Improvement of Hole Drilling in High-Strength Polymer Laminate


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When the end section of helicopter screw blades made of polymer laminate based on glass–carbon fiber and reinforced by titanium foil is drilled, peeling is noted at the entrance to the hole. Such peeling is investigated in the present work. The influence of the cutting speed and supply on the extent of the peeling is established.

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A. Maslov

Stankin Moscow State Technical University

编辑信件的主要联系方式.
Email: vestnik@stankin.ru
俄罗斯联邦, Moscow

A. Mamot’ko

Stankin Moscow State Technical University

Email: vestnik@stankin.ru
俄罗斯联邦, Moscow

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