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Open Access

A trajectory planning method on error compensation of residual height for aero-engine blades of robotic belt grinding

Chong LVLai ZOU( )Yun HUANGXifan LIUZhaorui LIMingwang GONGHeng LI
State Key Laboratory of Mechanical Transmission, Chongqing University, Chongqing 400044, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

While the traditional trajectory planning methods are used in robotic belt grinding of blades with an uneven machining allowance distribution, it is hard to obtain the preferable profile accuracy and surface quality to meet the high-performance requirements of aero-engine. To solve this problem, a novel trajectory planning method is proposed in this paper by considering the developed interpolation algorithm and the machining allowance threshold. The residual height error obtained from grinding experiments of titanium alloy sample was compensated to modify the calculation model of row spacing, and a new geometric algorithm was presented to dynamically calculate the cutter contact points based on this revised calculation model and the dichotomy method. Subsequently, the off-line machining program is generated based on a double-vector controlling method to obtain an optimal contact posture. On this basis, three sets of robotic grinding tests of titanium alloy blades were conducted to investigate the advantages of the proposed method. The comparative experimental results revealed that the presented algorithm had improved the surface profile accuracy of blade by 34.2% and 55.1%, respectively. Moreover, the average machined surface roughness was achieved to 0.3 µm and the machining efficiency was obviously promoted. It is concluded that this research work is beneficial to comprehensively improve the machined quality of blades in robotic belt grinding.

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Chinese Journal of Aeronautics
Pages 508-520

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Cite this article:
LV C, ZOU L, HUANG Y, et al. A trajectory planning method on error compensation of residual height for aero-engine blades of robotic belt grinding. Chinese Journal of Aeronautics, 2022, 35(4): 508-520. https://doi.org/10.1016/j.cja.2021.06.018

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Received: 25 December 2020
Revised: 25 January 2021
Accepted: 23 April 2021
Published: 07 July 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).