2014
DOI: 10.1177/0954405413508117
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Mechanism of damage generation during drilling of carbon/epoxy composites and titanium alloy stacks

Abstract: Composite/metal stacks are widely used in aerospace structures. To study the mechanism of damage generation during drilling of carbon/epoxy composites and titanium alloy stacks, both traditional drilling and orbital drilling were used. Because the cutting parameters of the two drilling processes were different from each other, an appropriate comparing method was proposed based on the analysis of kinematics of orbital drilling and traditional drilling. The results show that high cutting temperature is the main … Show more

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Cited by 41 publications
(32 citation statements)
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“…There are damages caused on the drilled composite materials as a result of their composition such as delamination, hole dimensional inaccuracy, surface roughness, fuzzing and composite fibre pull-out or uncut fibres. 99,104,105 The damaged composite materials are susceptible to fatigue strength and load bearing capacity. 105 Problems associated with drilling of CFRC laminate materials Kim and Ramulu 47 reported that for years, carbon fibre composites have been drilled using the same methods applied in drilling metals.…”
Section: Composition Of Carbon Fibre Compositesmentioning
confidence: 99%
See 1 more Smart Citation
“…There are damages caused on the drilled composite materials as a result of their composition such as delamination, hole dimensional inaccuracy, surface roughness, fuzzing and composite fibre pull-out or uncut fibres. 99,104,105 The damaged composite materials are susceptible to fatigue strength and load bearing capacity. 105 Problems associated with drilling of CFRC laminate materials Kim and Ramulu 47 reported that for years, carbon fibre composites have been drilled using the same methods applied in drilling metals.…”
Section: Composition Of Carbon Fibre Compositesmentioning
confidence: 99%
“…106 Among these, delamination is the most critical defect as it has the highest level of impact on accuracy and quality of a drilled hole. 54,105 Delamination Delamination in a composite material occurs whereby reinforced fibre plies separate, either by peel-up or push-out phenomenon. This defect occurs at the upper most layer of the laminate from the rest of the body and/or on the drill bit's tip which pushes the bottom layers of the laminate, respectively 77,107 (Figure 7).…”
Section: Composition Of Carbon Fibre Compositesmentioning
confidence: 99%
“…В [12] описана обработка отверстия спиральными сверлами в двухслойном пакете углепластик-титан. Толщина слоя композита составляла 5 мм, титана -4 мм.…”
Section: а) б)unclassified
“…Experimental setup for drilling of CFRP/Ti stacks and cutting tools surface condition: a) Infrared thermal camera and temperature measurement points for CFRP/Ti stacks and b) Titanium alloy adhered to the cutting tool edge) Delme işlemi esnasında KETPK/Ti'nin farklı bölgelerinde oluşan sıcaklıklar, a) A noktası, b) B noktası ve c) C noktası[52] (Temperatures in different areas of CFRP/Ti stacks during drilling: a) A point, b) B point and c) C point) Gr-Bi/Ti istiflenmiş plakaların delinmesi: a) Standart HSS matkaplar için derinliğe bağlı olarak tork ve ilerleme kuvvetindeki değişim (N: 660 dev/dak, f:0,2mm/dev) ve b) HSS kobalt matkap ile delinmiş Gr-Bi/Ti plakaların üstten ve yandan görünüşü(N: 660 dev/dak, f:0,13 mm/dev)[53] (Drilling of Gr-Bi/Ti stack: a) Relationship torque and thrust force depending on depth for standard HSS drills (N:660 rev/min, f:0.2 mm/rev) and b) Top and side view of Gr-Bi/Ti stack drilled by a HSS-Co drill (N:660 rev/min, f:0.13 mm/rev))…”
mentioning
confidence: 99%
“…KETPK/Ti'nin delinmesi için deney düzeneği ve kesici takım yüzey durumu, a) Kızıl ötesi termal kamera ve KETPK/Ti istiflenmiş yapı için sıcaklık ölçüm noktaları ve b) Titanyum alaşımının kesici takım kenarına yapışması[52] …”
unclassified