中国民航大学学报 ›› 2026, Vol. 44 ›› Issue (5): 14-23.doi: 10.27055/j.1674-5590.2026.05.002

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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 

  

  1. 1. 中国民航大学 a. 科技创新研究院;b. 航空工程学院;c. 交通科学与工程学院;d. 理学院,天津 300300; 2. 深圳航空有限责任公司,广东 深圳 518128
  • 收稿日期:2026-08-06 修回日期:2026-09-17 出版日期:2026-10-30 发布日期:2026-10-30
  • 作者简介:李双宝(1978— ),男,河北承德人,教授,博士,研究方向为飞机地面动力学与安全评估、机械系统非线性动力学.
  • 基金资助:
    天津市自然科学基金联合基金资助项目(25JCLMJC00630)

Kinematics and traversal feasibility of a quadruped robot with prismatic-joint redundancy for aircraft fuel tanks

  1. 1a. Research Institute of Science and Technology Innovation; 1b. College of Aeronautical Engineering; 1c. College of Transportation Science and Engineering; 1d. College of Science, CAUC, Tianjin 300300, China; 2. Shenzhen Airlines Co., Ltd., Shenzhen 518128, Guangdong, China
  • Received:2026-08-06 Revised:2026-09-17 Online:2026-10-30 Published:2026-10-30

摘要: 针对传统油箱巡检四足机器人难以穿越检修口的问题袁本文首先引入直线导轨并配合髋部翻转重构腿部 自由度配置袁使摆动腿在有限净空内分阶段完成穿越袁而不将检修口边框作为支撑点曰其次袁开展整体结构 设计尧腿部机构设计与运动学建模袁并在连杆尺寸和关节限位相同的条件下袁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曰最后袁在固定阶段顺序下进行穿越轨迹规划袁并对候选穿越序列开 展逐帧审计遥结果表明袁引入移动副后袁四腿平均离散落足点可达率由 50.0%提升至 92.9%袁检修口远侧 落足区面积覆盖率由约26%提升至约 96%袁构型切换可为同一落足点提供姿态冗余曰696 帧候选穿越序列 的最小检修口边框间隙为 26.989 mm袁最小静态稳定裕度渊SSM袁static stability margin冤为 9.034 mm袁自碰撞 距离始终为正袁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遥研究结果可为飞机 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

Abstract: To address the problem that conventional quadruped robots for fuel tank inspection can hardly traverse an in spection 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, af鄄 ter 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.

Key words: aircraft fuel tanks, quadruped robot, prismatic-revolute-revolute-revolute (PRRR) mechanism, foothold reachability

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