2017
DOI: 10.1007/s00170-017-1339-1
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In situ chip formation analyses in micro single-lip and twist deep hole drilling

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Cited by 10 publications
(5 citation statements)
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“…With the aggravation of wear and the deterioration of the lubrication conditions of the chip and the rake face, the roughness of the chip's extruded surface is increased, and grooves appear. The friction between the chip and the rake face increases, the resistance of the chip flow increases, and the chip thickness increases [31,32]. In addition, after the bluntness of the teeth and the abrading of tool coating, the cutting force, and the heat generated in the cutting zone increase.…”
Section: Chimentioning
confidence: 99%
“…With the aggravation of wear and the deterioration of the lubrication conditions of the chip and the rake face, the roughness of the chip's extruded surface is increased, and grooves appear. The friction between the chip and the rake face increases, the resistance of the chip flow increases, and the chip thickness increases [31,32]. In addition, after the bluntness of the teeth and the abrading of tool coating, the cutting force, and the heat generated in the cutting zone increase.…”
Section: Chimentioning
confidence: 99%
“…However, this super high strength steel has extremely poor cutting performance and belongs to the typical aviation difficult processing material. In the current cutting process, there are the following main problems [5][6][7]: ① is the complex inner cavity of the landing gear front / main piston rod and the outer cylinder parts of the modern advanced aircraft and the large aircraft, the step hole, the ring slot, the keyway, the conical hole, the threaded hole, Many special structures such as bottom cavity coexist, which makes machining more difficult, especially in deep hole machining, the cutter rod is more deep, the rigidity of tool rod is insufficient and the inherent defect of tool durability is low, it is very difficult to meet the machining requirements of parts.② in the front / main lifting cylinder and piston rod of the landing gear, most of the parts are deep holes whose aspect ratio is greater than 10, the main difficulties in machining these parts are the large cutting force, the easy wear of the tool, the low durability, the long chip-discharge channel and the difficult chip removal [8][9][10].…”
Section: Introductionmentioning
confidence: 99%
“…Nickel-based alloy materials have a range of advantages, such as high strength, high temperature resistance, and corrosion resistance, enabling engines to withstand extremely high temperatures and mechanical stresses, and are widely used in the aerospace industry [1][2][3]. However, the high elongation and low thermal conductivity of nickel-based alloy led to significant plastic deformation resistance and high cutting temperature during the machining, which is prone to tool sticking, resulting in tool wear and work hardening, affecting chip flow direction and fracture [4][5][6][7]. Therefore, automatic chip breakage during the machining of nickel-based alloy is a critical factor that restricts high-quality and efficient processing.…”
Section: Introductionmentioning
confidence: 99%