A Novel Approach For The Fabrication of High Performance Titanium Alloy Laminate For Aerospace Application
In this investigation attempts have been made to modify the surface characteristics of titanium in order to increase the adhesion of high performance epoxy based nano adhesive which in turn would help in fabricating a high heat resistant weather proof high performance laminate with prolonged durability meant for aerospace application. The surface modification was carried out by Plasma Nitriding. The plasma treated Ti surface was coated with high performance epoxy based adhesive containing nano reinforcing materials and then laminated with another sheet of treated titanium. After necessary curing of the adhesive the laminate was subjected to various mechanical,thermal, and morphology studies.
Introduction surf ace modification characterization adhesive properties and characterization
Sabbir Ahmed Ayan Dey Alphonsa Joseph Ghanshyam Jhala Subrata Mukherjee Debabrata Chakraborty Shantanu Bhowmik
International Centre for Nanotechnology and Applied Adhesion,SikkimManipal University,Majitar,Rangpo Polymer Science and Technology,Calcutta University,Kolkata-700009,West Bengal,India Facilitation Centre for Industrial Plasma technologies,Institute of Plasma Research,Gandhinagar-3820 Faculty of Aerospace Engineering,Del ft University of Technology Kluyverweg 1,2629 HS Delft,The Neth
国际会议
The 12th World Conference Titanium(第十二届世界钛会 Ti-2011)
北京
英文
1948-1951
2011-06-19(万方平台首次上网日期,不代表论文的发表时间)