Chisel Edge and Pilot Hole Effects in Drilling Composite Laminates
By M. Won, C. Dharan. 2002
179 citations recorded by the source corpus.
Subfields: Biomedical Engineering, Electrical and Electronic Engineering, Mechanical Engineering
View Paper: https://www.semanticscholar.org/paper/ea64a9fa4b62c5cc5266206406732cf02166dd19
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In Biomedical Engineering
In Electrical and Electronic Engineering
In Mechanical Engineering
Citations in the corpus
- The effect of chisel length and associated pilot hole on delamination when drilling composite materials (2003, methodology): “force, and an innovative process model was developed to predict the advantage of a specimen with pre-drilled pilot hole [24].”
- Drill geometry and operating effects when cutting small diameter holes in CFRP (2009, methodology): “The use of pilot hole strategies prior to finish sizing can considerably reduce thrust force due to the absence of contact between chisel edge and work material, thus further reducing delamination [13].”
- Study of drilling of composite material and aluminium stack (2010, background): “[41] show that the thrust force due to the chisel edge is 40% from the total thrust force when feed rate is low and 60% when the feed rate is high.”
- Drilling tool geometry evaluation for reinforced composite laminates (2010, background): “Won and Dharan [17] determined quantitatively the effect of chisel edge and a pilot hole in composites laminates drilling.”
- Effects of special drill bits on drilling-induced delamination of composite materials (2006, unknown): “Recently, Won and Dharan investigated the effect of chisel edge on the thrust force, and an innovative process model was developed to predict the advantage of a specimen with pre-drilled pilot hole [34].”
- Experimental study of drilling composite materials with step-core drill (2008, background): “Pre-drilled, back-up plates and special drills can reduce delamination when drilling composite materials [5–13].”