Fretting fatigue
Fretting fatigue
Fretting fatigue and wear describes the break down of solid materials in large scale machinery over the course of everyday operation.
A common example is in the dovetail joint between a turbine blade and the central rotating disk in, for example, an engine. This is illustrated schematically in the picture. As the blade spins, the applied loads - the force, F, and torque, T, in the picture - cause the contact region (lower part of the picture) between the blade and the central disk to change.
Locally, this leads to variations in the contact pressure and shear in the contact region. Typically, they will cycle through different values.
This constant cycling can lead to what is known as slip in the contact region between the solids.
Slip is believed to by the major cause of solid degradation, wear and eventual breakdown, so obviously is something to avoid!
These types of contacts occur widely in large industrial machinery, from turbine engines to heads in oil well risers. Sometimes these are had to access, so understanding how and why degradation occurs is of vital importance in condition monitoring and/or predictive maintenance!
My interest in the area is twofold.
Firstly, I am interested in what is known as half-plane theory, which exploits the fact that in large machines, we can often approximate the solid shapes by large half-planes in a linear elastic regime.
Secondly, given that in many industrial settings the geometry of the machine is quite complex, we often seek approximate or asymptotic solutions to the problem. This typically involves concentrating at the edge of the contact region as this is invariably where the effects of slip first arise.
Both of these strands are in collaboration with Prof. David Hills' group in the Department of Engineering at the University of Oxford. You can see my recent work on the Publications page.