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Recent advances in drilling hybrid FRP/Ti composite: A state-of-the-art review

Article dans une revue avec comité de lecture
Auteur
XU, Jinyang
ccEL MANSORI, Mohamed
211915 Mechanics surfaces and materials processing [MSMP]
ccMKADDEM, Ali
546361 Department of Mechanical Engineering, Faculty of Engineering – North Jeddah Campus, King Abdulaziz University, Jeddah, Saudi Arabia

URI
http://hdl.handle.net/10985/17655
DOI
10.1016/j.compstruct.2015.09.028
Date
2016
Journal
Composite Structures

Résumé

Hybrid composite stack, especially FRP/Ti assembly, is considered as an innovative structural configuration for manufacturing the key load-bearing components favoring energy saving in the aerospace industry. Several applications require mechanical drilling for finishing hybrid composite structures. The drilling operation of hybrid FRP/Ti composite, however, represents the most challenging task in modern manufacturing sectors due to the disparate natures of each constituent involved and the complexity to control tool–material interfaces during one single cutting shot. Special issues may arise from the severe subsurface damage, excessive interface consumption, rapid tool wear, etc. In this paper, a rigorous review concerning the state-of-the-art results and advances on drilling solutions of hybrid FRP/Ti composite was presented by referring to the wide comparisons among literature analyses. The multiple aspects of cutting responses and physical phenomena generated when drilling these materials were precisely addressed. A special focus was made on the material removal modes and tool wear mechanisms dominating the bi-material interface consumption (BIC) with respect of investigating strategies used. The key conclusions from the literature review were drawn to point out the potential solutions and limitations to be necessarily overcome for reaching both (i) enhanced control of drilling operation, and (ii) better finish quality of FRP/Ti parts

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  • Laboratoire Mechanics, Surfaces and Materials Processing (MSMP)

Documents liés

Visualiser des documents liés par titre, auteur, créateur et sujet.

  • Orthogonal cutting mechanisms of CFRP/Ti6Al4V stacks 
    Article dans une revue avec comité de lecture
    XU, Jinyang; CHEN, Ming; REN, Fei; ccEL MANSORI, Mohamed (Springer Verlag, 2019)
    The enhanced mechanical/physical properties and improved functionalities have made the carbon fiber–reinforced polymer/titanium alloy (CFRP/Ti6Al4V) stacks very attractive to the modern aerospace industry. However, the ...
  • An investigation of drilling high-strength CFRP composites using specialized drills 
    Article dans une revue avec comité de lecture
    XU, Jinyang; LI, Chao; CHEN, Ming; REN, Fei; ccEL MANSORI, Mohamed (Springer Verlag, 2019)
    Machining of high-strength carbon fiber reinforced polymers (CFRPs) has faced great challenges in quality control and tool wear management due to their inherent heterogeneity and high abrasiveness leading to serious workpiece ...
  • A Study on Drilling High-Strength CFRP Laminates: Frictional Heat and Cutting Temperature 
    Article dans une revue avec comité de lecture
    XU, Jinyang; LI, Chao; DANG, Jiaqiang; REN, Fei; ccEL MANSORI, Mohamed (MDPI, 2018)
    High-strength carbon fiber reinforced polymer (CFRP) composites have become popular materials to be utilized in the aerospace and automotive industries, due to their unique and superior mechanical properties. An understanding ...
  • Cutting Modeling of Hybrid CFRP/Ti Composite with Induced Damage Analysis 
    Article dans une revue avec comité de lecture
    XU, Jinyang; ccEL MANSORI, Mohamed (MDPI, 2016)
    In hybrid carbon fiber reinforced polymer (CFRP)/Ti machining, the bi-material interface is the weakest region vulnerable to severe damage formation when the tool cutting from one phase to another phase and vice versa. The ...
  • Wear characteristics of polycrystalline diamond tools in orthogonal cutting of CFRP/Ti stacks 
    Article dans une revue avec comité de lecture
    XU, Jinyang; ccEL MANSORI, Mohamed (Elsevier, 2017)
    CFRP/Ti stacks have become a viable alternative to conventional composite laminates and metal alloys in various aerospace applications because of their enhanced mechanical properties and improved structural functions. ...

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