基于软性跨介质的仿生潜空航行器设计

Design of biomimetic aerial-aquatic vehicle based on soft cross-medium technology

  • 摘要:
    目的 旨在设计一种新型潜空跨介质无人航行器,该航行器可以进行空中飞行和水下潜航,并具备反复跨介质能力和良好的流体动力性能。
    方法 对自然选择进化后具有良好流体动力学性能的蝠鲼进行外形分析,采用三维扫描和数学拟合方法开展航行器构型研究;为实现水下隐蔽推进,通过拟合蝠鲼游动步态,采用数值分析方法,确定其推进幅值和频率;为了保护旋翼并提高空飞效率,采用涵道旋翼装置作为飞行推进装置,制定软性跨介质方案,对航行器的水下快速性、空飞性能和跨介质性能进行数值仿真。
    结果 结果表明:水下航行时,仿生鱼鳍摆动周期为2 s,最大摆动角度为15°时,航行器水下航速大于3 kn;空中飞行时,当潜空航行器飞行攻角为7°且旋翼转速取3 000 r/min时,航行器空飞航速大于100 km/h;空转水时平均载荷为0.171 MPa,局部最大载荷发生在结构边缘突变处,最大应力可达0.464 MPa。对航行器底部中心施加0.17 1MPa载荷,底部边缘施加0.464 MPa载荷,结构强度计算结果表明,最大应力发生在航行器底部中心,最大应力值为47.937 MPa,最大变形值为0.17411 mm。
    结论 设计的潜空跨介质航行器满足空飞和潜航性能指标要求,且空转水方案的流体载荷和结构安全性分析结果确保了航行器可以安全多次地在空−水介质间转换。

     

    Abstract:
    Objectives This study aims to develop a concept design for an unmanned aerial-aquatic cross-medium vehicle that can fly in the air and navigate underwater, and features repeatable medium transitions and superior hydrodynamic performance.
    Methods After analyzing the shape of batoid fish that evolved good fluid dynamics performance through natural selection, 3D scanning and mathematical fitting methods are employed to conduct a configuration study of the unmanned vehicle. To achieve covert propulsion underwater, numerical analysis methods are used to determine the propulsion amplitude and frequency by fitting the swimming gaits of batoid fish. To protect the rotor blades and enhance airborne efficiency, an innovative soft hybrid cross-medium approach is developed that uses ducted rotor devices as flight propulsion units. The numerical simulation method is then employed to study the unmanned vehicle's rapid underwater movement, aerial performance, and cross-medium capabilities.
    Results The results show that during underwater navigation, with a biomimetic fish fin swinging cycle of 2 seconds and a maximum swing angle of 15°, the unmanned vehicle achieves a speed of over 3 knots. During aerial flight, with an attack angle of 7° for the hybrid vehicle and rotor speed set at 3 000 r/min, the aerial speed exceeds 100 km/h. During the transition from air to water, the average load is 0.17 MPa, with the maximum load occurring at abrupt structural edges, reaching up to 0.46 MPa stress. Structural strength calculations are performed for applying 0.17 MPa load at the center bottom and 0.46 MPa load at the bottom edge of the vehicle. The maximum stress occurs at the center bottom, measuring 47.94 MPa, with maximum deformation of 0.02 mm.
    Conclusions The designed cross-medium unmanned aerial-aquatic vehiclesatisfies the proposed requirements for both aerial and underwater operation. Furthermore, the fluid loads andstructural safety during the air-to-water transition scheme are assessed, ensuring the vehicle's ability to safelyand repeatedly shift between aerial and aquatic environments.

     

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