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Investigation on nanoadhesive bonding of plasma modified titanium for aerospace application
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  • Investigation on nanoadhesive bonding of plasma modified titanium for aerospace application
  • Investigation on nanoadhesive bonding of plasma modified titanium for aerospace application
저자명
Ahmed. Sabbir,Chakrabarty. Debabrata,Mukherjee. Subroto,Joseph. Alphonsa,Jhala. Ghanshyam,Bhowmik. Shantanu
간행물명
Advances in aircraft and spacecraft science
권/호정보
2014년|1권 1호|pp.1-14 (14 pages)
발행정보
테크노프레스
파일정보
정기간행물|ENG|
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기타
이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
서지반출

기타언어초록

Physico-chemical changes of the plasma modified titanium alloy [Ti-6Al-4V] surface were studied with respect to their crystallographic changes by X-Ray Diffraction (XRD) and Scanning Electron Microscope (SEM).The plasma-treatment of surface was carried out to enhance adhesion of high performance nano reinforced epoxy adhesive, a phenomenon that was manifested in subsequent experimental results. The enhancement of adhesion as a consequence of improved spreading and wetting on metal surface was studied by contact angle (sessile drop method) and surface energy determination, which shows a distinct increase in polar component of surface energy. The synergism in bond strength was established by analyzing the lap-shear strength of titanium laminate. The extent of enhancement in thermal stability of the dispersed nanosilica particles reinforced epoxy adhesive was studied by Thermo Gravimetric Analysis (TGA), which shows an increase in onset of degradation and high amount of residuals at the high temperature range under study. The fractured surfaces of the joint were examined by Scanning electron microscope (SEM).