Microstructural investigation of drilling induced damage in fibre metal laminates constituents

被引:40
作者
Giasin, Khaled [1 ]
Ayvar-Soberanis, Sabino [2 ]
机构
[1] Univ Sheffield, Composite Syst Innovat Ctr, Dept Mech Engn, Garden St,North Campus,Broad Lane, Sheffield S3 7HQ, S Yorkshire, England
[2] Univ Sheffield, Adv Mfg Res Ctr Boeing, Adv Mfg Pk,Wallis Way, Rotherham S60 5TZ, S Yorkshire, England
关键词
Machining; Delamination; Fibre metal laminates; Coolants; MINIMUM QUANTITY LUBRICATION; THRUST FORCE; COMPOSITE-MATERIALS; HOLE QUALITY; CUTTING PARAMETERS; TOOL WEAR; DELAMINATION; CFRP; GFRP; MQL;
D O I
10.1016/j.compositesa.2017.02.024
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Fibre metal laminates (FMLs) are used in the upper fuselage of the Airbus A380 aircraft. Machining FMLs might cause various forms of damage around the hole either in the composite layers or the metallic sheets, all of which are known as drilling-induced damage which deteriorates the surface quality of the metal/composite. The current study investigates the effects of cutting parameters on the drilling induced damage during drilling of GLARE FMLs at a microstructural level. This study extends the previous investigation of our study on dry drilling of GLARE laminates by incorporating two modern cooling technologies namely cryogenic liquid nitrogen (LN2) and minimum quantity lubrication (MQL) to investigate their impact on drilling-induced damage in FMLs. The results showed that both cutting parameters had an impact on the drilling induced damage in the borehole, while using MQL and cryogenic coolants showed the ability to eliminate waste formation on the machined borehole surface. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:166 / 178
页数:13
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