飞机油箱移动副冗余四足机器人运动学与穿越可行性分析
李双宝 , 路志强 , 彭文伶 , 刘国光 , 寇力英
中国民航大学学报 ›› 2026, Vol. 44 ›› Issue (5) : 14 -23.
飞机油箱移动副冗余四足机器人运动学与穿越可行性分析
Kinematics and traversal feasibility of a quadruped robot with prismatic-joint redundancy for aircraft fuel tanks
针对传统油箱巡检四足机器人难以穿越检修口的问题,本文首先引入直线导轨并配合髋部翻转重构腿部自由度配置,使摆动腿在有限净空内分阶段完成穿越,而不将检修口边框作为支撑点;其次,开展整体结构设计、腿部机构设计与运动学建模,并在连杆尺寸和关节限位相同的条件下,对引入移动副前后的检修口远侧落足可达性及构型冗余进行分析;最后,在固定阶段顺序下进行穿越轨迹规划,并对候选穿越序列开展逐帧审计。结果表明,引入移动副后,四腿平均离散落足点可达率由50.0%提升至92.9%,检修口远侧落足区面积覆盖率由约26%提升至约96%,构型切换可为同一落足点提供姿态冗余;696帧候选穿越序列的最小检修口边框间隙为26.989 mm,最小静态稳定裕度(SSM,static stability margin)为9.034 mm,自碰撞距离始终为正,说明该分阶段穿越路径在本文数字模型与名义工况下具有数值可行性。研究结果可为飞机油箱巡检机器人以低接触风险穿越舱间检修口提供腿部机构设计与穿越规划依据。
To address the problem that conventional quadruped robots for fuel tank inspection can hardly traverse an inspection opening, this paper firstly introduces a linear guide rail and combines it with hip flipping to reconfigure the leg degree-of-freedom layout. The swing leg can thus complete the traversal in stages within the limited clearance without taking the inspection opening frame as a supporting point. Secondly, the overall structure and the leg mechanism are designed, and a kinematic model is established. Under identical link dimensions and joint limits, the reachability of footholds on the far side of the inspection opening and the configuration redundancy are then analyzed before and after the prismatic joint is introduced. Finally, the traversal trajectory is planned under a fixed stage sequence, and the candidate traversal sequence is audited frame by frame. The results show that, after the prismatic joint is introduced, the average reachability rate of discrete footholds of the four legs increases from 50.0% to 92.9%. The area coverage of the far-side foothold region of the inspection opening increases from about 26% to about 96%. Configuration switching can provide posture redundancy for the same foothold. For the 696-frame candidate traversal sequence, the minimum clearance from the inspection opening frame is 26.989 mm, and the minimum static stability margin (SSM) is 9.034 mm. The self-collision distance remains positive, indicating that the staged traversal path is numerically feasible under the digital model and nominal working conditions adopted in this study. The results can provide a basis for the leg mechanism design and traversal planning of aircraft fuel tank inspection robots that traverse inter-bay inspection openings with low contact risk.
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