High-performance processing of film cooling holes with a picosecond fiber laser in DD6 single-crystal superalloy

The configuration accuracy and inner surface quality of film cooling holes (FCHs) critically influence the cooling efficiency and fatigue resistance of aero-engine turbine blades. A highly stable and high-power picosecond fiber laser was input into a helical scanning machining head, and integrated into a five-axis cradle machine, so as to establish a high-efficiency and high-stability system for precision drilling FCHs. In order to overcome the high thermal effects of picosecond laser, a three-step processing strategy was proposed and systematically optimized. In step 1, a through-hole was rapidly pierced by fully spiral scanning, where high-pressure gas effectively removes ablated ejecta, thereby improving processing efficiency and depressing thermal effects. Step 2 produces taper-free holes with designed sizes by half spiral scanning. Step 3 eliminates the thin surface layer on the inner wall by helical scanning, effectively reducing the oxygen content and surface roughness. High-quality taper-free FCHs were efficiently fabricated on a 1.5 mm thick DD6 single-crystal superalloy in 39 s, featured with a diameter of 500 ± 3.5 μm, roundness of 98%, and heat affected zone width below 7 μm on average. Furthermore, the inner wall surface quality was excellent, characterized by extremely low roughness and oxygen content, with average values of 0.145 μm and 2.95 wt.%, respectively. This technique has been successfully applied to turbine blade specimens, where the processed FCHs demonstrate stable water flow performance compliant with design requirements, indicating broad prospects for industrial applications. • A ps fiber laser with a helical scanning head enables stable FCH drilling in DD6. • A three-step processing strategy reduces thermal effects and improves efficiency. • Taper-free FCHs (500 ± 3.5 μm, 98% roundness, 2.9 μm HAZ) achieved within 39 s. • Inner walls show Ra 0.145 μm and 2.95 wt.% Oxygen with uniform LIPSS distribution. • Turbine blade with FCHs demonstrates stable water flow and industrial applicability.

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Publication Details

Journal
Journal of Manufacturing Processes
Published
2026-03-05
DOI
https://doi.org/10.1016/j.jmapro.2026.02.055
Primary Topic
Solid State Laser Technologies
Type
article
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article

High-performance processing of film cooling holes with a picosecond fiber laser in DD6 single-crystal superalloy

Mengqi Suo, Zhenrong Sun Zhenrong Sun, Donghai Feng Donghai Feng, Tianqing Jia Tianqing Jia et al.
Journal of Manufacturing Processes
Solid State Laser Technologies
article

High-performance processing of film cooling holes with a picosecond fiber laser in DD6 single-crystal superalloy

Mengqi Suo, Zhenrong Sun Zhenrong Sun, Donghai Feng Donghai Feng, Tianqing Jia Tianqing Jia, Kang Li, Chaowei Sun, Mingyang Xin, Hongxing Xu, Shian Zhang, Kaiqiang Cao, Jichao Yang
article en

Abstract

The configuration accuracy and inner surface quality of film cooling holes (FCHs) critically influence the cooling efficiency and fatigue resistance of aero-engine turbine blades. A highly stable and high-power picosecond fiber laser was input into a helical scanning machining head, and integrated into a five-axis cradle machine, so as to establish a high-efficiency and high-stability system for precision drilling FCHs. In order to overcome the high thermal effects of picosecond laser, a three-step processing strategy was proposed and systematically optimized. In step 1, a through-hole was rapidly pierced by fully spiral scanning, where high-pressure gas effectively removes ablated ejecta, thereby improving processing efficiency and depressing thermal effects. Step 2 produces taper-free holes with designed sizes by half spiral scanning. Step 3 eliminates the thin surface layer on the inner wall by helical scanning, effectively reducing the oxygen content and surface roughness. High-quality taper-free FCHs were efficiently fabricated on a 1.5 mm thick DD6 single-crystal superalloy in 39 s, featured with a diameter of 500 ± 3.5 μm, roundness of 98%, and heat affected zone width below 7 μm on average. Furthermore, the inner wall surface quality was excellent, characterized by extremely low roughness and oxygen content, with average values of 0.145 μm and 2.95 wt.%, respectively. This technique has been successfully applied to turbine blade specimens, where the processed FCHs demonstrate stable water flow performance compliant with design requirements, indicating broad prospects for industrial applications. • A ps fiber laser with a helical scanning head enables stable FCH drilling in DD6. • A three-step processing strategy reduces thermal effects and improves efficiency. • Taper-free FCHs (500 ± 3.5 μm, 98% roundness, 2.9 μm HAZ) achieved within 39 s. • Inner walls show Ra 0.145 μm and 2.95 wt.% Oxygen with uniform LIPSS distribution. • Turbine blade with FCHs demonstrates stable water flow and industrial applicability.

Journal of Manufacturing ProcessesVol. 165
Beijing Institute of Technology (CN), Henan Academy of Sciences (CN), East China Normal University (CN)
Affordable and clean energy
Openalex Percentile: Top 34%
Solid State Laser Technologies
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