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March 21, 2026Aerospace2 citationsOpen Access

An Ultra-High-Aspect-Ratio Telescopic Continuum Robot Design for Aero-Engine Borescope Inspection

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DHDa HongYHYuancan HuangNSNianfeng Shao

Key Points

  • The research aims to develop a highly flexible and effective robot for inspecting internal aero-engine components.
  • Designed a telescopic continuum robot with an ultra-high aspect ratio.
  • Implemented a configuration-space control strategy for improved motion control.
  • Validated the mechanism through experimental simulation focused on turbine and compressor blades.
  • Achieved a flexible design that increases accessibility to confined spaces within aero-engines.
  • Reduced blind spots during inspections, enhancing non-destructive evaluation efficiency.
  • Demonstrated effective motion control despite challenges of multi-segment actuation and tendon slack.

Abstract

Conventional borescopes are limited by inadequate mechanical flexibility, poor environmental adaptability and reachability, and heavy reliance on operator expertise during aero-engine inspections, making it difficult to meet the demands for efficient and dependable in situ nondestructive evaluation (NDE). This paper presents a novel telescopic continuum robot mechanism with an ultra-high aspect ratio (63.75:1) and three constant-curvature segments, achieving a synergistic design between the robot’s body structure and the long-stroke linear actuator of its central backbone to realize ultra-high-aspect-ratio configurations. This design improves the robot’s ability to access complex and confined internal spaces within aero-engines, thereby reducing inspection blind spots. Furthermore, a configuration-space control strategy integrating kinematic decoupling and driving tendon tension compensation is proposed. This strategy addresses the issues of multi-segment actuation coupling and tendon slack, ensuring the motion control performance for in situ aero-engine blade inspection. The feasibility of the mechanism design was validated through an experimental simulation platform incorporating both turbine blade and compressor blade scenarios. This work offers a new solution for in situ NDE in aero-engines by synergistically integrating an innovative ultra-high-aspect-ratio telescopic mechanism with a dedicated configuration-space controller that addresses multi-segment coupling and tendon slack.

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Cite This Study

Hong et al. (2026) studied this question.

synapsesocial.com/papers/69be372b6e48c4981c676a96https://doi.org/10.3390/aerospace13030291
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