2017
DOI: 10.1007/s10033-017-0123-3
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Machining the Integral Impeller and Blisk of Aero-Engines: A Review of Surface Finishing and Strengthening Technologies

Abstract: The integral impeller and blisk of an aero-engine are high performance parts with complex structure and made of difficult-to-cut materials. The blade surfaces of the integral impeller and blisk are functional surfaces for power transmission, and their surface integrity has significant effects on the aerodynamic efficiency and service life of an aero-engine. Thus, it is indispensable to finish and strengthen the blades before use. This paper presents a comprehensive literature review of studies on finishing and… Show more

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Cited by 70 publications
(14 citation statements)
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“…These blades are designed to have higher rigidity and lower weight compared to conventional blades. This design results in higher compressor efficiency, maximum engine thrust-to-weight ratio, and increased operational reliability for aero-engines [3].…”
Section: Introductionmentioning
confidence: 99%
“…These blades are designed to have higher rigidity and lower weight compared to conventional blades. This design results in higher compressor efficiency, maximum engine thrust-to-weight ratio, and increased operational reliability for aero-engines [3].…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, with the rapid development of digitalization and intelligent manufacturing, various CNC forms and special processing methods have been widely used in the field of blade polishing, such as CNC precision milling [3], robotic polishing [2,6], abrasive flow polishing [1], and abrasive belt polishing [5], 5-axis CNC machining is one of the most common processing methods for integral impellers [7,8], due to its advantages of high machining adaptability and controllability of machining dimensional accuracy. Although this method can successfully process an integral impeller with the surface roughness of Ra 0.8 μm, the machining trajectory planning is complicated and the tool marks on the machining surface are obvious [9].…”
Section: Introductionmentioning
confidence: 99%
“…In the working process, the parts with multi-curvature complex surface boundaries have more advantages in guiding fluid, heat transfer, wave-transmitting, and part accuracy retention than the single curvature surface boundary 1 . For example, the aero-engine blade is designed as a curved surface with torsional angles, which can improve the blade stability in the process of high-speed rotation (the rotation speed of high-pressure blades is more than 10000r/min) 2 . At the same time, the engine cooling efficiency can be improved by adding condensation holes on the blades, thus increasing the thrust-toweight ratio of the engine 3 .…”
Section: Introductionmentioning
confidence: 99%