2016
DOI: 10.1016/j.procir.2016.02.293
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EDM Drilling and Shaping of Cooling Holes in Inconel 718 Turbine Blades

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Cited by 70 publications
(29 citation statements)
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“…The input parameters are drilling speed, recast layer thickness, and hole taper. In Inconel 718, drilling and shaping process made into a single progression with identical electrode found that shape accuracy is affected by relative tool wear [10]. MRR, relative tool wear, and surface reliability are the objective parameters.…”
Section: Literature Reviewmentioning
confidence: 99%
“…The input parameters are drilling speed, recast layer thickness, and hole taper. In Inconel 718, drilling and shaping process made into a single progression with identical electrode found that shape accuracy is affected by relative tool wear [10]. MRR, relative tool wear, and surface reliability are the objective parameters.…”
Section: Literature Reviewmentioning
confidence: 99%
“…The erosion current, I d , is set to 8 A and open voltage, U op , is set to 100 V. As mentioned in [36], the layer thickness per one pass cannot be higher than a half of electrode radius, which is considered in the present work. The diameter of the pyrometer fiber is 0.5 mm.…”
Section: Desigmentioning
confidence: 99%
“…Due to extremely tough nature (such as lower thermal conductivity, high work hardening, presence of abrasive carbide particles, high hardness, affinity to react with tool material, high toughness) of the Inconel 718 superalloy, the making of high aspect ratio holes in its structure involves significant difficulties in the case of conventional machining [5,6]. In order to overcome the limitations, the aerospace industry currently applies non-conventional methods such as electrochemical machining (ECM), laser beam machining (LBM) and electrical discharge machining (EDM) to produce micro-scale cooling holes in superalloy materials [7].…”
Section: Introductionmentioning
confidence: 99%
“…To enhance the additional resistance of these materials of components into high temperature, a considerable number of holes (20,000-40,000) with a diameter in the range of 0.3-5 mm and an aspect ratio in the range of (40-600):1 (depth-to-diameter ratio) are made in their structure [5,[8][9][10]. The main task of the holes (named "cooling holes") is to reduce the temperature of the component material by flow of the cooling factor (gas or liquid) through the holes [7]. The efficiency of the cooling process depends on the dimensional shape accuracy and the quality of the holes' inner surface.…”
Section: Introductionmentioning
confidence: 99%