双稳态空中变压器 (BAT):通过被动软机制动态变形的四旋翼固定翼混合动力机

Jessica Weakly, Xuan Li, Tejas Agarwal, Minchen Li, Spencer Folk, Chenfanfu Jiang, Cynthia Sung
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摘要

航空飞行器在执行任务时,需要在设计过程中进行权衡,如航程、速度、机动性和尺寸。多模式航空飞行器可以在飞行过程中进行这种权衡。本文介绍的双稳态空中变压器(BAT)机器人是一种新型变形混合飞行器(HAV),可通过快速加速在四旋翼和固定翼模式之间切换,除正常飞行所需的驱动外无需任何额外驱动。该设计的特点是采用热塑性聚氨酯(TPU)制成的顺应式双稳态机构,在机器人身体中心承载一个大质量。加速时,惯性力会使飞行器在稳定模式之间转换,而与双稳态机构相连的四杆连杆则会使飞行器的机翼折叠或收起。论文包括完整的机器人设计以及制造系统与弹性动力学模拟的比较。飞行中期两种模式之间的成功转换以及每种模式下的持续飞行表明,飞行器在四旋翼模式下具有更高的灵活性,在固定翼模式下具有更高的飞行效率,而每对转换的能量等效成本仅为 2 秒钟的飞行时间。该飞行器展示了如何将顺从和双稳态机制集成到未来的航空飞行器中,实现可控的自我重新配置,以完成监视和采样等需要机动性和长距离飞行相结合的任务。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Bistable Aerial Transformer (BAT): A Quadrotor Fixed-Wing Hybrid that Morphs Dynamically via Passive Soft Mechanism
Aerial vehicle missions require navigating trade-offs during design, such as the range, speed, maneuverability, and size. Multi-modal aerial vehicles enable this trade-off to be negotiated during flight. This paper presents a Bistable Aerial Transformer (BAT) robot, a novel morphing hybrid aerial vehicle (HAV) that switches between quadrotor and fixed- wing modes via rapid acceleration and without any additional actuation beyond those required for normal flight. The design features a compliant bistable mechanism made of thermoplastic polyurethane (TPU) that bears a large mass at the center of the robot's body. When accelerating, inertial forces transition the vehicle between its stable modes, and a four-bar linkage connected to the bistable mechanism folds the vehicle's wings in and out. The paper includes the full robot design and a comparison of the fabricated system to the elastodynamic simulation. Successful transitions between the two modes in mid-flight, as well as sustained flight in each mode indicate that the vehicle experiences higher agility in the quadrotor mode and higher flight efficiency in the fixed-wing mode, at an energy equivalent cost of only 2 s of flight time per pair of transitions. The vehicle demonstrates how compliant and bistable mechanisms can be integrated into future aerial vehicles for controllable self-reconfiguration for tasks such as surveillance and sampling that require a combination of maneuverability and long-distance flight.
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