. Furthermore, through extremum analysis, the optimal power matching condition is derived, indicating that the tether speed should be one-third of the wind speed to achieve maximum power output (<1.7% error). Finally, based on the mechanical model and the optimal tether-speed matching condition, the maximum power output of the system is calculated, operational safety is evaluated, and a rapid design approach for the parachute system is achieved under constraints such as specific target power, stability, and engineering feasibility. Overall, the mechanical model provides a practical design tool for parachute systems under expected operating conditions.

     

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